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arXiv:2608.20252v1 [math.PR] 20 Aug 2026

Notes on Hydrodynamic Limits and Related Topics

Sunder Sethuraman

University of Arizona

In these lecture notes, we discuss various ‘hydrodynamic LLN’ and ‘CLT’ scaling limits, among others, in types of stochastic interacting particle systems, connecting ‘microscopic’ behaviors to continuum laws. Via ‘short stories’, the aim is to present some of the ‘basics’ for students and those entering the field, as a complement to books such as [130], [133], [147], [148]. To be concrete, attention is restricted to a few ‘mass conservative’ systems on discrete spaces, namely exclusion and zero-range processes, that have proved robust in the study of different phenomena.

After preliminaries, we discuss the ‘entropy’ and ‘relative entropy’ methods to prove hydrodynamic limits of the bulk mass in finite volume, as well as other items such as construction of systems in infinite volume and the structure of their invariant measures, and scaling limits of local functionals, such as occupation times of sites and the motion of a tagged particle. In the last part, we also discuss equilibrium fluctuations of the bulk mass when the process starts from an invariant measure.

While such a list forms a brief introduction, there are of course several results not covered. For instance, those with respect to large deviations, mixing times, metastability and condensation phenomena, non-equilibrium fluctuations, the ‘KPZ’ equation and ‘KPZ’ fixed point, and integrable probability, though referenced, are not much discussed.

Acknowledgements. These notes were begun for a topics course given in Spring 2012 at the University of Arizona, with input from research papers and texts, and revised during a 2026 sabbatical, supported in part by the Simons Foundation. They have also served as background for recent minicourses in Crete 2023 (Stochastic Methods in Finance and Physics IV), Rio 2024 (IMPA), and Hermosillo 2025 (XV Symposium on Probability and Stochastic Processes). Many thanks to the participants in these venues for their comments and interest.

Section 1 Preliminaries and hydrodynamics of independent random walks

Before discussing a basic example, illustrating possibilities in the study of ‘hydrodynamics of stochastic particle systems’, we recall some basic notions in Markov chains to set the stage.

1.1. Markov chains

1.1.1. Construction

A family of random variables {Xn:n0}\{X_{n}:n\geq 0\} taking values on a countable state space Ω\Omega is called a ‘discrete time Markov chain’ if the ‘stationary Markov property’ is satisfied:

P(Xn=xn|X0=x0,,Xm=xm)\displaystyle P(X_{n}=x_{n}|X_{0}=x_{0},\ldots,X_{m}=x_{m}) =\displaystyle= P(Xn=xn|Xm=xm)\displaystyle P(X_{n}=x_{n}|X_{m}=x_{m})
=\displaystyle= P(Xnm=xn|X0=xm)\displaystyle P(X_{n-m}=x_{n}|X_{0}=x_{m})

for all x0,,xmΩx_{0},\ldots,x_{m}\in\Omega and n>m0n>m\geq 0. When n=1n=1 and m=0m=0, the last quantity on the right-side represents a ‘transition probability’ of the Markov chain, denoted p(x,y)=P(X1=y|X0=x)p(x,y)=P(X_{1}=y|X_{0}=x). The nn-step probability p(n)(x,y)=P(Xn=y|X0=x)p^{(n)}(x,y)=P(X_{n}=y|X_{0}=x) satisfies a recurrence, p(n+1)(x,y)=zΩp(n)(x,z)p(z,y)p^{(n+1)}(x,y)=\sum_{z\in\Omega}p^{(n)}(x,z)p(z,y).

We now construct a ‘continuous time Markov chain’ on Ω\Omega with ‘skeleton’ {Xn:n0}\{X_{n}:n\geq 0\} and a transition probability vanishing on the diagonal, that is p(x,x)=0p(x,x)=0 for all xΩx\in\Omega. Let {λx:xΩ}\{\lambda_{x}:x\in\Omega\} be a collection of positive numbers, and let {Wn:n0}\{W_{n}:n\geq 0\} be a collection of independent identically distributed exponential random variables with rate 11, independent of the skeleton discrete time chain.

Define the process {Zt:t0}\{Z_{t}:t\geq 0\} as follows: Initially, Z0=X0ΩZ_{0}=X_{0}\in\Omega. After time λX01W0\lambda_{X_{0}}^{-1}W_{0}, the process jumps to value X1X_{1}, and after a subsequent time λX11W1\lambda_{X_{1}}^{-1}W_{1}, the process jumps to value X2X_{2}, and so on. Let Tk=i=0kλXi1WiT_{k}=\sum_{i=0}^{k}\lambda_{X_{i}}^{-1}W_{i} for k0k\geq 0. Then,

Zt={xfor 0t<T0X1forT0t<T1XnforTn1t<TnZ_{t}\ =\ \left\{\begin{array}[]{rl}x&\ {\rm for\ }0\leq t<T_{0}\\ X_{1}&\ {\rm for\ }T_{0}\leq t<T_{1}\\ \vdots&\ \ \vdots\\ X_{n}&\ {\rm for\ }T_{n-1}\leq t<T_{n}\\ \vdots&\ \ \vdots\end{array}\right.

where 0t<T=limnTn0\leq t<T_{\infty}=\lim_{n\uparrow\infty}T_{n}. Sufficient conditions for T=T_{\infty}=\infty include the cases that the state space Ω\Omega is finite, or that supxΩλx<\sup_{x\in\Omega}\lambda_{x}<\infty. We will assume from now on that the process is ‘regular’, that is T=T_{\infty}=\infty, so that the process ZtZ_{t} is defined for all time t0t\geq 0.

One can show that the ‘continuous time’ chain {Zt:t0}\{Z_{t}:t\geq 0\} satisfies the stationary Markov property, which in this context is equivalent to

P(Zt=y|Zt0=x0,,Ztm=xm,Zs=x)\displaystyle P(Z_{t}=y|Z_{t_{0}}=x_{0},\ldots,Z_{t_{m}}=x_{m},Z_{s}=x) =\displaystyle= P(Zt=y|Zs=x)\displaystyle P(Z_{t}=y|Z_{s}=x) (1.1.1)
=\displaystyle= P(Zts=y|Z0=x)\displaystyle P(Z_{t-s}=y|Z_{0}=x)

for all x,y,x0,,xmΩx,y,x_{0},\ldots,x_{m}\in\Omega, 0t0<tm<s<t0\leq t_{0}<\cdots t_{m}<s<t and m0m\geq 0.

Conversely, given a process {Zt:t0}\{Z_{t}:t\geq 0\} satisfying (1.1.1) and also the ‘jump property’ that there exists a sequence of strictly increasing stopping times {Tn:n0}\{T_{n}:n\geq 0\} such that T0>0=T1T_{0}>0=T_{-1} and ZtZ_{t} is constant on intervals [Tn,Tn+1)[T_{n},T_{n+1}) and ZTnZTnZ_{T_{n}^{-}}\neq Z_{T_{n}} for n0n\geq 0, one can determine a unique skeleton discrete time Markov chain {Xn:n0}\{X_{n}:n\geq 0\} and positive jump parameters {λx:xΩ}\{\lambda_{x}:x\in\Omega\} such that Xn=ZTnX_{n}=Z_{T_{n}}, p(x,y)=P(ZTn+1=y|ZTn=x)p(x,y)=P(Z_{T_{n+1}}=y|Z_{T_{n}}=x), and TnTn1|{Xn}n0T_{n}-T_{n-1}\big|\{X_{n}\}_{n\geq 0} are independent exponentials with rates λXn\lambda_{X_{n}} for n0n\geq 0. Chains with the same skeleton and jump parameters have the same joint distributions. The condition ZTnZTnZ_{T_{n}^{-}}\neq Z_{T_{n}} ensures pp vanishes on the diagonal.

1.1.2. Generators and Kolmogorov equations

In the discrete time setting, we can define the transition operator P=(p(x,y):x,yΩ)P=\big(p(x,y):x,y\in\Omega\big), which is a matrix when Ω\Omega is finite. Then, the nnth powers give the nnth step probabilities, Pn(x,y)=P(Xn=y|X0=x)P^{n}(x,y)=P(X_{n}=y|X_{0}=x).

Computing the tt-time probabilities for the continuous time Markov chain ZtZ_{t} is more complicated. Define the transition probability

Pt(x,y)=P(Zt=y|Z0=x).P_{t}(x,y)\ =\ P(Z_{t}=y|Z_{0}=x).

Then, by the Markov property we have

Pt+s(x,y)=zΩPt(x,z)Ps(z,y)P_{t+s}(x,y)\ =\ \sum_{z\in\Omega}P_{t}(x,z)P_{s}(z,y)

or in terms of operators Pt+s=PtPsP_{t+s}=P_{t}P_{s}, the semigroup property.

Given regularity of the process, the transition functions are differentiable in time, and satisfy the ‘first jump’ relation

Pt(x,y)\displaystyle P_{t}(x,y) =P(Zt=y,T0>t|Z0=x)+P(Zt=y,T0t|Z0=x)\displaystyle=P(Z_{t}=y,T_{0}>t|Z_{0}=x)+P(Z_{t}=y,T_{0}\leq t|Z_{0}=x)
=1(x=y)eλxt+0tλxeλxszxp(x,z)Pts(z,y),\displaystyle=1(x=y)e^{-\lambda_{x}t}+\int_{0}^{t}\lambda_{x}e^{-\lambda_{x}s}\sum_{z\neq x}p(x,z)P_{t-s}(z,y),

from which the backward equation is seen:

ddtPt(x,y)\displaystyle\frac{d}{dt}P_{t}(x,y) =\displaystyle= zΩλxp(x,z)[Pt(z,y)Pt(x,y)]\displaystyle\sum_{z\in\Omega}\lambda_{x}p(x,z)[P_{t}(z,y)-P_{t}(x,y)]
P0(x,y)\displaystyle P_{0}(x,y) =\displaystyle= 1(x=y).\displaystyle 1(x=y).

Similarly, from a decomposition of the jump time just before time tt, one has the forward equation

ddtPt(x,y)=zΩ[Pt(x,z)Pt(x,y)]λzp(z,y).\frac{d}{dt}P_{t}(x,y)\ =\ \sum_{z\in\Omega}[P_{t}(x,z)-P_{t}(x,y)]\lambda_{z}p(z,y).
Exercise 1.1.1.

Review and perform these derivations.

Define the operator

L(x,y)={λxp(x,y)foryxλxfory=x.L(x,y)\ =\ \left\{\begin{array}[]{rl}\lambda_{x}p(x,y)&\ {\rm for\ }y\neq x\\ -\lambda_{x}&\ {\rm for\ }y=x.\end{array}\right.

Then, neatly expressed, the backward and forward equations become

ddtPt=LPtandddtPt=PtL.\frac{d}{dt}P_{t}\ =\ LP_{t}\ \ \ {\rm and\ \ \ }\frac{d}{dt}P_{t}\ =\ P_{t}L.

Also, limt0t1[PtI]=L\lim_{t\downarrow 0}t^{-1}[P_{t}-I]=L and Pt(x,y)=δx,y+tL(x,y)+o(t)P_{t}(x,y)=\delta_{x,y}+tL(x,y)+o(t) as t0t\downarrow 0.

When the space Ω\Omega is finite, LL is a ‘generator’ matrix, that is L(x,y)0L(x,y)\geq 0 for xyx\neq y and L(x,x)=yxL(x,y)L(x,x)=-\sum_{y\neq x}L(x,y), and by solving the ODE’s, one obtains Pt=etLP_{t}=e^{tL} which can be computed in some cases. More generally, the semigroup PtP_{t} can be understood in terms of the Hille-Yosida formulation.

Let f:Ωf:\Omega\rightarrow\mathbb{R} be a bounded function on the state space. In the discrete time case, define Pf(x)=yΩp(x,y)f(y)Pf(x)=\sum_{y\in\Omega}p(x,y)f(y), which is the conditional expectation of f(X1)f(X_{1}) given X0=xX_{0}=x. Then, Pnf(x)=yΩp(n)(x,y)f(y)P^{n}f(x)=\sum_{y\in\Omega}p^{(n)}(x,y)f(y) is the conditional expectation of f(Xn)f(X_{n}) given X0=xX_{0}=x, where p(n)(x,y)p^{(n)}(x,y) is the nn-fold convolution, or nnth step transition probability.

In the continuous case, define Ptf(x)=yΩPt(x,y)f(y)P_{t}f(x)=\sum_{y\in\Omega}P_{t}(x,y)f(y) which is the conditional expectation of f(Zt)f(Z_{t}) given Z0=xZ_{0}=x. In this framework, the generator LL is often expressed in terms of its action on compactly supported ff:

(Lf)(x)\displaystyle(Lf)(x) =\displaystyle= yΩL(x,y)[f(y)f(x)]\displaystyle\sum_{y\in\Omega}L(x,y)[f(y)-f(x)]
=\displaystyle= yΩλxp(x,y)[f(y)f(x)].\displaystyle\sum_{y\in\Omega}\lambda_{x}p(x,y)[f(y)-f(x)].

1.1.3. Invariant measures

Let μ\mu be a probability measure on Ω\Omega. In the discrete time situation, define μP(x)=yΩμ(y)p(y,x)\mu P(x)=\sum_{y\in\Omega}\mu(y)p(y,x). Hence, we see that μPn\mu P^{n} is the distribution at time nn when the initial state is distributed according to μ\mu.

In the continuous-time model, define

μPt(x)=yΩμ(y)Pt(y,x),andμL(x)=yΩμ(y)L(y,x).\mu P_{t}(x)\ =\ \sum_{y\in\Omega}\mu(y)P_{t}(y,x),\ \ {\rm and}\ \ \mu L(x)\ =\ \sum_{y\in\Omega}\mu(y)L(y,x).

We say that μ\mu is an ‘invariant measure’ for discrete time chains if μP=μ\mu P=\mu, and for continuous time chains if μPt=μ\mu P_{t}=\mu for all t0t\geq 0. We also say that μ\mu is a ‘reversible’ invariant measure in discrete time chains if μ(x)p(x,y)=μ(y)p(y,x)\mu(x)p(x,y)=\mu(y)p(y,x) for all x,yΩx,y\in\Omega. In continuous time chains, μ\mu is ‘reversible’ when PtP_{t} is self-adjoint, that is xΩμ(x)f(x)Pt(x,y)g(y)=xΩμ(x)g(x)Pt(x,y)f(y)\sum_{x\in\Omega}\mu(x)f(x)P_{t}(x,y)g(y)=\sum_{x\in\Omega}\mu(x)g(x)P_{t}(x,y)f(y), or in terms of the inner product, f,Ptgμ=Ptf,gμ\langle f,P_{t}g\rangle_{\mu}=\langle P_{t}f,g\rangle_{\mu} for all compactly supported f,gf,g.

One can verify that in the continuous time setting that μ\mu being invariant is equivalent to μL=0\mu L=0 or in terms of expectations Eμ[Lf]=0E_{\mu}\big[Lf\big]=0 for all compactly supported ff. Also, μ\mu being reversible is equivalent to μ(x)L(x,y)=μ(y)L(y,x)\mu(x)L(x,y)=\mu(y)L(y,x) for all x,yΩx,y\in\Omega, or in terms of inner products f,Lgμ=Lf,gμ\langle f,Lg\rangle_{\mu}=\langle Lf,g\rangle_{\mu} for all compactly supported f,gf,g.

In the finite state space case, invariant measures always exist, and if the skeleton chain can reach every state from any state in finite time, that is pp is irreducible, the invariant measure is unique. However, in the countable state case there may be no invariant measures.

Reversibility has the following interesting implication. Fix a time t>0t>0, and consider Rs=ZtsR_{s}=Z_{t-s} for 0st0\leq s\leq t. Suppose that initially Z0Z_{0} is distributed according to an invariant measure μ\mu. Then, it can be seen that RsR_{s} is a continuous time Markov chain with transition probability Qs(x,y)=(μ(y)/μ(x))Ps(y,x)Q_{s}(x,y)=(\mu(y)/\mu(x))P_{s}(y,x). In particular, when μ\mu is reversible, Qs(x,y)=Ps(x,y)Q_{s}(x,y)=P_{s}(x,y) and in this case the ‘forward in time’ and ‘backward in time’ chains have the same distribution. We remark that it may be easier to find directly a reversible measure and therefore an invariant measure by checking the reversibility conditions.

1.1.4. Examples

We will content ourselves for the moment with two basic continuous time examples, the two-state Markov chain, and random walk.

Example 1.1.2.

Let Ω={0,1}\Omega=\{0,1\} correspond to states ‘on’ and ‘off’, or sometimes ‘empty’ and ‘occupied’. Here, state 00 can transition to state 11 and vice versa. Let λ0\lambda_{0} and λ1\lambda_{1} be the corresponding jump rates. The skeleton chain probabilities are p(0,1)=p(1,0)=1p(0,1)=p(1,0)=1. The generator matrix is

L=[λ0λ0λ1λ1].L\ =\ \left[\begin{array}[]{cc}-\lambda_{0}&\lambda_{0}\\ \lambda_{1}&-\lambda_{1}\end{array}\right].

and correspondingly, it is an exercise in diagonalization to compute Pt=etLP_{t}=e^{tL} and to find the unique invariant measure.

Exercise 1.1.3.

Compute the invariant measure and PtP_{t}. Is it reversible?

Example 1.1.4.

We define the Poisson process with parameter α\alpha. Let Ω=0:={0,1,2,}\Omega=\mathbb{N}_{0}:=\{0,1,2,\ldots\}, the whole numbers. Let λxα\lambda_{x}\equiv\alpha. The skeleton chain is deterministic where transitions are to the nearest right site: p(x,x+1)=1p(x,x+1)=1 for x0x\geq 0. Then, with Z0=0Z_{0}=0, the continuous time chain ZtZ_{t} counts the number steps made up to time t0t\geq 0. The trajectories are step functions, which are right-continuous, with left limits.

Exercise 1.1.5.

Compute the backward/forward equation, and show that the transition probability is in ‘Poisson’ form Pt(0,x)=Pt(y,y+x)=eαt(αt)x/x!P_{t}(0,x)=P_{t}(y,y+x)=e^{-\alpha t}(\alpha t)^{x}/x!.

Example 1.1.6.

Let Ω=𝕋Nd\Omega={\mathbb{T}}^{d}_{N} the dd-dimensional torus where 𝕋N=/N{\mathbb{T}}_{N}=\mathbb{Z}/N\mathbb{Z}, or integers modulo NN. Let also λx1\lambda_{x}\equiv 1, and pp be a finite-range, translation-invariant transition probability: For all x,yΩx,y\in\Omega, p(x,y)=0p(x,y)=0 if |xy|R|x-y|\geq R some R<R<\infty, and p(x,y)=p(0,yx)=:p(yx)p(x,y)=p(0,y-x)=:p(y-x). We will also assume that pp is irreducible. For instance, the nearest-neighbor, symmetric case is one possibility.

Then, L(x,y)=p(x,y)L(x,y)=p(x,y) for xyx\neq y and L(x,x)=yxL(x,y)L(x,x)=-\sum_{y\neq x}L(x,y). In particular, the uniform distribution μ(x)N1\mu(x)\equiv N^{-1} is the unique invariant measure. Moreover, μ\mu is reversible exactly when p(x)=p(x)p(x)=p(-x) for all xΩx\in\Omega.

Now let RtR_{t} be the number of jumps before time tt. Since the jump rates are all 11, we see that RtR_{t} is a Poisson process with rate 11. In particular, the transition probability satisfies

PtN(yx):=Pt(x,y)=E[p(Rt)(x,y)]=n0ettnn!p(n)(x,y).P^{N}_{t}(y-x):=P_{t}(x,y)\ =\ E\big[p^{(R_{t})}(x,y)\big]\ =\ \sum_{n\geq 0}\frac{e^{-t}t^{n}}{n!}p^{(n)}(x,y).

We now consider a sequence of chains Zt=Zt(N)Z_{t}=Z^{(N)}_{t} on a sequence of torii 𝕋Nd{\mathbb{T}}_{N}^{d} as N1N\geq 1 increases. Define m=xΩxp(x)m=\sum_{x\in\Omega}xp(x) to be the mean displacement of the position. Then, it is not difficult to extablish the following law of large numbers,

limNZNt(N)N=mtinprobability.\lim_{N\uparrow\infty}\frac{Z^{(N)}_{Nt}}{N}\ =\ mt\ \ \ {\rm in\ probability}.

Here, m𝕋dm\in{\mathbb{T}}^{d} where 𝕋{\mathbb{T}} is the unit circle.

Exercise 1.1.7.

Show this LLN (law of large numbes) by say variance computations. Noting RtR_{t} is Poisson with variance tt is useful. One can do it also by regeneration, and other methods.

Also, if m=0m=0, let CC be the matrix of covariances, Ci,j=xxixjp(x)C_{i,j}=\sum_{x}x_{i}x_{j}p(x) for 0i,jd0\leq i,j\leq d. We have the central limit theorem,

ZN2t(N)NN(0,Ct).\frac{Z^{(N)}_{N^{2}t}}{N}\ \Rightarrow\ {\rm N}(0,Ct).
Exercise 1.1.8.

There are a few ways to show this CLT (central limit theorem). One way is to compute the moment generating function or characteristic function, noting independence of Rt(N)R^{(N)}_{t} and the displacements.

Finally, when m=xxp(x)0m=\sum_{x}xp(x)\neq 0, we say the walk is asymmetric, and when m=0m=0 and p()p(\cdot) is not symmetric, we say the walk is mean-zero asymmetric, and when p()p(\cdot) is symmetric, we say the walk is symmetric.

1.2. Evolution of the mass of independent random walks

We would like to understand the space-time evolution of the mass in a system of particles with a conservation law. Perhaps the simplest model is that of unlabeled non-interacting random walks on a dd-dimensional torus with NN locations. When NN is large, and one looks at the system from afar, after long times, one can discern better the motion of the bulk of the mass rather than individual components. The goal is to make precise the evolution of the mass in this scale in terms of a continuum equation.

We will be working with a Markov chain on Ω=0𝕋Nd\Omega=\mathbb{N}_{0}^{{\mathbb{T}}^{d}_{N}}, where we recall 0={0,1,2,}\mathbb{N}_{0}=\{0,1,2,\ldots\}, which governs the motion of KK independent random walks on 𝕋Nd{\mathbb{T}}^{d}_{N} specified in Example 1.1.6. Since we are interested in the ‘mass’ of particles, we will consider the occupation numbers at each location on the lattice 𝕋Nd{\mathbb{T}}^{d}_{N}. That is, let ZtiZ^{i}_{t} be the position of the iith particle at time tt. Define

ηt(x)=i=1K1(Zti=x).\eta_{t}(x)\ =\ \sum_{i=1}^{K}1(Z^{i}_{t}=x).

We now observe that the process ηt={ηt(x):x𝕋Nd}\eta_{t}=\{\eta_{t}(x):x\in{\mathbb{T}}^{d}_{N}\} is a Markov chain. Indeed, given independence and the Markov property of the individual particle movement, by splitting over all possibilities, the Markov property of ηt\eta_{t} can be deduced.

Exercise 1.2.1.

Show this Markov property.

1.2.1. Invariant measures and distribution at time t0t\geq 0

What are the invariant measures for the process? Since the process ηt\eta_{t}, corresponding to KK particles, is irreducible, there is a unique invariant measure. It is not so easy to characterize it immediately.

Indeed, let us relax the assumption that there are KK particles in the system. If we do not specify the initial number of particles, then ηt\eta_{t} is no longer irreducible, since there is no birth or death possible: For instance, a system with 1010 particles cannot evolve to one with 2020 random walks. Nevertheless, we may specify in good form several invariant measures for this ‘relaxed’ reducible system.

Recall the Poisson distribution with parameter α\alpha: κα(k)=eααk/k!\kappa_{\alpha}(k)=e^{-\alpha}\alpha^{k}/k! for k0k\geq 0. Its moment generating function is given by

k0eλkeααkk!=eα(eλ1).\sum_{k\geq 0}e^{\lambda k}e^{-\alpha}\frac{\alpha^{k}}{k!}\ =\ e^{\alpha(e^{\lambda}-1)}.

For a nonnegative function ρ0:𝕋d+\rho_{0}:{\mathbb{T}}^{d}\rightarrow\mathbb{R}_{+}, define the product measure νρ0()N=x𝕋Ndκρ0(x/N)\nu^{N}_{\rho_{0}(\cdot)}=\prod_{x\in{\mathbb{T}}_{N}^{d}}\kappa_{\rho_{0}(x/N)} on 0𝕋Nd\mathbb{N}_{0}^{{\mathbb{T}}^{d}_{N}} so that the means

Eνρ()N[η(x)]=k0kκρ0(x/N)(k)=ρ0(x/N).E_{\nu^{N}_{\rho(\cdot)}}[\eta(x)]\ =\ \sum_{k\geq 0}k\kappa_{\rho_{0}(x/N)}(k)\ =\ \rho_{0}(x/N).

When ρ0()α\rho_{0}(\cdot)\equiv\alpha is constant, we denote ναN=νρ0()N\nu^{N}_{\alpha}=\nu^{N}_{\rho_{0}(\cdot)}.

The process {ηt:t0}\{\eta_{t}:t\geq 0\} belongs to the space D([0,),Ω)D([0,\infty),\Omega) of right-continuous paths with left limits in Ω=0𝕋Nd\Omega=\mathbb{N}_{0}^{{\mathbb{T}}^{d}_{N}}. We will denote by μ\mathbb{P}_{\mu} and 𝔼μ\mathbb{E}_{\mu} the probability measure and expectation with respect to the evolution of the process when initially η0\eta_{0} is distributed according to μ\mu. On the other hand, EμE_{\mu} refers to the expectation with respect to μ\mu on Ω\Omega.

Now, starting from νρ()N\nu^{N}_{\rho(\cdot)}, we observe that we may calculate the distribution at later times t>0t>0.

Proposition 1.2.2.

Under νρ0()N\mathbb{P}_{\nu^{N}_{\rho_{0}(\cdot)}}, the distribution of ηt\eta_{t} is the inhomogeneous product of Poisson measures x𝕋NdκψN,t(x)\prod_{x\in{\mathbb{T}}_{N}^{d}}\kappa_{\psi_{N,t}(x)} where ψN,t(x)=E[ρ0(N1(xZtN))]\psi_{N,t}(x)=E\big[\rho_{0}(N^{-1}(x-Z_{t}^{N}))\big] is the expectation with respect to the position of a random walk ZtNZ^{N}_{t} with rates p()p(\cdot) starting from the origin at time tt.

That the later time tt-distribution would still be a product measure is a feature of the independence of the particles–not a generic feature in more general interacting particle systems!

When ρ0α\rho_{0}\equiv\alpha is constant, we immediately arrive at the following characterization.

Corollary 1.2.3.

The measures ναN\nu^{N}_{\alpha} are invariant for the Markov chain ηt\eta_{t}.

Proof of Proposition 1.2.2. We need only compute the moment generating function of ηt\eta_{t}. Write

ηt(x)=y𝕋Ndk=1η0(y)1(Zty,k=x)\eta_{t}(x)\ =\ \sum_{y\in{\mathbb{T}}^{d}_{N}}\sum_{k=1}^{\eta_{0}(y)}1(Z^{y,k}_{t}=x)

and, for θ:𝕋Nd\theta:{\mathbb{T}}_{N}^{d}\rightarrow\mathbb{R},

x𝕋Ndθ(x)ηt(x)=x𝕋Ndy𝕋Ndk=1η0(y)θ(x)1(Zty,k=x)=y𝕋Ndk=1η0(y)θ(Zty,k)\sum_{x\in{\mathbb{T}}^{d}_{N}}\theta(x)\eta_{t}(x)\ =\ \sum_{x\in{\mathbb{T}}^{d}_{N}}\sum_{y\in{\mathbb{T}}^{d}_{N}}\sum_{k=1}^{\eta_{0}(y)}\theta(x)1(Z^{y,k}_{t}=x)\ =\ \sum_{y\in{\mathbb{T}}^{d}_{N}}\sum_{k=1}^{\eta_{0}(y)}\theta(Z^{y,k}_{t})

where Zty,kZ^{y,k}_{t} denotes the position at time tt of the kkth particle initially at location yy.

Since particles move independently, and initially there are a Poisson number of particles on each site of the lattice,

𝔼νρ0()N[expx𝕋Ndθ(x)ηt(x)]\displaystyle\mathbb{E}_{\nu^{N}_{\rho_{0}(\cdot)}}\Big[\exp\sum_{x\in{\mathbb{T}}^{d}_{N}}\theta(x)\eta_{t}(x)\Big] =\displaystyle= y𝕋Nd𝔼νρ0()N[expk=1η0(y)θ(Zty,k)]\displaystyle\prod_{y\in{\mathbb{T}}^{d}_{N}}\mathbb{E}_{\nu^{N}_{\rho_{0}(\cdot)}}\Big[\exp\sum_{k=1}^{\eta_{0}(y)}\theta(Z^{y,k}_{t})\Big]
=\displaystyle= y𝕋NdEνρ0()N(E[expθ(Zty,1)])η0(y)\displaystyle\prod_{y\in{\mathbb{T}}^{d}_{N}}E_{\nu^{N}_{\rho_{0}(\cdot)}}\Big(E\big[\exp\theta(Z^{y,1}_{t})\big]\Big)^{\eta_{0}(y)}
=\displaystyle= y𝕋Ndexp[ρ0(y/N)(E[eθ(y+Zt)]1)]\displaystyle\prod_{y\in{\mathbb{T}}^{d}_{N}}\exp\Big[\rho_{0}(y/N)\big(E\big[e^{\theta(y+Z_{t})}\big]-1\big)\Big]

where Zt=ZtNZ_{t}=Z_{t}^{N} is the position of a random walk on 𝕋Nd{\mathbb{T}}^{d}_{N} starting at the origin.

Now,

E[eθ(y+Zt)]=x𝕋NdPtN(xy)eθ(x)E\big[e^{\theta(y+Z_{t})}\big]\ =\ \sum_{x\in{\mathbb{T}}^{d}_{N}}P^{N}_{t}(x-y)e^{\theta(x)}

and

E[eθ(y+Zt)]1=x𝕋NdPtN(xy)(eθ(x)1).E\big[e^{\theta(y+Z_{t})}\big]-1\ =\ \sum_{x\in{\mathbb{T}}^{d}_{N}}P^{N}_{t}(x-y)(e^{\theta(x)}-1).

Hence, after a calculation,

𝔼νρ0()N[expx𝕋Ndθ(x)ηt(x)]\displaystyle\mathbb{E}_{\nu^{N}_{\rho_{0}(\cdot)}}\Big[\exp\sum_{x\in{\mathbb{T}}^{d}_{N}}\theta(x)\eta_{t}(x)\Big] =\displaystyle= expy𝕋Ndρ0(y/N)x𝕋NdPtN(xy)(eθ(x)1).\displaystyle\exp\sum_{y\in{\mathbb{T}}^{d}_{N}}\rho_{0}(y/N)\sum_{x\in{\mathbb{T}}^{d}_{N}}P^{N}_{t}(x-y)\big(e^{\theta(x)}-1\big).

Since

y𝕋NdPtN(xy)ρ0(y/N)\displaystyle\sum_{y\in{\mathbb{T}}^{d}_{N}}P^{N}_{t}(x-y)\rho_{0}(y/N) =\displaystyle= z𝕋NdPtN(z)ρ0(N1(xz))\displaystyle\sum_{z\in{\mathbb{T}}^{d}_{N}}P^{N}_{t}(z)\rho_{0}(N^{-1}(x-z))
=\displaystyle= E[ρ0(N1(xZtN))]=ψN,t(x),\displaystyle E\big[\rho_{0}\big(N^{-1}(x-Z^{N}_{t})\big)\big]\ =\ \psi_{N,t}(x),

the proof concludes. ∎

To come back to our initial question, we remark that the invariant measure ναN\nu^{N}_{\alpha} can be decomposed in terms of its restrictions to the sets ΩK={ηΩ:x𝕋Ndη(x)=K}\Omega_{K}=\{\eta\in\Omega:\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta(x)=K\} for K0K\geq 0. These are closed and irreducible for the motion. Then, each νN,K=ναN(|x𝕋Ndη(x)=K)\nu_{N,K}=\nu^{N}_{\alpha}(\cdot|\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta(x)=K) is the unique invariant measure on the restriction, and does not depend on α\alpha. In physics terminology, ναN\nu^{N}_{\alpha} is the ‘grand canonical’ measure and ν𝕋Nd,K\nu_{{\mathbb{T}}^{d}_{N},K} is the ‘canonical’ one.

Since the mean of η(x)\eta(x) under ναN\nu^{N}_{\alpha} equals α\alpha, it makes sense to call α\alpha the ‘mass density’ of the process. In this way, {ναN:α0}\{\nu^{N}_{\alpha}:\alpha\geq 0\} is a family of invariant measures indexed by density α\alpha.

When ρ0\rho_{0} is not constant, the measures νρ0()N\nu^{N}_{\rho_{0}(\cdot)} are examples of ‘local equilibrium’ measures, as near a continuity of point u𝕋du\in{\mathbb{T}}^{d} of ρ0()\rho_{0}(\cdot), they distribute particles near uN\lfloor uN\rfloor near that of the invariant measure νρ0(u)N\nu^{N}_{\rho_{0}(u)}. One may consider other non-product ‘local equilibrium’ and ‘nonequilibrium’ measures, but, as we have seen, these local equilibrium measures allow for some computations.

1.2.2. Hydrodynamics in mean-value

If we start with a local equilibrium measure νρ0()N\nu^{N}_{\rho_{0}(\cdot)}, then initially, the means {ρ0(x/N):x𝕋Nd}\{\rho_{0}(x/N):x\in{\mathbb{T}}_{N}^{d}\} are a discretization of the density ‘profile’ ρ0\rho_{0} defined on the continuous space 𝕋d{\mathbb{T}}^{d}. At a later time tt, the means have evolved to {ψN,t(x):x𝕋Nd}\{\psi_{N,t}(x):x\in{\mathbb{T}}_{N}^{d}\}. But, how to understand a macroscopic picture?

The answers depend on the particular time and space scales chosen in the problem. We will think of 𝕋Nd{\mathbb{T}}^{d}_{N} as embedded in 𝕋d{\mathbb{T}}^{d} where grid points on 𝕋Nd{\mathbb{T}}^{d}_{N} are separated by distance N1N^{-1}. In this way, a ‘macroscopic’ point uu on 𝕋d{\mathbb{T}}^{d} corresponds to the ‘microscopic’ point uN\lfloor uN\rfloor. As we will see, time should now be appropriately speeded up to see movement of the system. How fast this speed up should be will depend on the structure of the underlying jump probability p()p(\cdot).

When tt is fixed, one can see that N1ZtNN^{-1}Z^{N}_{t} converges weakly to 00. Hence, at a continuity point uu for ρ0()\rho_{0}(\cdot), we have limNψN,t(uN)=ρ0(u)\lim_{N\uparrow\infty}\psi_{N,t}(\lfloor uN\rfloor)=\rho_{0}(u). So, if we do not speed up time at all, the system does not move.

Asymmetric motions

In the asymmetric setting, let m=xp(x)0m=\sum xp(x)\neq 0. Since N1ZtNNmtN^{-1}Z^{N}_{tN}\rightarrow mt in probability, we have, for ϵ>0\epsilon>0,

limN|z/Nmt|ϵPtNN(z)=limNP[|ZNtNNmt|ϵ]= 1.\lim_{N\uparrow\infty}\sum_{|z/N-mt|\leq\epsilon}P^{N}_{tN}(z)\ =\ \lim_{N\uparrow\infty}P\Big[\Big|\frac{Z^{N}_{Nt}}{N}-mt\Big|\leq\epsilon\Big]\ =\ 1.

In this case, when the initial profile ρ0\rho_{0} is continuous,

limNψN,Nt(uN)=ρ0(umt):=ρ(t,u).\lim_{N\uparrow\infty}\psi_{N,Nt}(\lfloor uN\rfloor)\ =\ \rho_{0}(u-mt)\ :=\ \rho(t,u).

Therefore, if we speed up time by a factor of NN, we see that the density profile has translated by mtmt. In this sense NtNt is referred to as the ‘microscopic’ time, and tt as the ‘macroscopic’ time. Moreover, the density ρ(t,u)\rho(t,u) satisfies

tρ+mρ= 0.\partial_{t}\rho+m\cdot\nabla\rho\ =\ 0. (1.2.1)

This makes sense as individual particles displace an order NN microscopic locations at microscopic time NtNt.

Mean-zero motions

However, when m=0m=0, particles do not displace as much, but follow the ‘square root’ law, when say the underlying jump rates are finite-range. In other words, displacements are of order N\sqrt{N} at time NtNt, or alternatively of order NN at times N2tN^{2}t. The latter version fits in nicely with our space scaling of N1N^{-1}.

By the central limit theorem for random walks in this case, N1ZN2tNN(0,Ct)N^{-1}Z^{N}_{N^{2}t}\Rightarrow{\rm N}(0,Ct) and, when again ρ0\rho_{0} is continuous, we have

limNψN,N2t(Nu)\displaystyle\lim_{N\uparrow\infty}\psi_{N,N^{2}t}(\lfloor Nu\rfloor) =\displaystyle= limNz𝕋NdPN2tN(z)ρ0(N1(Nuz))\displaystyle\lim_{N\uparrow\infty}\sum_{z\in{\mathbb{T}}^{d}_{N}}P^{N}_{N^{2}t}(z)\rho_{0}\big(N^{-1}(\lfloor Nu\rfloor-z)\big)
=\displaystyle= limNE[ρ0(uN1ZN2tN)]=dρ¯0(x)Gt(ux)𝑑x.\displaystyle\lim_{N\uparrow\infty}E\Big[\rho_{0}(u-N^{-1}Z^{N}_{N^{2}t})\Big]\ =\ \int_{\mathbb{R}^{d}}\bar{\rho}_{0}(x)G_{t}(u-x)dx.

Here, ρ¯0\bar{\rho}_{0} is the periodic extension of ρ0\rho_{0} with period 𝕋d{\mathbb{T}}^{d}, and GtG_{t} is the Gaussian density with covariance CtCt. It follows that ρ(t,u):=dρ¯0(x)Gt(ux)𝑑x\rho(t,u):=\int_{\mathbb{R}^{d}}\bar{\rho}_{0}(x)G_{t}(u-x)dx, being a convolution with the ρ¯0\bar{\rho}_{0}, satisfies the heat equation on 𝕋d{\mathbb{T}}^{d}:

tρ\displaystyle\partial_{t}\rho =\displaystyle= Cρ:=1i,jdCi,jui,uj2ρ\displaystyle\triangle_{C}\rho:=\sum_{1\leq i,j\leq d}C_{i,j}\partial^{2}_{u_{i},u_{j}}\rho
ρ(0,u)\displaystyle\rho(0,u) =\displaystyle= ρ0(u).\displaystyle\rho_{0}(u). (1.2.2)

1.2.3. Conclusion

What we have done so far is to derive a macroscopic ‘hydrodynamic limit’ for the mean values over x𝕋Ndx\in{\mathbb{T}}_{N}^{d}. In the next Section 2, we will view the hydrodynamic limit as a full fledged law of large numbers of the empirical measure of particles. We also give some physical motivation for the name ‘hydrodynamics’.

We call the equations (1.2.1) and (1.2.2) and their solutions ρ(t,u)\rho(t,u) as ‘hydrodynamic’ equations and ‘hydrodynamic’ solutions for the space-time evolution of the macroscopic density. For independent particles, to summarize, we have proved the following:

Theorem 1.2.4.

Suppose ρ0:𝕋d+\rho_{0}:{\mathbb{T}}^{d}\rightarrow\mathbb{R}_{+} is continuous. Let v(N)=Nv(N)=N if m0m\neq 0 and v(N)=N2v(N)=N^{2} if m=0m=0. Then, starting from the sequence νρ0()N\nu^{N}_{\rho_{0}(\cdot)}, the density average ψN,v(N)t(Nu)\psi_{N,v(N)t}(\lfloor Nu\rfloor) at location Nu\lfloor Nu\rfloor and time v(N)tv(N)t converges to ρ(t,u)\rho(t,u) which solves equation (1.2.1) if m0m\neq 0 and equation (1.2.2) if m=0m=0.

1.3. Notes

The material on Markov chains is a standard treatment based on the development in [127], [178] and [130, Appendix 1]. The discussion on hydrodynamics of independent walks follows that in [130, Chapter 1] and [135]. See also [157] for a more general treatment. An early rigorous work on hydrodynamics of independent particle systems is [62].

Other work on invariant measures and hydrodynamics of systems of independent particles includes [122], [124], [146], [138], [166].

Section 2 Empirical measures, and a first look at hydrodynamics of exclusion processes

We introduce a notion of ‘hydrodynamics’ via empirical measures, which will be used in the analysis of more general interacting particle systems. Then, after a preliminary discussion of certain martingales in the Markov chain context, we discuss the hydrodynamics of exclusion processes. At the end, we comment on the physical motivation behind the name ‘hydrodynamics’.

2.1. Empirical measures and view of ‘hydrodynamics’ as a LLN

We may recast the derivation of ‘hydrodynamics’ in systems of independent random walks in terms of the random space-time scaled empirical distribution

πv(N)tN=1Ndx𝕋Ndηv(N)t(x)δx/N.\pi^{N}_{v(N)t}\ =\ \frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta_{v(N)t}(x)\delta_{x/N}.

Here, πv(N)tN\pi^{N}_{v(N)t} is a member of +(𝕋d){\mathcal{M}}_{+}({\mathbb{T}}^{d}), the nonnegative measures on 𝕋d{\mathbb{T}}^{d}. Recall our definition of the independent particle process in Section 1: We derived the distribution of the particle numbers ηv(N)t\eta_{v(N)t} at later times, starting from a local equilibrium measure νρ0()N\nu^{N}_{\rho_{0}(\cdot)}. However, it will be easier in what follows to consider the weaker notion of the asymptotic behavior of the empirical distribution. In this sense, what is meant by ‘hydrodynamics’ is a law of large numbers, characterizing ‘first-order’ behavior.

Let GG be a smooth, bounded function on 𝕋d{\mathbb{T}}^{d}, and write

G,πv(N)tN:=1Ndx𝕋NdG(x/N)ηv(N)t(x).\langle G,\pi^{N}_{v(N)t}\rangle\ :=\ \frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}G(x/N)\eta_{v(N)t}(x). (2.1.1)

Here, the pairing F,π\langle F,\pi\rangle is another way to write the expectation Eπ[G]E_{\pi}[G]. Recall, from Section 1, the distribution of ηv(N)t\eta_{v(N)t} starting from νρ0()N\nu^{N}_{\rho_{0}(\cdot)} is a product of Poisson measures with intensity ψN,v(N)t()=E[ρ0(N1(xZv(N)tN))]\psi_{N,v(N)t}(\cdot)=E\big[\rho_{0}\big(N^{-1}(x-Z^{N}_{v(N)t})\big)\big], where the expectation is with respect to the random walk ZNZ^{N}_{\cdot}. Then, in mean-value, starting in νρ0()N\nu^{N}_{\rho_{0}(\cdot)}, we have

𝔼νρ0()N[1Ndx𝕋NdG(x/N)ηv(N)t(x)]=1Ndx𝕋NdG(x/N)𝔼νρ0()N[ηv(N)t(x)]\displaystyle\mathbb{E}_{\nu^{N}_{\rho_{0}(\cdot)}}\Big[\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}G(x/N)\eta_{v(N)t}(x)\Big]=\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}G(x/N)\mathbb{E}_{\nu^{N}_{\rho_{0}(\cdot)}}[\eta_{v(N)t}(x)]
=1Ndx𝕋NdG(x/N)E[ρ0(N1(xZv(N)t))].\displaystyle\ \ \ \ \ \ \ \ \ \ \ \ \ =\ \frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}G(x/N)E\big[\rho_{0}\big(N^{-1}(x-Z_{v(N)t})\big)\big].

Depending on whether m0m\neq 0 or m=0m=0, in which case v(N)=Nv(N)=N or v(N)=N2v(N)=N^{2}, the last quantity as before tends respectively to

ρ0(umt)G(u)𝑑uorG(u)ρ¯0(w)Gt(uw)𝑑w𝑑u.\int\rho_{0}(u-mt)G(u)du\ \ {\rm or\ \ }\int G(u)\int\bar{\rho}_{0}(w)G_{t}(u-w)dwdu. (2.1.2)

However, the variance of (2.1.1), when starting in νρ0()N\nu^{N}_{\rho_{0}(\cdot)}, since the occupation numbers ηv(N)t\eta_{v(N)t} are independent Poisson variables with intensities {ψN,v(N)t(x):x𝕋Nd}\{\psi_{N,v(N)t}(x):x\in{\mathbb{T}}_{N}^{d}\}, vanishes:

Var[1Ndx𝕋NdG(x/N)ηv(N)t(x)]\displaystyle{\rm Var}\Big[\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}G(x/N)\eta_{v(N)t}(x)\Big] =\displaystyle= 1N2dx𝕋NdG2(x/N)ψN,v(N)t(x)\displaystyle\frac{1}{N^{2d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}G^{2}(x/N)\psi_{N,v(N)t}(x)
=\displaystyle= O(Nd) 0,\displaystyle O(N^{-d})\ \rightarrow\ 0,

as GG and ρ0\rho_{0} are bounded. Hence, G,πv(N)tN\langle G,\pi^{N}_{v(N)t}\rangle converges variously to the expressions in (2.1.2) in probability, depending on the drift mm.

In particular, we have shown, with respect to the initial distribution μN\mu^{N} for the process η0\eta_{0}, the empirical measure πv(N)tN\pi^{N}_{v(N)t}, a random element of +(𝕋d)\mathcal{M}_{+}({\mathbb{T}}^{d}), converges in probability to the deterministic measure ρ(t,u)du\rho(t,u)du corresponding to the macroscopic space-time mass evolution.

Here, the topology on +(𝕋d)\mathcal{M}_{+}({\mathbb{T}}^{d}) used is as follows: Consider C(𝕋d)C({\mathbb{T}}^{d}), the space of real continuous functions on 𝕋d{\mathbb{T}}^{d} endowed with the sup-metric. Let {fk:k1}\{f_{k}:k\geq 1\} be a dense, countable family of continuous functions in C(𝕋d)C({\mathbb{T}}^{d}). Then, define the distance δ(μ,ν)\delta(\mu,\nu) on +(𝕋d)\mathcal{M}_{+}({\mathbb{T}}^{d}) by

δ(μ,ν)=k=112k|μ,fkν,fk|1+|μ,fkν,fk|.\delta(\mu,\nu)\ =\ \sum_{k=1}^{\infty}\frac{1}{2^{k}}\frac{|\langle\mu,f_{k}\rangle-\langle\nu,f_{k}\rangle|}{1+|\langle\mu,f_{k}\rangle-\langle\nu,f_{k}\rangle|}.

Therefore, capturing the limit behavior of G,πv(N)tN\langle G,\pi^{N}_{v(N)t}\rangle for each continuous function GG is enough to compute the limits of πv(N)tN\pi^{N}_{v(N)t}.

2.2. Exclusion processes

The exclusion process is one of the ‘canonical’ interacting particle systems, introduced in [205]. Consider particles on 𝕋Nd{\mathbb{T}}^{d}_{N} with the minimal interaction that no particle can jump onto another. Accordingly, a configuration of occupation numbers ηt\eta_{t} belongs to the finite state space Ω={0,1}𝕋Nd\Omega=\{0,1\}^{{\mathbb{T}}^{d}_{N}} where ηt(x)=0\eta_{t}(x)=0 or 11 depending on whether x𝕋Ndx\in{\mathbb{T}}^{d}_{N} is empty or occupied at time t0t\geq 0. Informally, ηt\eta_{t} updates in that each particle is a continuous time random walk carrying an exponential 11 clock. When a clock rings, the particle tries to move with skeleton jump probability pp. However, if the site chosen is already occupied, the jump is suppressed, and all clocks reset. We will restrict attention to jump probabilities pp which are tranlsation-invariant: p(x,y)=p(yx)p(x,y)=p(y-x).

More formally, infinitesimally ηt\eta_{t} can change to ηtx,x+y\eta_{t}^{x,x+y} when a particle at xx displaces by increment yy where

ηa,b(z)={η(b)whenz=aη(a)whenz=bη(z)whenzx,y\eta^{a,b}(z)\ =\ \left\{\begin{array}[]{rl}\eta(b)&\ {\rm when\ }z=a\\ \eta(a)&\ {\rm when\ }z=b\\ \eta(z)&\ {\rm when\ }z\neq x,y\end{array}\right.

with rate η(x)(1η(x+y))p(y)\eta(x)(1-\eta(x+y))p(y). The ‘exclusion’ factor ‘η(x)(1η(x+y))\eta(x)(1-\eta(x+y))’ is 11 exactly when xx is occupied and the destination x+yx+y is unoccupied; otherwise, it is 00. The generator of the process ηt\eta_{t} is given by

(Lf)(η)=x𝕋Ndy𝕋Ndη(x)(1η(x+y))p(y)[f(ηx,x+y)f(η)]\displaystyle(Lf)(\eta)\ =\ \sum_{x\in{\mathbb{T}}^{d}_{N}}\sum_{y\in{\mathbb{T}}^{d}_{N}}\eta(x)(1-\eta(x+y))p(y)\big[f(\eta^{x,x+y})-f(\eta)\big] (2.2.1)

for functions f:Ωf:\Omega\rightarrow\mathbb{R}.

In the following, we will also assume that pp is finite-range, that is p(z)=0p(z)=0 for |z|>R|z|>R for some RR. Of course, a case is when pp is nearest-neighbor, that is when the range R=1R=1.

When pp is symmetric, the process is called the ‘symmetric simple exclusion process’. When pp is asymmetric, ηt\eta_{t} is termed the ‘asymmetric exclusion process’. When the range R=1R=1, the label ‘simple’ is sometimes added to the names.

There is a simplification of the form of LL when pp is symmetric. Namely, since ηx,x+y=ηx+y,x\eta^{x,x+y}=\eta^{x+y,x} and p(y)=p(y)p(y)=p(-y), we have

(Lf)(η)\displaystyle(Lf)(\eta) =\displaystyle= 12x𝕋Ndy𝕋Nd{η(x)(1η(x+y))+η(x+y)(1η(x))}p(y)\displaystyle\frac{1}{2}\sum_{x\in{\mathbb{T}}^{d}_{N}}\sum_{y\in{\mathbb{T}}^{d}_{N}}\big\{\eta(x)(1-\eta(x+y))+\eta(x+y)(1-\eta(x))\big\}p(y) (2.2.2)
×[f(ηx,x+y)f(η)]\displaystyle\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \times\big[f(\eta^{x,x+y})-f(\eta)\big]
=\displaystyle= 12x𝕋Ndy𝕋Ndp(y)[f(ηx,x+y)f(η)].\displaystyle\frac{1}{2}\sum_{x\in{\mathbb{T}}^{d}_{N}}\sum_{y\in{\mathbb{T}}^{d}_{N}}p(y)\big[f(\eta^{x,x+y})-f(\eta)\big].

The last line follows as the term in curly braces equals |η(x)η(x+y)|=1|\eta(x)-\eta(x+y)|=1 exactly when the difference in square brackets vanishes.

Let ναN=x𝕋NdBern(α)\nu^{N}_{\alpha}=\prod_{x\in{\mathbb{T}}_{N}^{d}}{\rm Bern}(\alpha) be the product measure on 𝕋Nd{\mathbb{T}}^{d}_{N} with Bernoulli marginals with success probability α\alpha. Recall from Subsection 1.1.3 that EμE_{\mu} stands for the expectation under μ\mu, and μ\mathbb{P}_{\mu} and 𝔼μ\mathbb{E}_{\mu} for the process measure and expectation when starting in μ\mu.

Proposition 2.2.1.

The measures {ναN:0α1}\{\nu^{N}_{\alpha}:0\leq\alpha\leq 1\} are invariant measures for ηt\eta_{t}, for both symmetric and asymmetric pp. In the symmetric case, ναN\nu^{N}_{\alpha} is also reversible.

Proof.

First note that f(ηx,x+y)f(η)f(\eta^{x,x+y})-f(\eta) vanishes if η(x)=η(x+y)\eta(x)=\eta(x+y). Hence, we may write

(Lf)(η)=x𝕋Ndy𝕋Ndη(x)p(y)[f(ηx,x+y)f(η)],(Lf)(\eta)\ =\ \sum_{x\in{\mathbb{T}}^{d}_{N}}\sum_{y\in{\mathbb{T}}^{d}_{N}}\eta(x)p(y)\big[f(\eta^{x,x+y})-f(\eta)\big],

where we dropped the factor ‘1η(x+y)1-\eta(x+y)’.

Note also, under the change of measure ζ=ηx,y\zeta=\eta^{x,y}, which exchanges values η(x)\eta(x) and η(y)\eta(y), the measure ναN\nu^{N}_{\alpha} remains the same. Hence, for functions f,hf,h, the term

EναN[h(η)η(x)(1η(x+y))p(y)f(ηx,x+y)]\displaystyle E_{\nu^{N}_{\alpha}}\big[h(\eta)\eta(x)(1-\eta(x+y))p(y)f(\eta^{x,x+y})\big]
=EναN[h(ηx,x+y)η(x+y)(1η(x))p(y)f(η)].\displaystyle\ \ \ \ \ \ \ =\ E_{\nu^{N}_{\alpha}}\big[h(\eta^{x,x+y})\eta(x+y)(1-\eta(x))p(y)f(\eta)].

Then, by collecting terms, with simple manipulation,

EναN[hLf]=EναN[(Lh)f],E_{\nu^{N}_{\alpha}}\big[hLf\big]\ =\ E_{\nu^{N}_{\alpha}}\big[(L^{*}h)f\big],

where the ναN\nu^{N}_{\alpha}-adjoint LL^{*} is seen as the exclusion generator with single particle jump probability q(z)=p(z)q(z)=p(-z).

Now, since L1=0L^{*}1=0, by inspection, we have that EναN[Lf]=0E_{\nu^{N}_{\alpha}}[Lf]=0 for all ff. This shows ναN\nu^{N}_{\alpha} is invariant.

Moreover, as L=LL^{*}=L when pp is symmetric, ναN\nu^{N}_{\alpha} is reversible. ∎

From this result, we can deduce when there are exactly KK particles in the system that ναN(|x𝕋Ndη(x)=K)\nu_{\alpha}^{N}(\cdot|\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta(x)=K) is the unique ‘canonical’ invariant measure for the motion on ΩK={η:x𝕋Ndη(x)=K}\Omega_{K}=\big\{\eta:\sum_{x\in{\mathbb{T}}_{N}^{d}}\eta(x)=K\big\}.

Exercise 2.2.2 (Duality).

Suppose pp is symmetric. Show that the space of linear combinations of occupation variables η(x)\eta(x) for x𝕋dNx\in{\mathbb{T}}^{N}_{d} remains invariant under action by generator LL. In fact, the space of linear combinations of j=1nη(xj)\prod_{j=1}^{n}\eta(x_{j}) for {xjdN:1jn}\{x_{j}\in\mathbb{R}^{N}_{d}:1\leq j\leq n\} is closed. We comment that this property is sometimes referred to as ‘duality’. Hint: A case of the property is straightforwardly seen by computing the action on the variable η(x)\eta(x).

2.3. Martingales and Markov chains

Recall that a martingale MtM_{t} corresponding to sigma-fields t\mathcal{F}_{t} is a random process, adapted to the filtration {t}\{\mathcal{F}_{t}\}, which satisfies

E[Mt|s]=MsandE|Mt|<E[M_{t}|\mathcal{F}_{s}]\ =\ M_{s}\ \ {\rm and\ \ }E|M_{t}|<\infty

for all ts0t\geq s\geq 0.

Exercise 2.3.1.

Let N(t)N(t) be a Poisson process with rate λ\lambda. Then, Mt=N(t)λtM_{t}=N(t)-\lambda t is a martingale with respect to the ‘natural’ sigma-fields t=σ{Nu:ut}\mathcal{F}_{t}=\sigma\{N_{u}:u\leq t\}. Also, Qt=Mt2λtQ_{t}=M^{2}_{t}-\lambda t is also a martingale with respect to {t}\{\mathcal{F}_{t}\}.

Let XtX_{t} be a Markov process on a countable state space Ω\Omega. Let F:+×ΩF:\mathbb{R}_{+}\times\Omega\rightarrow\mathbb{R} be a twice continuously differentiable function whose first and second partial time derivatives are uniformly bounded. Define

MtF\displaystyle M^{F}_{t} =\displaystyle= F(t,Xt)F(0,X0)0t(s+L)F(s,Xs)ds\displaystyle F(t,X_{t})-F(0,X_{0})-\int_{0}^{t}\Big(\partial_{s}+L\Big)F(s,X_{s})ds
NtF\displaystyle N^{F}_{t} =\displaystyle= (MtF)20t[(LF2)(s,Xs)2F(s,Xs)(LF)(s,Xs)]𝑑s.\displaystyle(M^{F}_{t})^{2}-\int_{0}^{t}\Big[(LF^{2})(s,X_{s})-2F(s,X_{s})(LF)(s,X_{s})\Big]ds.

These two processes, which we show below are martingales, will be very useful in our stochastic analysis of Markov systems. The term,

MFt=0t[(LF2)(s,Xs)2F(s,Xs)(LF)(s,Xs)]𝑑s\langle M^{F}\rangle_{t}\ =\ \int_{0}^{t}\Big[(LF^{2})(s,X_{s})-2F(s,X_{s})(LF)(s,X_{s})\Big]ds

is the ‘(predictable) quadratic variation’ of the martingale MtFM^{F}_{t}.

Proposition 2.3.2.

With respect to natural sigma-fields t=σ{Xu:ut}\mathcal{F}_{t}=\sigma\{X_{u}:u\leq t\}, both MtFM^{F}_{t} and NtFN^{F}_{t} are martingales.

Proof.

We will show that MtFM^{F}_{t} is a martingale when FF does not depend on time. Generalizations and verification of NtFN^{F}_{t} as a martingale are left to the reader. We need only show that

E[F(Xt)|s]F(Xs)stE[(LF)(Xu)|s]𝑑u= 0.E\big[F(X_{t})|\mathcal{F}_{s}\big]-F(X_{s})-\int_{s}^{t}E\big[(LF)(X_{u})|\mathcal{F}_{s}\big]du\ =\ 0.

Now, E[F(Xt)|s]=PtsF(Xs)E[F(X_{t})|\mathcal{F}_{s}]=P_{t-s}F(X_{s}) and E[(LF)(Xu)|s]=Pus(LF)(Xs)E[(LF)(X_{u})|\mathcal{F}_{s}]=P_{u-s}(LF)(X_{s}) from the Markov property. From the forward equation, the derivative of the left-side of the above display in tt equals

Pts(LF)(Xs)Pts(LF)(Xs)= 0.P_{t-s}(LF)(X_{s})-P_{t-s}(LF)(X_{s})\ =\ 0.

At time t=st=s, the left-side also vanishes. This concludes the proof. ∎

Exercise 2.3.3.

Complete the proof of Proposition 2.3.2. Hint: With respect to MtFM^{F}_{t}, we need to show

E[F(t,Xt)|s]F(s,Xs)=stE[(s+L)F(u,Xu)|s]ds.E\big[F(t,X_{t})|\mathcal{F}_{s}\big]-F(s,X_{s})=\int_{s}^{t}E\Big[\big(\partial_{s}+L\big)F(u,X_{u})\Big|\mathcal{F}_{s}\Big]ds.

When t=st=s, the relation holds. Hence, if one shows the derivatives with respect to tt match, that is

tE[F(t,Xt)|s]=Pts(tF)(t,x)|x=Xs+Pts(LF)(t,x)|x=Xs.\partial_{t}E\big[F(t,X_{t})|\mathcal{F}_{s}\big]=P_{t-s}\big(\partial_{t}F\big)(t,x)|_{x=X_{s}}+P_{t-s}(LF)(t,x)|_{x=X_{s}}.

2.4. Sketch of hydrodynamics for exclusion processes

Let ρ0:𝕋d+\rho_{0}:{\mathbb{T}}^{d}\rightarrow\mathbb{R}_{+} be a continuous function. We will denote by νρ0()N=x𝕋NdBern(ρ0(x/N))\nu^{N}_{\rho_{0}(\cdot)}=\prod_{x\in{\mathbb{T}}_{N}^{d}}{\rm Bern}(\rho_{0}(x/N)) the product measure with Bernoulli marginal at site x𝕋Ndx\in{\mathbb{T}}_{N}^{d} with success probability ρ0(x/N)\rho_{0}(x/N).

Our goal is to analyze the asymptotic behavior of the empirical measure with respect simple exclusion process ηt\eta_{t},

πv(N)tN=1Ndx𝕋Ndηt(x)δx/N,\pi^{N}_{v(N)t}\ =\ \frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta_{t}(x)\delta_{x/N},

in a time scale v(N)v(N) to be chosen later. We will start the process from local equilibrium measures μN=νρ0()N\mu^{N}=\nu^{N}_{\rho_{0}(\cdot)}.

In general, one doesn’t expect {ηv(N)t(x):x𝕋Nd}\{\eta_{v(N)t}(x):x\in{\mathbb{T}}_{N}^{d}\} to consist of independent random variables, even if initially at t=0t=0 they are independent. Instead of computing the mean and variance, as with independent particles, we will use the martingale formulation.

To understand main ideas, let G:𝕋dG:{\mathbb{T}}^{d}\rightarrow\mathbb{R} be a smooth function, not depending on time. Treating

G,πv(N)tN=1Ndx𝕋NdG(x/N)ηv(N)t(x)\langle G,\pi^{N}_{v(N)t}\rangle\ =\ \frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}G(x/N)\eta_{v(N)t}(x)

as a function FF of the Markov process ηv(N)t\eta_{v(N)t} on the state space Ω\Omega, we obtain a microscopic evolution equation:

G,πv(N)tN=G,π0N+0v(N)tLG,πsN𝑑s+MtN(G)\langle G,\pi^{N}_{v(N)t}\rangle\ =\ \langle G,\pi^{N}_{0}\rangle+\int_{0}^{v(N)t}L\langle G,\pi^{N}_{s}\rangle ds+M^{N}_{t}(G)

where MtN(G)M^{N}_{t}(G) is a martingale (cf. Proposition 2.3.2) with quadratic variation

MN(G)t=0v(N)t[L(G,πsN)22G,πsN(LG,πsN)]𝑑s.\langle M^{N}(G)\rangle_{t}\ =\ \int_{0}^{v(N)t}\Big[L\big(\langle G,\pi^{N}_{s}\rangle\big)^{2}-2\langle G,\pi^{N}_{s}\rangle\big(L\langle G,\pi^{N}_{s}\rangle\big)\Big]ds.

Now, the martingale is negligible in the NN\uparrow\infty limit: We compute that

𝔼μN[(MtN(G))2]\displaystyle\mathbb{E}_{\mu^{N}}\big[(M^{N}_{t}(G))^{2}\big] (2.4.1)
=0v(N)t1N2(d+1)x,y𝕋Nd(x,x+yNG)2p(y)ηs(x)(1ηs(x+y))𝑑s\displaystyle\ \ \ \ \ \ =\int_{0}^{v(N)t}\frac{1}{N^{2(d+1)}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}\big(\nabla^{N}_{x,x+y}G\big)^{2}p(y)\eta_{s}(x)(1-\eta_{s}(x+y))ds
v(N)tN2(d+1)x,y𝕋Nd(x,x+yNG)2p(y)=O(v(N)Nd2).\displaystyle\ \ \ \ \ \ \leq\frac{v(N)t}{N^{2(d+1)}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}\big(\nabla^{N}_{x,x+y}G\big)^{2}p(y)\ =\ O(v(N)N^{-d-2}).

In the last line, we have used that the occupation variables are bounded by 11 and that the jump probabilities are finite-range.

A calculation shows that

LG,πsN\displaystyle L\langle G,\pi^{N}_{s}\rangle (2.4.2)
=1Nd+1x,y𝕋Ndηs(x)(1ηs(x+y))p(y)[x+y,xNG(ηs(x)ηs(x+y))]\displaystyle\ \ \ \ \ \ \ =\frac{1}{N^{d+1}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}\eta_{s}(x)(1-\eta_{s}(x+y))p(y)\big[\nabla^{N}_{x+y,x}G\cdot(\eta_{s}(x)-\eta_{s}(x+y))\big]
=1Nd+1x,y𝕋Ndηs(x)(1ηs(x+y))p(y)[x+y,xNG]\displaystyle\ \ \ \ \ \ \ =\frac{1}{N^{d+1}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}\eta_{s}(x)(1-\eta_{s}(x+y))p(y)\big[\nabla^{N}_{x+y,x}G\big]

where u,vNG=N[G(u/N)G(v/N)](uv)G(v/N)\nabla^{N}_{u,v}G=N[G(u/N)-G(v/N)]\sim(u-v)\cdot\nabla G(v/N).

Exercise 2.4.1.

Verify the derivation of the quadratic variation given in (2.4.1).

2.4.1. Symmetric case.

When pp is symmetric, recalling the simpler form of the generator (2.2.2), a further summation by parts is possible and we obtain

LG,πsN\displaystyle L\langle G,\pi^{N}_{s}\rangle =\displaystyle= 12Nd+1x,y𝕋Nd[ηs(x)ηs(x+y)]p(y)x+y,xNG\displaystyle\frac{1}{2N^{d+1}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}\big[\eta_{s}(x)-\eta_{s}(x+y)\big]p(y)\nabla^{N}_{x+y,x}G
=\displaystyle= 12Nd+2x,y𝕋Ndp(y)ηs(x)x,yNG\displaystyle\frac{1}{2N^{d+2}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}p(y)\eta_{s}(x)\triangle^{N}_{x,y}G

where x,yNG=N2[G(x+y/N)2G(x/N)+G(xy/N)]\triangle^{N}_{x,y}G=N^{2}[G(x+y/N)-2G(x/N)+G(x-y/N)].

Now, yp(y)x,yNG=CG(x/N)+o(1)\sum_{y}p(y)\triangle^{N}_{x,y}G=\triangle_{C}G(x/N)+o(1) where we recall

C=1i,jdCi,jxi,xj2,andcovariancesCi,j=z𝕋Ndzizjp(z).\triangle_{C}\ =\ \sum_{1\leq i,j\leq d}C_{i,j}\partial^{2}_{x_{i},x_{j}},\ \ {\rm and\ covariances\ }C_{i,j}\ =\ \sum_{z\in{\mathbb{T}}^{d}_{N}}z_{i}z_{j}p(z).

Hence, if v(N)=N2v(N)=N^{2}, we have that

G,πv(N)tN=G,π0N+12N20v(N)tCG,πsN𝑑s+MtN(G)+o(1).\langle G,\pi^{N}_{v(N)t}\rangle\ =\ \langle G,\pi^{N}_{0}\rangle+\frac{1}{2N^{2}}\int_{0}^{v(N)t}\langle\triangle_{C}G,\pi^{N}_{s}\rangle ds+M^{N}_{t}(G)+o(1).

Putting these estimates together, along with (2.4.1), for symmetric pp, we have ‘closed’ the equation:

G,πv(N)tN=G,π0N+120tCG,πv(N)sN𝑑s+o(1).\langle G,\pi^{N}_{v(N)t}\rangle\ =\ \langle G,\pi^{N}_{0}\rangle+\frac{1}{2}\int_{0}^{t}\langle\triangle_{C}G,\pi^{N}_{v(N)s}\rangle ds+o(1).

This suggests in the NN\uparrow\infty limit that the empirical measures πN2tN\pi^{N}_{N^{2}t} converge in the weak sense to a solution of the heat equation

tρ=12Cρ.\partial_{t}\rho=\frac{1}{2}\triangle_{C}\rho.

The goal of Chapter 3 is to make precise this statement for symmetric simple exclusion.

The reader will have noticed that the above display is virtually the same equation derived for independent particles. This is due to the definition of the empirical measure πtN\pi^{N}_{t}, which uses the occupation variables η(x)\eta(x) as the masses at locations x/Nx/N. The ‘duality’ property of such functions with respect to symmetric exclusion mentioned earlier (cf. Exercise 2.2.2) allows to recover the heat equation. There are differences however in the associated fluctuations, for instance as seen in Sections 11, and 12 (specialized to independent particles).

2.4.2. Drift case.

When pp is asymmetric, say m=zzp(z)0m=\sum_{z}zp(z)\neq 0, as in the independent particle model, we should choose v(N)=Nv(N)=N. But, one cannot ‘close’ the equation. One has to deal with the term

NNd+1x,y𝕋Ndηs(x)(1ηs(x+y))p(y)[x+y,xNG]\frac{N}{N^{d+1}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}\eta_{s}(x)(1-\eta_{s}(x+y))p(y)\big[\nabla^{N}_{x+y,x}G\big]

composed of ‘two-point’ functions η(x)η(x+y)\eta(x)\eta(x+y). In the limit, such a term due to ‘local averaging’ should be replaced by a quadratic function of the empirical density.

Formally, one would obtain a form of Burger’s equation

t+mρ(1ρ)= 0.\partial_{t}+m\cdot\nabla\rho(1-\rho)\ =\ 0.

There is much work on such hyperbolic mass conservation laws. In particular, there may be several solutions even starting from smooth initial data. It will turn out that the solution found by hydrodynamics is the unique ‘entropy’ or ‘vanishing viscosity’ solution. We will discuss the m0m\neq 0 case in the context of ‘TASEP’, that is in totally asymmetric simple exclusion setting in d=1d=1 when p(1)=1p(1)=1 and p(j)=0p(j)=0f or j1j\neq 1 in Section 6.

2.4.3. Asymmetric, mean-zero case.

In the final case when pp is asymmetric, but mean-zero, that is p(z)p(z)p(z)\neq p(-z) for some zz, but zzp(z)=0\sum_{z}zp(z)=0, there are other complications. The system is referred to as a ‘non-gradient’ model. Although, we should speed up time by v(N)=N2v(N)=N^{2}, a second summation-by-parts as in the symmetric situation cannot be done. Indeed, multiplying (2.4.2) by N2N^{2}, we have

N22Nd+1x𝕋NdG(x/N)\displaystyle\frac{N^{2}}{2N^{d+1}}\sum_{x\in{\mathbb{T}}^{d}_{N}}\nabla G(x/N)
y𝕋Nd{ηs(x)(1ηs(x+y))yp(y)ηs(x+y)(1ηs(x))yp(y)}.\displaystyle\ \ \ \ \ \ \cdot\sum_{y\in{\mathbb{T}}_{N}^{d}}\big\{\eta_{s}(x)(1-\eta_{s}(x+y))yp(y)-\eta_{s}(x+y)(1-\eta_{s}(x))yp(-y)\big\}.

Unless pp is symmetric, one cannot rewrite the expression in curly braces as the exact difference of a function ff and its translate.

Let {ei}i=1d\{e_{i}\}_{i=1}^{d} be the standard basis in d\mathbb{Z}^{d}. It can be shown that the sum over yy dotted with eie_{i} can be approximated by a difference j=1dai,j(η(x))ai,j(η(x+ej))\sum_{j=1}^{d}a_{i,j}(\eta(x))-a_{i,j}(\eta(x+e_{j})), a ‘gradient’. The function ai,ja_{i,j} depends on pp. With respect to a certain ’homogenization’ a¯i,j\bar{a}_{i,j} of ai,ja_{i,j}, the hydrodynamic equation can then be written down as a nonlinear Heat equation,

tρ=12i=1dxi,xja¯i,j(ρ(t,θ)).\partial_{t}\rho=\frac{1}{2}\sum_{i=1}^{d}\partial_{x_{i},x_{j}}\bar{a}_{i,j}(\rho(t,\theta)).

We refer to [15], [130], [213] for more discussion and details.

2.5. Why is it called ‘hydrodynamics’?

Finally, we comment on why the scaling limit is called a ‘hydrodynamic limit’. The origins go back to the study of L=ρNL=\rho N identical mass 11 particles with certain positions {q=qi:i=1,2,3}=1L\{q^{\ell}=\langle q^{\ell}_{i}:i=1,2,3\rangle\}_{\ell=1}^{L} and momenta {p=pi:i=1,2,3}=1L\{p^{\ell}=\langle p^{\ell}_{i}:i=1,2,3\rangle\}_{\ell=1}^{L} moving on a torus N𝕋3N{\mathbb{T}}^{3}, with width NN, according to Newtonian dynamics:

dqidt\displaystyle\frac{dq^{\ell}_{i}}{dt} =Hpi=piand\displaystyle=\frac{\partial H}{\partial p^{\ell}_{i}}\ =\ p_{i}^{\ell}\ \ {\rm and\ \ }
dpidt\displaystyle\frac{dp^{\ell}_{i}}{dt} =Hqi=kVi(qqk),\displaystyle=-\frac{\partial H}{\partial q^{\ell}_{i}}\ =\ -\sum_{k}V_{i}(q^{\ell}-q^{k}),

where the energy HH is given by

H\displaystyle H =12i|pi|2+12kV(qqk)\displaystyle=\ \frac{1}{2}\sum_{\ell}\sum_{i}|p^{\ell}_{i}|^{2}+\frac{1}{2}\sum_{\ell\neq k}V\big(q^{\ell}-q^{k}\big)

and V=V1,V2,V3\nabla V=\langle V_{1},V_{2},V_{3}\rangle in terms of an even, nonnegative, smooth, compactly supported function V:3V:\mathbb{R}^{3}\rightarrow\mathbb{R}.

In the system, the total mass, the three components of momentum, and energy are conserved. The question is how to understand in a scaling limit, as time is speeded up by NN, and space is rescaled by N1N^{-1}, the evolution of the local density ρ(t,x)\rho(t,x), momenta w=w1(t,x),w2(t,x),w3(t,x)w=\langle w_{1}(t,x),w_{2}(t,x),w_{3}(t,x)\rangle, and energy e(t,x)e(t,x), that is the ‘hydrodynamic flow’ of the system.

One can form the scaled empirical measures corresponding to these quantities: Writing δ()\delta(\cdot) for the point mass δ\delta_{\cdot},

ξt0\displaystyle\xi^{0}_{t} =\displaystyle= 1N3δ(q(Nt)N)\displaystyle\frac{1}{N^{3}}\sum_{\ell}\delta\Big(\frac{q^{\ell}(Nt)}{N}\Big)
ξti\displaystyle\xi^{i}_{t} =\displaystyle= 1N3δ(q(Nt)N)pi(Nt)fori=1,2,3\displaystyle\frac{1}{N^{3}}\sum_{\ell}\delta\Big(\frac{q^{\ell}(Nt)}{N}\Big)p^{\ell}_{i}(Nt)\ \ \ {\rm for\ }i=1,2,3
ξt4\displaystyle\xi^{4}_{t} =\displaystyle= 1N3δ(q(Nt)N)h(Nt)\displaystyle\frac{1}{N^{3}}\sum_{\ell}\delta\Big(\frac{q^{\ell}(Nt)}{N}\Big)h^{\ell}(Nt)

where energy of the \ellth particle is

h(Nt)=12|p(Nt)|2+12kV(q(Nt)qk(Nt)).h^{\ell}(Nt)\ =\ \frac{1}{2}|p^{\ell}(Nt)|^{2}+\frac{1}{2}\sum_{k}V\big(q^{\ell}(Nt)-q^{k}(Nt)\big).

On the torus N𝕋3N{\mathbb{T}}^{3}, one can define a 55 parameter family of canonical point measures μρ,w,βN\mu^{N}_{\rho,w,\beta}, corresponding to density ρ\rho, velocity ww, and inverse temperature β\beta, which are invariant for the dynamics: Here, L=ρN3L=\rho N^{3} points {q}\{q^{\ell}\} are distributed in N𝕋3N{\mathbb{T}}^{3} according to joint density, with respect to Lebesgue measure,

1Zexp{β2kV(qqk)}\frac{1}{Z}\exp\Big\{-\frac{\beta}{2}\sum_{\ell\neq k}V(q^{\ell}-q^{k})\Big\}

where ZZ is a normalization. The momenta {p}\{p^{\ell}\} are i.i.d. vectors with independent Gaussian components {N(wi,β1):i=1,2,3}\big\{N(w_{i},\beta^{-1}):i=1,2,3\big\}, independent of the positions {q}\{q^{\ell}\}. An infinite volume limit of these measures, as NN\uparrow\infty, might be taken under some conditions.

The goal is to show in some sense the limits ξtiyi(t,x)du\xi^{i}_{t}\rightarrow y^{i}(t,x)du for i=0,1,2,3,4i=0,1,2,3,4 where y=yi:i=0,1,2,3,4y=\langle y_{i}:i=0,1,2,3,4\rangle satisfies an ‘Euler’ equation

ty+xF(y)= 0.\partial_{t}y+\nabla_{x}F(y)\ =\ 0.

Here FF is a 5×35\times 3 matrix. The rigorous passage to such a limit in general is open! In computing tξi\frac{\partial}{\partial t}\xi^{i}, one has to ‘close’ the expressions in terms of functions of the empirical measures. Formally, one can do this and derive the form of FF, subject to a certain ansatz.

For instance, let us derive the equation for the formal limiting ‘local average’ density y0=ρ(t,x)y^{0}=\rho(t,x) in terms of the formal limiting ‘local average’ momentum y1,y2,y3=w(t,x)\langle y^{1},y^{2},y^{3}\rangle=w(t,x). With respect to a test function GG,

ddt1N3G(q(Nt)N)\displaystyle\frac{d}{dt}\frac{1}{N^{3}}\sum_{\ell}G\Big(\frac{q^{\ell}(Nt)}{N}\Big) =1N3G(q(Nt)N)p(Nt)\displaystyle=\frac{1}{N^{3}}\sum_{\ell}\nabla G\Big(\frac{q^{\ell}(Nt)}{N}\Big)\cdot p^{\ell}(Nt)
𝕋3[G(x)w(t,x)]ρ(t,x)𝑑x.\displaystyle\sim\int_{{\mathbb{T}}^{3}}\big[\nabla G(x)\cdot w(t,x)\big]\rho(t,x)dx.

Then,

tρ+(ρw)=0.\partial_{t}\rho+\nabla\cdot(\rho w)=0.

To derive an equation for w(t,x)w(t,x), however, we will need to understand how to average time-dependent quantities involving nonlinear terms such as

pi(Nt)pj(Nt)and(q(Nt)qk(Nt))Vi(q(Nt)qk(Nt)).p^{\ell}_{i}(Nt)p^{\ell}_{j}(Nt)\ {\rm\ and\ \ }\big(q^{\ell}(Nt)-q^{k}(Nt)\big)V_{i}(q^{\ell}(Nt)-q^{k}(Nt)).

One would expect that these quantities could be replaced by space averages with respect to an infinite volume local equilibrium measure.

Such an ergodic theorem for the purely deterministic coupled ODE dynamics to ‘close’ the equation is however difficult to obtain. One of the best results is in [164] where a small amount of noise is added to the dynamics to make it into a reasonable Markov process so that local averaging can be done, and a rigorous limit can be proved. See also the recent developments in the solution of Hilbert’s sixth problem with respect to Boltzmann’s equation [59].

One motivation, among others, for our study of stochastic interacting particle systems is that the randomness of the microscopic motions may allow for suitable ergodic theorems. In a sense, to quote S.R.S. Varadhan, instead of ‘approximating an exact problem’, we will try to solve ‘exactly an approximate problem’. Of course, in the modeling of various phenomena, adding noise to the dynamics is often natural.

Exercise 2.5.1.

Consider the ansatz, with respect to the canonical measures μN(ρ,w,β)\mu^{N}(\rho,w,\beta), that

pi(Nt)pj(Nt)wi(t,x)wj(t,x)+1(i=j)β1(t,x)p^{\ell}_{i}(Nt)p^{\ell}_{j}(Nt)\sim w_{i}(t,x)w_{j}(t,x)+1(i=j)\beta^{-1}(t,x)

and the ‘pressure’

12k(qj(Nt)qjk(Nt))Vi(q(Nt)qk(Nt))Pj,i(ρ(t,x),w(t,x),β1(t,x)),\displaystyle\frac{-1}{2}\sum_{k}\big(q_{j}^{\ell}(Nt)-q_{j}^{k}(Nt)\big)V_{i}\big(q^{\ell}(Nt)-q^{k}(Nt)\big)\sim P_{j,i}\big(\rho(t,x),w(t,x),\beta^{-1}(t,x)\big),

Note that

G(q(Nt)N)kVi(q(Nt)qk(Nt))\displaystyle\sum_{\ell}G\Big(\frac{q^{\ell}(Nt)}{N}\Big)\sum_{k}V_{i}\big(q^{\ell}(Nt)-q^{k}(Nt)\big)
=12,k(G(q(Nt)N)G(qk(Nt)N))Vi(q(Nt)qk(Nt))\displaystyle\quad\quad=\frac{1}{2}\sum_{\ell,k}\Big(G\Big(\frac{q^{\ell}(Nt)}{N}\Big)-G\Big(\frac{q^{k}(Nt)}{N}\Big)\Big)V_{i}\big(q^{\ell}(Nt)-q^{k}(Nt)\big)

as ViV_{i} is anti-symmetric. Derive formally from the ansatz that the equation for w(t,x)w(t,x) is given by

t(wi(t,x)ρ(t,x))+xi(β1(t,x)ρ(t,x))\displaystyle\frac{\partial}{\partial t}\big(w_{i}(t,x)\rho(t,x)\big)+\frac{\partial}{\partial x_{i}}\big(\beta^{-1}(t,x)\rho(t,x)\big)
+j=13xj(wj(t,x)wi(t,x)ρ(t,x))\displaystyle\quad\quad+\sum_{j=1}^{3}\frac{\partial}{\partial x_{j}}\big(w_{j}(t,x)w_{i}(t,x)\rho(t,x)\big)
+j=13xj[Pj,i(ρ(t,x),w(t,x),β1(t,x))ρ(t,x)]=0.\displaystyle\quad\quad+\sum_{j=1}^{3}\frac{\partial}{\partial x_{j}}\big[P_{j,i}\big(\rho(t,x),w(t,x),\beta^{-1}(t,x)\big)\rho(t,x)\big]=0.

We note that the last equation for the energy y5=ey^{5}=e should be

t(e(t,x)ρ(t,x))+j=13xj(e(t,x)wj(t,x)ρ(t,x))\displaystyle\frac{\partial}{\partial t}\big(e(t,x)\rho(t,x)\big)+\sum_{j=1}^{3}\frac{\partial}{\partial x_{j}}\big(e(t,x)w_{j}(t,x)\rho(t,x)\big)
+j=13i=13xj[Pj,i(ρ(t,x),w(t,x),β1(t,x))wi(t,x)ρ(t,x)]=0.\displaystyle\quad\quad+\sum_{j=1}^{3}\sum_{i=1}^{3}\frac{\partial}{\partial x_{j}}\big[P_{j,i}\big(\rho(t,x),w(t,x),\beta^{-1}(t,x)\big)w_{i}(t,x)\rho(t,x)\big]=0.

2.6. Notes

The material on martingales can be found in [66] for instance, and other places. Similar treatments of the hydrodynamics of exclusion can be found in [130] and [213].

The exclusion process–see [100] for a retrospective–has many properties which make it amenable to calculation. It has proved to be a versatile model, which can be defined on very general graphs. See [58], [147], [148], [149], [150], [190] for detailed studies using different properties.

We comment one may formulate other empirical measures of interest, those of ‘higher order’ [46], or with respect to ‘local functions’ [130][Chapter III, Lemma V.5.5].

As one can see in the sketch of the hydrodynamics for symmetric exclusion processes, requirements may be weakened on the initial measure. In fact, what is needed is a guarantee of a law of large numbers at time 00. The concept of ‘very weak local equilibrium’ given below (cf. Chapter III in [130]) is sufficient and somewhat general.

Let ρ0:𝕋d+\rho_{0}:{\mathbb{T}}^{d}\rightarrow\mathbb{R}_{+} be a function. We say that a sequence of probability measures μN\mu^{N} on 𝕋Nd{\mathbb{T}}^{d}_{N} is a ‘very weak local equilibrium’ according to profile ρ0\rho_{0} if

limNEμN[|1Ndx𝕋NdG(x/N)η(x)𝕋dG(u)ρ0(u)𝑑u|]= 0.\lim_{N\uparrow\infty}E_{\mu^{N}}\Big[\Big|\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}G(x/N)\eta(x)-\int_{{\mathbb{T}}^{d}}G(u)\rho_{0}(u)du\Big|\Big]\ =\ 0.

for all bounded, continuous G:𝕋dG:{\mathbb{T}}^{d}\rightarrow\mathbb{R}.

We remark that μN\mu^{N} may be degenerate, that is supported on a single configuration, and that the sequence {μN}\{\mu^{N}\} may consist of deterministic configurations which satisfy the law of large numbers in the definition above.

With respect to Subsection 2.5, for further discussion of hydrodynamics of deterministic evolutions see [206][Part 1], [186], [59]. An early work in this regard is [161]. We have followed the scheme in [213] which also elaborates more on the calculations surrounding Exercise 2.5.1.

Section 3 Proof of hydrodynamics for symmetric exclusion processes

After stating the main theorem, we provide an outline of the proof and provide details on the associated steps. Such an outline can be used to prove ‘hydrodynamic limits’ in other models, in particular in zero-range processes in Chapter 4.

3.1. Statement of hydrodynamics

Recall the notation from the last subsection, with respect to dd-dimensional symmetric exclusion processes with finite-range symmetric jump rate pp, in particular the definition of the operator C=1i,jdCi,j2xi,xj\triangle_{C}\ =\ \sum_{1\leq i,j\leq d}C_{i,j}\partial^{2}_{x_{i},x_{j}} with Ci,j=z𝕋Ndzizjp(z)C_{i,j}=\sum_{z\in{\mathbb{T}}^{d}_{N}}z_{i}z_{j}p(z), and the measure μN=νρ0()N=x𝕋NdBern(ρ0(x/N))\mu^{N}=\nu^{N}_{\rho_{0}(\cdot)}=\prod_{x\in{\mathbb{T}}_{N}^{d}}{\rm Bern}(\rho_{0}(x/N)). Recall also that μN\mathbb{P}_{\mu^{N}} and 𝔼μN\mathbb{E}_{\mu^{N}} stand for the process measure and expectation starting from μN\mu^{N}.

Theorem 3.1.1.

Consider the symmetric exclusion process with finite-range translation-invariant jump probabilities. Then, starting from the local equilibrium measure μN\mu^{N}, associated with continuous profile ρ0()\rho_{0}(\cdot), the empirical measure πN2tN\pi^{N}_{N^{2}t} converges in probability to the measure ρ(t,u)du\rho(t,u)du where ρ(t,u)\rho(t,u) satisfies the hydrodynamic equation

tρ(t,u)=12Cρ(t,u),andρ(0,u)=ρ0(u).\partial_{t}\rho(t,u)\ =\ \frac{1}{2}\triangle_{C}\rho(t,u),\ \ \ {\rm and\ \ \ }\rho(0,u)=\rho_{0}(u). (3.1.1)

The proof is given through the following rough steps, which are then explained in more detail in later subsections.

Step 1. Consider the trajectory of empirical measures indexed in an interval of time, πN=πN2tN:t[0,T]\pi^{N}=\langle\pi^{N}_{N^{2}t}:t\in[0,T]\rangle. Here, T>0T>0 is time length, fixed throughout. Let QNQ^{N} be the law of the trajectory. The first step is to show that the laws {QN:N1}\{Q^{N}:N\geq 1\} are tight in the space of measure-valued right-continuous trajectories with left limits, the Skorohod space 𝒟([0,T],+(𝕋d))\mathcal{D}([0,T];\mathcal{M}_{+}({\mathbb{T}}^{d})). We will show this tightness in the stronger uniform topology.

Step 2. Given tightness, we will show that any subsequential limit QQ of QNQ^{N} must be supported on trajectories πt:t[0,T]\langle\pi_{t}:t\in[0,T]\rangle satisfying

G(t,),πtG(0,),ρ0=0t(s+12C)G(s,),πsds.\langle G(t,\cdot),\pi_{t}\rangle-\langle G(0,\cdot),\rho_{0}\rangle\ =\ \int_{0}^{t}\Big\langle\Big(\partial_{s}+\frac{1}{2}\triangle_{C}\Big)G(s,\cdot),\pi_{s}\Big\rangle ds. (3.1.2)

This equation is similar to what was derived in the last subsection when GG did not depend on time. However, to input into PDE uniqueness results, we will need to derive the equation with respect to this wider class of functions GG. Moreover, after also showing in Step 3 below that trajectories under a limit point QQ are absolutely continuous, we will be able to conclude the associated densities satisfy a weak formulation of (3.1.1).

Step 3. We will show that QQ supports trajectories such that for each t[0,T]t\in[0,T], πt\pi_{t} is absolutely continuous with respect to Lebesgue measure on 𝕋d{\mathbb{T}}^{d}, and hence can be written as πt=ρ(t,u)du\pi_{t}=\rho(t,u)du, which is a priori random. Therefore, from Step 2, ρ(t,u)\rho(t,u) is a weak solution of the hydrodynamic equation (3.1.1). By uniqueness of weak solutions to the heat equation in the class of bounded solutions, we see that ρ(t,u)\rho(t,u) is actually deterministic. In particular, all subsequential limits of QNQ^{N} converge to the point mass supported on the trajectory ρ(t,u)du:t[0,T]\langle\rho(t,u)du:t\in[0,T]\rangle. Since tightness was proved in the uniform topology, this trajectory is continuous in time. [This can also be inferred from regularity results in PDE.] Hence, it can be concluded, at a fixed time t[0,T]t\in[0,T], that πN2tN\pi^{N}_{N^{2}t} converges weakly to a constant, the measure ρ(t,u)du\rho(t,u)du, and hence in fact converges in probability.

3.1.1. Proof of Step 2: Identification

We recall that we have almost shown Step 2 in the last subsection. To this end, let G:+×𝕋dG:\mathbb{R}_{+}\times{\mathbb{T}}^{d}\rightarrow\mathbb{R} be a smooth C2C^{2} function. By the development in Subsection 2.4.1, we obtain

G(t,),πN2tN\displaystyle\langle G(t,\cdot),\pi^{N}_{N^{2}t}\rangle =\displaystyle= G(0,),π0N+0t(s+N2L)G(s,),πsNds+MtN(G)\displaystyle\langle G(0,\cdot),\pi^{N}_{0}\rangle+\int_{0}^{t}(\partial_{s}+N^{2}L)\langle G(s,\cdot),\pi^{N}_{s}\rangle ds+M^{N}_{t}(G)
=\displaystyle= G(0,),π0N+0t(s+N2N22C)G(s,),πsNds+o(1)\displaystyle\langle G(0,\cdot),\pi^{N}_{0}\rangle+\int_{0}^{t}\Big\langle\Big(\partial_{s}+\frac{N^{2}N^{-2}}{2}\triangle_{C}\Big)G(s,\cdot),\pi^{N}_{s}\Big\rangle ds+o(1)
=\displaystyle= G(0,),π0N+0t(s+12C)G(s,),πsNds+o(1).\displaystyle\langle G(0,\cdot),\pi^{N}_{0}\rangle+\int_{0}^{t}\Big\langle\Big(\partial_{s}+\frac{1}{2}\triangle_{C}\Big)G(s,\cdot),\pi^{N}_{s}\big\rangle ds+o(1).

Therefore, if πt:t[0,T]\langle\pi_{t}:t\in[0,T]\rangle is a limit point of πtN:t[0,T]\langle\pi^{N}_{t}:t\in[0,T]\rangle, we obtain (3.1.2).

We now discuss more carefully some topological considerations and argue Step 1, the most difficult part. Afterwards, we concentrate on Step 3 in a subsequent subsection.

3.2. Topology and compactness

Before making calculations with respect to Step 1, we first recall some definitions and results on weak convergence, and the spaces C([0,T],+(𝕋d))C\big([0,T];\mathcal{M}_{+}({\mathbb{T}}^{d})\big) and 𝒟([0,T],+(𝕋d))\mathcal{D}\big([0,T];\mathcal{M}_{+}({\mathbb{T}}^{d})\big) with a view toward characterizing when a sequence of probability measures QQ on these spaces is tight. More details can be found in [27], [130][Section 4.1].

First, we recall that a family of probability measures QNQ^{N} on a metric space is relatively compact if any subsequence of the family has a weakly convergent subsequence. We say that the family is tight if for each ϵ>0\epsilon>0 there is a compact set KϵK_{\epsilon} such that all measures give at least weight 1ϵ1-\epsilon to KϵK_{\epsilon}. Recall that Ω\Omega is a complete metric space if all Cauchy sequences converge in Ω\Omega, and Ω\Omega is a separable space if it contains a countable dense set of points.

Proposition 3.2.1 (Prokhorov’s theorem).

Let Ω\Omega be a complete, separable metric space. Then, a family QNQ^{N} of probability measures on Ω\Omega is relatively compact exactly when the family is tight.

Moreover, if Ω\Omega is a complete metric space, then a family QNQ^{N} of probability measures on Ω\Omega is relatively compact when the family is tight.

We will consider in the following a generic complete, separable space Ω\Omega with metric δ\updelta. Often, Ω\Omega will be +\mathcal{M}_{+} the space of finite measures on 𝕋d{\mathbb{T}}^{d} equipped with the metric

δ(μ,ν)=k112k|fk,μfk,ν|1+|fk,μfk,ν|\updelta(\mu,\nu)\ =\ \sum_{k\geq 1}\frac{1}{2^{k}}\frac{|\langle f_{k},\mu\rangle-\langle f_{k},\nu\rangle|}{1+|\langle f_{k},\mu\rangle-\langle f_{k},\nu\rangle|}

where {fk}\{f_{k}\} is a countable dense set of functions in C(𝕋d)C({\mathbb{T}}^{d}), the space of continuous functions on the torus 𝕋d{\mathbb{T}}^{d} endowed with the ‘sup’ metric fg\|f-g\|_{\infty} between ff and gg. We may take f11f_{1}\equiv 1. Here, +=+(𝕋d)\mathcal{M}_{+}=\mathcal{M}_{+}({\mathbb{T}}^{d}) is a complete, separable metric space. Moreover, a set K+K\subset\mathcal{M}_{+} is relatively compact exactly when supμK|1,μ|<\sup_{\mu\in K}|\langle 1,\mu\rangle|<\infty.

At other times, Ω\Omega may be \mathbb{R} with usual Euclidean metric.

Now, we consider the space C([0,T],Ω)C([0,T];\Omega) with the ‘uniform’ distance,

d(π,χ)=supt[0,T]δ(πt,χt).d(\pi,\chi)\ =\ \sup_{t\in[0,T]}\updelta(\pi_{t},\chi_{t}).

It is known that this space is a complete separable space, and therefore amenable to Prokhorov’s theorem.

Since our basic building blocks in our study of hydrodynamics involve jump processes, the space of continuous trajectories is not sufficient for our purposes. We will often focus on the space 𝒟([0,T],Ω)\mathcal{D}([0,T],\Omega) of right-continuous trajectories with left limits. Unfortunately, the uniform distance will not make this space a complete, separable metric space. Define Λ\Lambda to be the set of strictly increasing continuous functions λ\lambda of [0,T][0,T] into itself, and

λ=supst|logλ(t)λ(s)ts|.\|\lambda\|\ =\ \sup_{s\neq t}\left|\log\frac{\lambda(t)-\lambda(s)}{t-s}\right|.

Then, define the Skorohod distance between elements in 𝒟([0,T],+)\mathcal{D}([0,T],\mathcal{M}_{+}) as

d(π,χ)=infλΛmax{λ,supt[0,T]δ(πt,χλ(t))}.d(\pi,\chi)\ =\ \inf_{\lambda\in\Lambda}\max\left\{\|\lambda\|,\sup_{t\in[0,T]}\updelta(\pi_{t},\chi_{\lambda(t)})\right\}.

In some sense, the Skorohod distance compares two trajectories allowing small variation both in space and in time. To contrast, the uniform distance only compares variation in space. With the Skorohod distance, 𝒟([0,T],Ω)\mathcal{D}([0,T],\Omega) is a complete, separable metric space.

How to characterize compact sets in these spaces? Consider the following moduli of continuity:

wπ(γ)\displaystyle w_{\pi}(\gamma) =\displaystyle= sups,t[0,T]|ts|γδ(πt,πs)\displaystyle\sup_{\stackrel{{\scriptstyle|t-s|\leq\gamma}}{{s,t\in[0,T]}}}\updelta(\pi_{t},\pi_{s})
wπ(γ)\displaystyle w^{\prime}_{\pi}(\gamma) =\displaystyle= inf{ti}i=0rmaxsuptis<t<ti+10ir1δ(πs,πt)\displaystyle\inf_{\{t_{i}\}_{i=0}^{r}}\max_{0\leq i\leq r-1}\sup_{t_{i}\leq s<t<t_{i+1}}\updelta(\pi_{s},\pi_{t})

where {ti}i=0r\{t_{i}\}_{i=0}^{r} refers to a partition 0=t0<<tr=T0=t_{0}<\cdots<t_{r}=T such that ti+1ti>γt_{i+1}-t_{i}>\gamma for 0ir10\leq i\leq r-1.

Then, π\pi belongs to C([0,T],Ω)C([0,T],\Omega) exactly when limγ0wπ(γ)=0\lim_{\gamma\downarrow 0}w_{\pi}(\gamma)=0, and π\pi belongs to 𝒟([0,T],Ω)\mathcal{D}([0,T],\Omega) exactly when limγ0wπ(γ)=0\lim_{\gamma\downarrow 0}w^{\prime}_{\pi}(\gamma)=0.

Exercise 3.2.2.

Relate the two moduli by showing that

wπ(γ)wπ(2γ).w^{\prime}_{\pi}(\gamma)\ \leq\ w_{\pi}(2\gamma).
Exercise 3.2.3.

Show, when Ω=\Omega=\mathbb{R} and π=1([0,T/2))\pi=1\big([0,T/2)\big), that limγ0wπ(γ)=0\lim_{\gamma\downarrow 0}w^{\prime}_{\pi}(\gamma)=0 but lim infγ0wπ(γ)>0\liminf_{\gamma\downarrow 0}w_{\pi}(\gamma)>0.

Compact sets in these spaces, since they are complete, are characterized as follows.

Proposition 3.2.4.

A set AA belonging to C([0,T],Ω)C([0,T],\Omega) or 𝒟([0,T],Ω)\mathcal{D}([0,T],\Omega) is compact exactly when

  • (a)

    {πt:πA}\{\pi_{t}:\pi\in A\} is relatively compact in Ω\Omega for each t[0,T]t\in[0,T].

  • (b)

    limγ0supπAw¯π(γ)=0\lim_{\gamma\downarrow 0}\sup_{\pi\in A}\bar{w}_{\pi}(\gamma)=0 where w¯π=wπ\bar{w}_{\pi}=w_{\pi} on C([0,T],Ω)C([0,T],\Omega) and w¯π=wπ\bar{w}_{\pi}=w^{\prime}_{\pi} on 𝒟([0,T],Ω)\mathcal{D}([0,T],\Omega).

We remark, when AC([0,T],[a,b])A\subset C([0,T],[a,b]), the above characterization reduces to the Ascoli-Arzela condition with respect to equicontinuous families of trajectories on the finite interval [a,b][a,b], and (a) can be replaced by ‘{π0:πA}\{\pi_{0}:\pi\in A\} is relatively compact in Ω\Omega’.

Recall now Exercise 3.2.2. We now have the following claim.

Proposition 3.2.5.

A family QNQ^{N} of probability measures on 𝒟([0,T],Ω)\mathcal{D}([0,T],\Omega) is tight exactly when

  • (1)

    For each t[0,T]t\in[0,T], the distributions of πt\pi_{t} under QNQ^{N} are tight.

  • (2)

    For every ϵ>0\epsilon>0, limγ0limNQN(π:wπ(γ)>ϵ)=0\lim_{\gamma\downarrow 0}\lim_{N\uparrow\infty}Q^{N}(\pi:w^{\prime}_{\pi}(\gamma)>\epsilon)=0.

Moreover, a sufficient condition for (2)(2) is

  • (2’)

    In condition (2)(2), replace wπw^{\prime}_{\pi} with wπw_{\pi}.

Exercise 3.2.6.

Observe that any limit point QQ of {Qn}\{Q^{n}\} satisfying (2)(2^{\prime}) is supported on continuous paths. This is a well-known property; see [27].

It is not so easy to work with (2)(2^{\prime}) directly. However, when Ω=+\Omega=\mathcal{M}_{+}, one can understand a family QNQ^{N} of probability measures on 𝒟([0,T],+)\mathcal{D}([0,T],\mathcal{M}_{+}) by their actions on smooth functions on 𝕋d{\mathbb{T}}^{d}.

Proposition 3.2.7.

A family {QN}\{Q^{N}\} of probability measures on 𝒟([0,T],+)\mathcal{D}([0,T],\mathcal{M}_{+}) is tight if the distributions of {G,πt:t[0,T]}\{\langle G,\pi_{t}\rangle:t\in[0,T]\} under QNQ^{N} for N1N\geq 1 are tight in 𝒟([0,T],)\mathcal{D}([0,T],\mathbb{R}), that is satisfying (1) and (2’) in Proposition 3.2.5, for each GC2(𝕋d)G\in C^{2}({\mathbb{T}}^{d}).

Exercise 3.2.8.

Give a proof of Proposition 3.2.7. Hint: See Proposition IV.1.7 in [130].

3.3. Proof of Step 1: Tightness

We are now back to considering the tightness of πN=πN2tN:t[0,T]\pi^{N}=\langle\pi^{N}_{N^{2}t}:t\in[0,T]\rangle for N1N\geq 1 which are elements of 𝒟([0,T],+)\mathcal{D}([0,T],\mathcal{M}_{+}). From Proposition 3.2.7, we need only show for a smooth function G:𝕋dG:{\mathbb{T}}^{d}\rightarrow\mathbb{R}, tightness of the distributions of {G,πN2tN:t[0,T]}\{\langle G,\pi^{N}_{N^{2}t}\rangle:t\in[0,T]\} for N1N\geq 1 which are elements of 𝒟([0,T],)\mathcal{D}([0,T],\mathbb{R}).

From Proposition 3.2.5, we need to show conditions (1)(1) and (2)(2^{\prime}). Condition (1)(1) is the simplest, and follows straightforwardly as for each t[0,T]t\in[0,T],

|G,πN2tN|G1Ndx𝕋NdηN2t(x)G.|\langle G,\pi^{N}_{N^{2}t}\rangle|\ \leq\ \|G\|_{\infty}\cdot\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta_{N^{2}t}(x)\ \leq\ \|G\|_{\infty}.

Then, G,πN2tN\langle G,\pi^{N}_{N^{2}t}\rangle is a tight sequence in \mathbb{R} as the sequence is uniformly bounded in NN with full probability.

Verifying Condition (2)(2^{\prime}), and therefore tightness in the uniform topology, is a little more involved. Since

G,πN2tN=G,π0N+120t1Ndx,y𝕋NdηN2s(x)p(y)x,yNG𝑑s+MtN(G),\langle G,\pi_{N^{2}t}^{N}\rangle\ =\ \langle G,\pi^{N}_{0}\rangle+\frac{1}{2}\int_{0}^{t}\frac{1}{N^{d}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}\eta_{N^{2}s}(x)p(y)\triangle^{N}_{x,y}Gds+M^{N}_{t}(G),

we need only show condition (2’) for each term separately. The initial term G,π0N\langle G,\pi^{N}_{0}\rangle does not contribute in this respect.

We now bound the second term. Condition (2’) follows as

sup|ts|γ|st1Ndx,y𝕋NdηN2s(x)p(y)x,yNG𝑑s|γRG\sup_{|t-s|\leq\gamma}\Big|\int_{s}^{t}\frac{1}{N^{d}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}\eta_{N^{2}s}(x)p(y)\triangle^{N}_{x,y}Gds\Big|\ \leq\ \gamma R\|\triangle G\|_{\infty}

where RR is the range of the probability pp.

For the third term, to treat condition (2’), we first recall Doob’s inequality (cf. [63]): For a martingale (Mt,t)(M_{t},\mathcal{F}_{t}), a,b[0,T]a,b\in[0,T] and λ>0\lambda>0, we have

μN(supt[a,b]|MtMa|>λ)\displaystyle\mathbb{P}_{\mu^{N}}\Big(\sup_{t\in[a,b]}|M_{t}-M_{a}|>\lambda\Big) \displaystyle\leq 1λ2𝔼μN[|MbMa|2].\displaystyle\frac{1}{\lambda^{2}}\mathbb{E}_{\mu^{N}}\Big[|M_{b}-M_{a}|^{2}\Big].

Now, partition the interval [0,T][0,T] into T/γ+1\lfloor T/\gamma\rfloor+1 divisions {lk}\{l_{k}\} of sublength γ\gamma, assuming γ\gamma does not divide TT and l0=0l_{0}=0. Noting, when |ts|γ|t-s|\leq\gamma, that either both t,st,s lie in the same subinterval or lie in adjacent intervals, we have

μN(sup|ts|γ|MtN(G)MsN(G)|>λ)\displaystyle\mathbb{P}_{\mu^{N}}\Big(\sup_{|t-s|\leq\gamma}|M^{N}_{t}(G)-M^{N}_{s}(G)|>\lambda\Big)
μN(sup0kT/γlk<tlk+1|MtN(G)MlkN(G)|>λ/3)\displaystyle\ \ \ \leq\ \mathbb{P}_{\mu^{N}}\Big(\sup_{\stackrel{{\scriptstyle l_{k}<t\leq l_{k+1}}}{{0\leq k\leq\lfloor T/\gamma\rfloor}}}|M^{N}_{t}(G)-M^{N}_{l_{k}}(G)|>\lambda/3\Big)
k=0T/γμN(suplk<tlk+1|MtN(G)MlkN(G)|>λ/3)\displaystyle\ \ \ \leq\ \sum_{k=0}^{\lfloor T/\gamma\rfloor}\mathbb{P}_{\mu^{N}}\Big(\sup_{l_{k}<t\leq l_{k+1}}|M^{N}_{t}(G)-M^{N}_{l_{k}}(G)|>\lambda/3\Big)
9λ2k=0T/γ𝔼μN[|Mlk+1N(G)MlkN(G)|2].\displaystyle\ \ \ \ \leq\ \frac{9}{\lambda^{2}}\sum_{k=0}^{\lfloor T/\gamma\rfloor}\mathbb{E}_{\mu^{N}}\Big[|M^{N}_{l_{k+1}}(G)-M^{N}_{l_{k}}(G)|^{2}\Big]. (3.3.1)

Note the quadratic variation bound for MtN(G)MlkN(G)M^{N}_{t}(G)-M^{N}_{l_{k}}(G) near (2.4.1),

𝔼μN[(Mlk+1N(G)MlkN(G))2]\displaystyle\mathbb{E}_{\mu^{N}}\Big[(M^{N}_{l_{k+1}}(G)-M^{N}_{l_{k}}(G))^{2}\Big] \displaystyle\leq 𝔼μN[Mlk+1N(G)MlkN(G)t]\displaystyle\mathbb{E}_{\mu^{N}}\Big[\langle M^{N}_{l_{k+1}}(G)-M^{N}_{l_{k}}(G)\rangle_{t}\Big]
=\displaystyle= 𝔼μN[N22N2d+2lklk+1x,y𝕋Ndp(y)(x,yNG)2𝑑u]\displaystyle\mathbb{E}_{\mu^{N}}\Big[\frac{N^{2}}{2N^{2d+2}}\int_{l_{k}}^{l_{k+1}}\sum_{x,y\in{\mathbb{T}}^{d}_{N}}p(y)(\nabla^{N}_{x,y}G)^{2}du\Big]
=\displaystyle= O(RGNd|lk+1lk|),\displaystyle O\big(R\|\nabla G\|_{\infty}N^{-d}|l_{k+1}-l_{k}|\big),

to bound (3.3) of order O(γ1γRGNd)O(\gamma^{-1}\gamma R\|\nabla G\|_{\infty}N^{-d}) which vanishes as NN\uparrow\infty.

3.4. Proof of Step 3: Absolute continuity

To show πt\pi_{t} is absolutely continuous, observe for any continuous function G:𝕋dG:{\mathbb{T}}^{d}\rightarrow\mathbb{R} that

supt[0,T]|G,πN2tN|\displaystyle\sup_{t\in[0,T]}|\langle G,\pi^{N}_{N^{2}t}\rangle| \displaystyle\leq 1Ndx𝕋Nd|G(x/N)|ηN2t(x)\displaystyle\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}|G(x/N)|\eta_{N^{2}t}(x)
\displaystyle\leq GL1,\displaystyle\|G\|_{L^{1}},

since at most one particle is allowed per site. Hence, since the function

πt:t[0,T]supt[0,T]|G,πt|\langle\pi_{t}:t\in[0,T]\rangle\ \mapsto\ \sup_{t\in[0,T]}|\langle G,\pi_{t}\rangle|

is continuous with respect to the Skorohod topology, any limit point satisfies, with full probability (see Portmanteau theorem [27][Chapter 1]),

supt[0,T]|G,πt|GL1.\sup_{t\in[0,T]}|\langle G,\pi_{t}\rangle|\ \leq\ \|G\|_{L^{1}}.

Hence, any limit point QQ of {QN}\{Q^{N}\} is supported on trajectories with the property that πt\pi_{t} is absolutely continuous for all t[0,T]t\in[0,T].

Exercise 3.4.1.

Detail the use of the Portmanteau theorem in the previous paragraph.

At this point, as noted in the initial strategy, for each t[0,T]t\in[0,T], πt\pi_{t} can be written as πt=ρ(t,u)du\pi_{t}=\rho(t,u)du where ρ\rho may be random. However, by Step 2, ρ\rho is a weak solution to the hydrodynamic equation, which has a unique bounded solution. Therefore, ρ\rho is deterministic, and πt=ρ(t,u)du\pi_{t}=\rho(t,u)du where ρ\rho is the hydrodynamic density. We remark when ρ0C2(𝕋d)\rho_{0}\in C^{2}({\mathbb{T}}^{d}) then m(t,u)m(t,u) is actually a ‘classical’ solution given in terms of a Gaussian kernel convolution with ρ0\rho_{0}.

What we have shown is that the law of πN2tN:t[0,T]\langle\pi^{N}_{N^{2}t}:t\in[0,T]\rangle, where initial configurations are distributed according to μN\mu^{N}, converges to the point mass on trajectory ρ(t,u)du:t[0,T]\langle\rho(t,u)du:t\in[0,T]\rangle. To conclude convergence at a fixed time t[0,T]t\in[0,T], we note that in Step 1, tightness of QNQ^{N} was obtained in the uniform topology. Hence, the trajectory in the support of the limit QQ is continuous for all t[0,T]t\in[0,T]. For t[0,T]t\in[0,T], let hth_{t} be the projection function,

πt:t[0,T]πt.\langle\pi_{t}:t\in[0,T]\rangle\ \mapsto\ \pi_{t}.

Now, hth_{t} is not continuous on 𝒟([0,T],+)\mathcal{D}([0,T];\mathcal{M}_{+}). However, since the limit QQ is supported on a continuous trajectory, hth_{t} is continuous on the support of QQ. Now it is known that if QNQQ^{N}\Rightarrow Q and h=hth=h_{t} is a continuous function almost surely on the support of QQ, then QNht1Qht1Q^{N}\circ h_{t}^{-1}\Rightarrow Q\circ h_{t}^{-1} (see [27][Chapter 1]). In other words, the projection πN2tN\pi^{N}_{N^{2}t} converges in law to the point mass at ρ(t,u)du\rho(t,u)du, and therefore also in probability.

3.5. Notes

There are other proofs of hydrodynamics for symmetric exclusion processes, for instance using correlation functions and ‘duality’ as in [58] or superexponential estimates as in [213]. We have followed mostly the treatment with some caveats in [130], following the strategy, in the symmetric exclusion context, expounded in [106], a classic in the field. It is worth noting by this method we have shown existence of weak solutions to the PDE (3.1.1).

Besides [27], other good references for ‘weak convergence’ in general spaces include [66], [116], [169].

We note, a subject of interest has been hydrodynamics of exclusion and other processes where the jump parameters are chosen from random environments, or when there are boundary conditions and reservoirs (cf. among others, [20], [70], [79], [122], [124], [138], [204], [223], and references therein).

Section 4 Entropy, Dirichlet form, and averaging principle in zero-range processes

We now consider another well-studied ‘mass conservative’ interacting particle system, the so called ‘zero-range’ model. Unlike for symmetric simple exclusion, the evolution equation for the mass empirical measure does not close, and one must invoke an ‘averaging principle’ to approximate a nonlinear term in terms of a function of the empirical measure. Here, we develop the ‘entropy method’ for this rigorous replacement in the associated hydrodynamics. To this end, notions of entropy and Dirichlet form, as well as the ‘basic coupling’, are introduced before defining the zero-range process. At the end, we give an outline to derive the associated hydrodynamical equation.

The following Chapter 5 is devoted to proving steps in the outline, including the famous so called ‘1-block’ and ‘2-block’ lemmas introduced in [106].

4.1. Relative entropy

Let Ω\Omega be a countable space. For probability measures μ\mu and ν\nu on Ω\Omega, define the relative entropy of μ\mu with respect to ν\nu as

H(μ|ν)=supf{Eμ[f]logEν[ef]}H(\mu|\nu)\ =\ \sup_{f}\left\{E_{\mu}[f]-\log E_{\nu}\big[e^{f}\big]\right\} (4.1.1)

where the supremum is over bounded functions f:Ωf:\Omega\rightarrow\mathbb{R}. Recall, as before, EκE_{\kappa} stands for the expectation under κ\kappa.

Since the expression

Eμ[(f+c)]logEν[e(f+c)]=Eμ[f]logEν[ef]E_{\mu}[(f+c)]-\log E_{\nu}\big[e^{(f+c)}\big]\ =\ E_{\mu}[f]-\log E_{\nu}\big[e^{f}\big]

is invariant for all constants cc, the above supremum can be taken over bounded nonnegative functions ff.

Exercise 4.1.1.

Show that H(μ|ν)H(\mu|\nu) is nonnegative, convex and lower semi-continuous in the argument μ\mu (where μnμ\mu_{n}\rightarrow\mu if μn\mu_{n} converges weakly to μ\mu). Hint: For nonnegativity, substitute ff equal to a constant.

Lemma 4.1.2 (Entropy inequality).

For all bounded functions f:Ωf:\Omega\rightarrow\mathbb{R} and α>0\alpha>0, we have

Eμ[f]1αH(μ|ν)+1αlogEν[eαf].E_{\mu}[f]\ \leq\ \frac{1}{\alpha}H(\mu|\nu)+\frac{1}{\alpha}\log E_{\nu}\big[e^{\alpha f}\big].

Also, when f=1(A)f=1(A), for AΩA\subset\Omega, one has

μ(A)log2+H(μ|ν)log(1+1ν(A)).\mu(A)\ \leq\frac{\log 2+H(\mu|\nu)}{\log\big(1+\frac{1}{\nu(A)}\big)}.
Exercise 4.1.3.

Prove this lemma. Hint: Multiply and divide by α\alpha.

Lemma 4.1.4.

We have H(μ|ν)<H(\mu|\nu)<\infty implies that μν\mu\ll\nu. Also, if μν\mu\ll\nu, then

H(μ|ν)=xΩμ(x)logμ(x)ν(x)=xΩν(x)μ(x)ν(x)logμ(x)ν(x).H(\mu|\nu)\ =\ \sum_{x\in\Omega}\mu(x)\log\frac{\mu(x)}{\nu(x)}=\sum_{x\in\Omega}\nu(x)\frac{\mu(x)}{\nu(x)}\log\frac{\mu(x)}{\nu(x)}.

Moreover, when Ω\Omega is finite, we have μνH(μ|ν)=xΩμ(x)logμ(x)ν(x)<\mu\ll\nu\Leftrightarrow H(\mu|\nu)=\sum_{x\in\Omega}\mu(x)\log\frac{\mu(x)}{\nu(x)}<\infty.

Proof.

If μ≪̸ν\mu\not\ll\nu, there is an x0Ωx_{0}\in\Omega such that μ(x0)>0\mu(x_{0})>0 but ν(x0)=0\nu(x_{0})=0. In the variational definition of H(μ|ν)H(\mu|\nu), we can insert the function f(x)=1(x=x0)f(x)=1(x=x_{0}) to see H(μ|ν)=H(\mu|\nu)=\infty. Hence, H(μ|ν)<μνH(\mu|\nu)<\infty\Rightarrow\mu\ll\nu.

We now suppose μν\mu\ll\nu and prove the equality in the display. By simple truncations, approximate H(μ|ν)H(\mu|\nu) in (4.1.1) by the supremum over functions which vanish except for a finite number of points in Ω\Omega. We now find the maximum of

fxΩkμ(x)f(x)log[xΩkν(x)ef(x)+(1ν(Ωk)],f\mapsto\sum_{x\in\Omega_{k}}\mu(x)f(x)-\log\Big[\sum_{x\in\Omega_{k}}\nu(x)e^{f(x)}+(1-\nu(\Omega_{k})\Big],

over functions ff supported on Ωk\Omega_{k} where ΩkΩ\Omega_{k}\subset\Omega and |Ωk|=k<|\Omega_{k}|=k<\infty. Indeed, the functional is concave and takes its maximum where its gradient vanishes. Computing the gradient, we obtain the maximum occurs when

μ(x0)=ν(x0)ef(x0)xΩkν(x)ef(x)+(1ν(Ωk)CLOSE\mu(x_{0})\ =\ \frac{\nu(x_{0})e^{f(x_{0})}}{\sum_{x\in\Omega_{k}}\nu(x)e^{f(x)}+(1-\nu(\Omega_{k})}

for each x0Ωkx_{0}\in\Omega_{k}. We can add a constant cc to ff, noting 1ν(Ωk)=xΩkef(x)1-\nu(\Omega_{k})=\sum_{x\not\in\Omega_{k}}e^{f(x)} and ef(x)+c=ece^{f(x)+c}=e^{c} for xΩkx\not\in\Omega_{k}, and not change this equation–the mapping is extended to functions which are constant off Ωk\Omega_{k}. Hence, we may choose cc so that

xΩkν(x)ef(x)+c+ec(1ν(Ωk))= 1.\sum_{x\in\Omega_{k}}\nu(x)e^{f(x)+c}+e^{c}(1-\nu(\Omega_{k}))\ =\ 1.

With this choice, we obtain f(x0)+c=log(μ(x0)/ν(x0))f(x_{0})+c=\log\big(\mu(x_{0})/\nu(x_{0})\big) for x0Ωkx_{0}\in\Omega_{k}, with convention 0/0=10/0=1 . As kk\uparrow\infty and ΩkΩ\Omega_{k}\uparrow\Omega, since log[μ(Ωk)+ec(1ν(Ωk))]\log\big[\mu(\Omega_{k})+e^{c}(1-\nu(\Omega_{k}))\big] vanishes, we have the upper bound

H(μ|ν)\displaystyle H(\mu|\nu) xΩμ(x)logμ(x)ν(x)limklog[xΩkν(x)μ(x)ν(x)+ec(1ν(Ωk))]\displaystyle\leq\sum_{x\in\Omega}\mu(x)\log\frac{\mu(x)}{\nu(x)}-\lim_{k\uparrow\infty}\log\Big[\sum_{x\in\Omega_{k}}\nu(x)\frac{\mu(x)}{\nu(x)}+e^{c}(1-\nu(\Omega_{k}))\Big]
=xΩμ(x)logμ(x)ν(x).\displaystyle=\sum_{x\in\Omega}\mu(x)\log\frac{\mu(x)}{\nu(x)}.

We obtain the lower bound H(μ|ν)xΩμ(x)logμ(x)ν(x)H(\mu|\nu)\geq\sum_{x\in\Omega}\mu(x)\log\frac{\mu(x)}{\nu(x)} by inserting f=1(xΩk)log(μ(x)/ν(x))f=1(x\in\Omega_{k})\log\big(\mu(x)/\nu(x)\big) into the variational formula for H(μ|ν)H(\mu|\nu), and then taking kk\uparrow\infty. Hence, μν\mu\ll\nu implies that H(μ|ν)=xΩμ(x)logμ(x)ν(x)H(\mu|\nu)=\sum_{x\in\Omega}\mu(x)\log\frac{\mu(x)}{\nu(x)}.

The second statement follows finiteness of Ω\Omega. ∎

4.2. Entropy with respect to Markov chains

Let ηt\eta_{t} be a continuous time Markov chain on a finite space Ω\Omega. Let π\pi be an invariant measure. Recall PtP_{t} and LL stand for the semigroup and generator of the process. We write in the following f,gμ:=Eμ[fg]\langle f,g\rangle_{\mu}:=E_{\mu}[fg].

Lemma 4.2.1.

For probability measures μ\mu such that μπ\mu\ll\pi, we have μPtπ\mu P_{t}\ll\pi, and H(μPt|π)H(μ|π)H(\mu P_{t}|\pi)\leq H(\mu|\pi) for t0t\geq 0.

Proof.

We show first that μPt\mu P_{t} is absolutely continuous with respect to π\pi, and therefore H(μPt|π)=xμPt(x)logμPt(x)π(x)H(\mu P_{t}|\pi)=\sum_{x}\mu P_{t}(x)\log\frac{\mu P_{t}(x)}{\pi(x)} by Lemma 4.1.4. As |Ω|<|\Omega|<\infty, and μπ\mu\ll\pi, we have maxxΩμ(x)/π(x)=C<\max_{x\in\Omega}\mu(x)/\pi(x)\ =\ C\ <\ \infty. Then, by the invariance xπ(x)Pt(x,y)=π(x)\sum_{x}\pi(x)P_{t}(x,y)=\pi(x), we conclude

μPt(y)=xΩμ(x)Pt(x,y)CxΩπ(x)Pt(x,y)=Cπ(x),\mu P_{t}(y)\ =\ \sum_{x\in\Omega}\mu(x)P_{t}(x,y)\ \leq\ C\sum_{x\in\Omega}\pi(x)P_{t}(x,y)\ =\ C\pi(x),

showing the absolute continuity.

Now, write H(μPt|π)H(\mu P_{t}|\pi) in form xπ(x)Φ(μPt(x)π(x))\sum_{x}\pi(x)\Phi\big(\frac{\mu P_{t}(x)}{\pi(x)}\big), where Φ(u)=ulogu\Phi(u)=u\log u is convex. Since

μPt(x)π(x)=zμ(z)π(z)π(z)Pt(z,x)π(x),\frac{\mu P_{t}(x)}{\pi(x)}=\sum_{z}\frac{\mu(z)}{\pi(z)}\frac{\pi(z)P_{t}(z,x)}{\pi(x)},

we have to finish,

xπ(x)Φ(μPt(x)π(x))xπ(x)zπ(z)Pt(z,x)π(x)Φ(μ(z)π(z))=H(μ|π).\sum_{x}\pi(x)\Phi\Big(\frac{\mu P_{t}(x)}{\pi(x)}\Big)\leq\sum_{x}\pi(x)\sum_{z}\frac{\pi(z)P_{t}(z,x)}{\pi(x)}\Phi\Big(\frac{\mu(z)}{\pi(z)}\Big)=H(\mu|\pi).\qed
Exercise 4.2.2.

One can update Lemma 4.2.1 to countable state space Ω\Omega by showing that μPtπ\mu P_{t}\ll\pi if μπ\mu\ll\pi. Perform this deduction when Ω\Omega is countable.

We now find the rate of decrease in the entropy.

Lemma 4.2.3.

Under the assumptions of Lemma 4.2.1, we have

ddtH(μPt|π)=dμPtdπ,LlogdμPtdππ.\frac{d}{dt}H(\mu P_{t}|\pi)\ =\ \Big\langle\frac{d\mu P_{t}}{d\pi},L\log\frac{d\mu P_{t}}{d\pi}\Big\rangle_{\pi}.
Proof.

Recall from the forward and backward equations that t(μPt(x))=μPtL(x)=μLPt(x)\partial_{t}(\mu P_{t}(x))=\mu P_{t}L(x)=\mu LP_{t}(x). Then, as there is no problem to interchange limits and sums in finite state space,

ddtxμPt(x)logμPt(x)π(x)\displaystyle\frac{d}{dt}\sum_{x}\mu P_{t}(x)\log\frac{\mu P_{t}(x)}{\pi(x)} =\displaystyle= xμPtL(x)logμPt(x)π(x)\displaystyle\sum_{x}\mu P_{t}L(x)\log\frac{\mu P_{t}(x)}{\pi(x)}
+xμPt(x)π(x)μPt(x)μLPt(x).\displaystyle\ +\ \sum_{x}\mu P_{t}(x)\frac{\pi(x)}{\mu P_{t}(x)}\mu LP_{t}(x).

The first term on the right-hand side equals

xzμPt(z)L(z,x)logμPt(x)π(x)\displaystyle\sum_{x}\sum_{z}\mu P_{t}(z)L(z,x)\log\frac{\mu P_{t}(x)}{\pi(x)} =\displaystyle= zμPt(z)(LlogμPtπ)(z)\displaystyle\sum_{z}\mu P_{t}(z)\Big(L\log\frac{\mu P_{t}}{\pi}\Big)(z)
=\displaystyle= dμPtdπ,LlogdμPtdππ\displaystyle\Big\langle\frac{d\mu P_{t}}{d\pi},L\log\frac{d\mu P_{t}}{d\pi}\Big\rangle_{\pi}

after interchanging the sum on zz and xx.

On the other hand, the second term vanishes:

xπ(x)zμ(z)LPt(z,x)=zμ(z)Eπ[Lgz]= 0.\sum_{x}\pi(x)\sum_{z}\mu(z)LP_{t}(z,x)\ =\ \sum_{z}\mu(z)E_{\pi}[Lg_{z}]\ =\ 0.

Here, gz=Pt(z,)g_{z}=P_{t}(z,\cdot) is a function on Ω\Omega for each zz, and so Eπ[Lgz]=0E_{\pi}[Lg_{z}]=0 given π\pi is invariant. ∎

4.2.1. Dirichlet forms

For a continuous time Markov process ηt\eta_{t} on a finite state space Ω\Omega with invariant measure π\pi, define the Dirichlet form on functions ff by

D(f)=f,Lfπ.D(f)\ =\ -\langle f,Lf\rangle_{\pi}.

We now define the adjoint L(x,y)L^{*}(x,y) by the relation π(x)L(x,y)=π(y)L(y,x)\pi(x)L(x,y)=\pi(y)L^{*}(y,x) for x,yΩx,y\in\Omega. Then, a simple computation shows

g,Lfπ=Lg,f.\langle g,Lf\rangle_{\pi}\ =\ \langle L^{*}g,f\rangle.

The operators S=(L+L)/2S=(L+L^{*})/2 and A=(LL)/2A=(L-L^{*})/2 may also be defined. If π\pi is reversible, L=L=SL=L^{*}=S. In particular, SS is a reversible operator, π(x)S(x,y)=π(y)S(y,x)\pi(x)S(x,y)=\pi(y)S(y,x), and AA is anti-symmetric in that π(x)A(x,y)=π(y)A(y,x)\pi(x)A(x,y)=-\pi(y)A(y,x) for all x,yΩx,y\in\Omega. Recall, also as we have seen before,

Lf(x)=yL(x,y)[f(y)f(x)].Lf(x)\ =\ \sum_{y}L(x,y)\big[f(y)-f(x)\big].

Then, by straightforward calculation, as also D(f)=Lf,fπD(f)=-\langle L^{*}f,f\rangle_{\pi},

D(f)\displaystyle D(f) =\displaystyle= x,yπ(x)f(x)L(x,y)[f(y)f(x)]\displaystyle-\sum_{x,y}\pi(x)f(x)L(x,y)\big[f(y)-f(x)\big]
=\displaystyle= x,yπ(x)f(x)L(x,y)[f(y)f(x)]\displaystyle-\sum_{x,y}\pi(x)f(x)L^{*}(x,y)\big[f(y)-f(x)\big]
=\displaystyle= x,yπ(x)f(x)S(x,y)[f(y)f(x)].\displaystyle-\sum_{x,y}\pi(x)f(x)S(x,y)\big[f(y)-f(x)\big].

Since SS is reversible, by interchanging xx and yy in the above sum and averaging the two expressions, we obtain the first of the following formulas. The second follows by anti-symmetry of AA.

Lemma 4.2.4.

We have

D(f)\displaystyle D(f) =\displaystyle= 12x,yπ(x)S(x,y)[f(y)f(x)]2\displaystyle\frac{1}{2}\sum_{x,y}\pi(x)S(x,y)\big[f(y)-f(x)\big]^{2} (4.2.1)
=\displaystyle= 12x,yπ(x)L(x,y)[f(y)f(x)]2.\displaystyle\frac{1}{2}\sum_{x,y}\pi(x)L(x,y)\big[f(y)-f(x)\big]^{2}.

We have the following properties of the Dirichlet form. For a nonnegative function, let I(f)=D(f)I(f)=D(\sqrt{f}).

Lemma 4.2.5.

We have fI(f)f\mapsto I(f) is nonnegative, convex, and lower semi-continuous. When the chain is irreducible and I(f)=0I(f)=0, then ff is a constant function.

Proof.

Nonnegativity follows from the expression (4.2.1). After squaring out terms, convexity follows by Jensen inequality applied to the crossterm. Clearly, the Dirichlet form is continuous, and therefore lower semi-continuous, in its argument as the space is finite.

When I(f)=0I(f)=0, we have (f(y)f(x))2=0(\sqrt{f}(y)-\sqrt{f}(x))^{2}=0 for all x,yx,y where S(x,y)>0S(x,y)>0. If the chain is irreducible, all values of ff must be the same. ∎

Remark 4.2.6.

Naturally, the above notions of Dirichlet form extend to countable state Markov chains, with respect to compactly supported functions ff, and to those in L2(π)L^{2}(\pi) in the domain of the generator LL.

4.2.2. Connection between entropy and Dirichlet form

Let ηt\eta_{t} be a continuous time finite space Markov chain with invariant measure π\pi. Recall in Lemma 4.2.3, that the derivative of H(μPt|π)H(\mu P_{t}|\pi) equals

dμPtdπ,LlogdμPtdππ.\Big\langle\frac{d\mu P_{t}}{d\pi},L\log\frac{d\mu P_{t}}{d\pi}\Big\rangle_{\pi}.

We now bound this expression in terms of the form I()I(\cdot).

Lemma 4.2.7.

We have

dμPtdπ,LlogdμPtdππ\displaystyle\Big\langle\frac{d\mu P_{t}}{d\pi},L\log\frac{d\mu P_{t}}{d\pi}\Big\rangle_{\pi} \displaystyle\leq 2D(dμPtdπ).\displaystyle-2D\Big(\sqrt{\frac{d\mu P_{t}}{d\pi}}\Big).
Proof.

The argument follows from an application of the inequality a(logbloga)2a(ba)a(\log b-\log a)\leq 2\sqrt{a}(\sqrt{b}-\sqrt{a}) for a,b0a,b\geq 0, which we leave to the reader. ∎

Remark 4.2.8.

We comment that the conclusion of Lemmas 4.2.3 and 4.2.7 may be compared with the more general Lemma 6.2.2, which bounds the derivative of relative entropy with a not necessarily invariant measure, given in Section 6.

4.3. Zero-range models

We now discuss the ‘zero-range’ system of interacting random walks on the dd-dimensional torus 𝕋Nd{\mathbb{T}}^{d}_{N} with NdN^{d} locations. Informally, particles interact infinitesimally only with those on their sites through their jump times, hence the name ‘zero-range’.

More specifically, at a vertex with kk particles, a particle displaces by yy with rate [g(k)/k]p(y)[g(k)/k]p(y) where again we assume p()p(\cdot) is a finite-range translation-invariant jump probability on 𝕋Nd{\mathbb{T}}^{d}_{N} and g:0+g:\mathbb{N}_{0}\rightarrow\mathbb{R}_{+} is a function such that g(0)=0g(0)=0 and g(k)>0g(k)>0 for k1k\geq 1. An alternate description is that each vertex has its own exponential clock which rings at rate g(k)g(k) when there are kk particles at the vertex. When rung, one of the kk particle is selected at random and then it displaces according to p()p(\cdot).

Formally, consider ηt={ηt(x):x𝕋Nd}\eta_{t}=\big\{\eta_{t}(x):x\in{\mathbb{T}}^{d}_{N}\big\} where ηt(x)0\eta_{t}(x)\in\mathbb{N}_{0} denotes the number of particles at xx at time t0t\geq 0. The process on the countable configuration space Ω=0TNd\Omega=\mathbb{N}_{0}^{T^{d}_{N}} is a continuous time Markov chain with semigroup PtP_{t} and generator

(Lf)(η)=x,yg(η(x))p(y)[f(ηx,y)f(η)](Lf)(\eta)\ =\ \sum_{x,y}g(\eta(x))p(y)\big[f(\eta^{x,y})-f(\eta)\big] (4.3.1)

where ηx,y\eta^{x,y} is the configuration obtained from η\eta by moving a particle from xx to yy:

ηx,y(z)={η(x)1whenz=xη(y)+1whenz=yη(z)otherwise.\eta^{x,y}(z)\ =\ \left\{\begin{array}[]{rl}\eta(x)-1&\ {\rm when\ }z=x\\ \eta(y)+1&\ {\rm when\ }z=y\\ \eta(z)&{\rm\ otherwise.}\end{array}\right.

4.3.1. Invariant measures

As with the exclusion process, there is an associated family of invariant measures depending on particle density. Let ν¯ΨN=x𝕋NdκΨ\bar{\nu}^{N}_{\Psi}=\prod_{x\in{\mathbb{T}}_{N}^{d}}\kappa_{\Psi} be the product measure with common marginal on 0\mathbb{N}_{0} given by

κΨ(k)={1Z(Ψ)Ψkg(1)g(k)whenk11Z(Ψ)whenk=0.\kappa_{\Psi}(k)\ =\ \left\{\begin{array}[]{rl}\frac{1}{Z(\Psi)}\frac{\Psi^{k}}{g(1)\cdots g(k)}&\ {\rm when\ }k\geq 1\\ \frac{1}{Z(\Psi)}&\ {\rm when\ }k=0.\end{array}\right.

Here, Z(Ψ)Z(\Psi) is the normalization which converges for 0Ψ<lim infg(k)0\leq\Psi<\liminf g(k).

An interesting point is that when g(k)kg(k)\equiv k, this is the model of ‘independent’ random walks considered in Section 1 when there is no interaction. In this case, of course κ\kappa are Poisson measures.

We now index the family in terms of ‘density’. Let ρ(Ψ)\rho(\Psi) be the density, Eν¯ΨN[η(0)]=ρ(Ψ)E_{\bar{\nu}^{N}_{\Psi}}[\eta(0)]=\rho(\Psi). One can check that the function Ψρ(Ψ)\Psi\mapsto\rho(\Psi) is a strictly increasing function which may or may not diverge when Ψlim infg(k)\Psi\uparrow\liminf g(k), depending on the structure of gg. In any case, for 0Ψ<lim infg(k)0\leq\Psi<\liminf g(k) we can invert ρ(Ψ)\rho(\Psi) and define

νρN:=ν¯Ψ(ρ)N,\nu^{N}_{\rho}\ :=\ \bar{\nu}^{N}_{\Psi(\rho)},

the product measure which places a mean ρ\rho number of particles at each location in 𝕋Nd{\mathbb{T}}_{N}^{d}. The term Ψ(ρ)\Psi(\rho) is sometimes called a ‘fugacity’ or ‘chemical potential’. One may calculate that is also the mean of the rate function: EνρN[g(η(0))]=Ψ(ρ)E_{\nu^{N}_{\rho}}[g(\eta(0))]=\Psi(\rho). In the following, we drop the superscript ‘NN’ and write νρ=νρN\nu_{\rho}=\nu^{N}_{\rho} to simplify notation.

Exercise 4.3.1.

For bounded, local ff, that is ff supported only on a finite number of variables {η(x):x𝕋Nd}\{\eta(x):x\in{\mathbb{T}}^{d}_{N}\}, show

Eνρ[g(η(x))f(ηx,y)]=Ψ(ρ)Eνρ[f(η+δy)]=Eνρ[g(η(y))f(η)]E_{\nu_{\rho}}\big[g(\eta(x))f(\eta^{x,y})\big]=\Psi(\rho)E_{\nu_{\rho}}\big[f(\eta+\delta_{y})\big]=E_{\nu_{\rho}}\big[g(\eta(y))f(\eta)\big]

where ηx,y=ηδx+δy\eta^{x,y}=\eta-\delta_{x}+\delta_{y} and δz\delta_{z} is the configuration with exactly one particle at zz.

Lemma 4.3.2.

Let ρ\rho be such that Ψ(ρ)<lim infg(k)\Psi(\rho)<\liminf g(k). Then, νρ\nu_{\rho} is an invariant measure for process on 𝕋Nd{\mathbb{T}}_{N}^{d}.

Moreover, νN,K:=νρ(|x𝕋Ndη(x)=K)\nu_{N,K}:=\nu_{\rho}\big(\cdot|\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta(x)=K\big) does not depend on ρ\rho and is the unique invariant measure on ΩK={η:x𝕋Ndη(x)=K}\Omega_{K}=\big\{\eta:\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta(x)=K\big\} when p()p(\cdot) is irreducible.

Proof.

Recall the expression for Lf(η)Lf(\eta) in (4.3.1). We need only show that Eνρ[Lf(η)]=0E_{\nu_{\rho}}[Lf(\eta)]=0 for all bounded local functions ff. Since p(x,y)=p(yx)p(x,y)=p(y-x) is translation-invariant, it is doubly stochastic, x𝕋Ndp(x,y)=y𝕋Ndp(x,y)=1\sum_{x\in{\mathbb{T}}_{N}^{d}}p(x,y)=\sum_{y\in{\mathbb{T}}_{N}^{d}}p(x,y)=1.

Noting Exercise 4.3.1, we have

x,y𝕋Ndp(x,y)Eνρ[g(η(x))f(ηx,y)]\displaystyle\sum_{x,y\in{\mathbb{T}}_{N}^{d}}p(x,y)E_{\nu_{\rho}}\big[g(\eta(x))f(\eta^{x,y})\big] =x,y𝕋Ndp(x,y)Eνρ[g(η(y))f(η)]\displaystyle=\sum_{x,y\in{\mathbb{T}}_{N}^{d}}p(x,y)E_{\nu_{\rho}}\big[g(\eta(y))f(\eta)\big]
=y𝕋NdEνρ[g(η(y))f(η)].\displaystyle=\sum_{y\in{\mathbb{T}}_{N}^{d}}E_{\nu_{\rho}}\big[g(\eta(y))f(\eta)\big].

But, also, x,y𝕋Ndp(x,y)Eνρ[g(η(x))f(η)]=x𝕋NdEνρ[g(η(x))f(η)]\sum_{x,y\in{\mathbb{T}}_{N}^{d}}p(x,y)E_{\nu_{\rho}}\big[g(\eta(x))f(\eta)\big]=\sum_{x\in{\mathbb{T}}_{N}^{d}}E_{\nu_{\rho}}\big[g(\eta(x))f(\eta)\big]. Hence, Eνρ[Lf]=0E_{\nu_{\rho}}[Lf]=0.

The second statement for νN,K\nu_{N,K}, the restriction of νρ\nu_{\rho} to ΩK\Omega_{K}, as for independent particles, follows by noting ΩK\Omega_{K} is a closed, irreducible set when p()p(\cdot) is irreducible. ∎

Local equilibrium. In the following, with respect to a continuous nonnegative function ρ0:𝕋d[0,Ψ1(lim infg(k)))\rho_{0}:{\mathbb{T}}^{d}\rightarrow\big[0,\Psi^{-1}(\liminf g(k))\big), define

νρ0()N=x𝕋NdκΨ(ρ0(x/N))\nu^{N}_{\rho_{0}(\cdot)}=\prod_{x\in{\mathbb{T}}_{N}^{d}}\kappa_{\Psi(\rho_{0}(x/N))}

to be the (inhomogeneous) product measure with marginals κΨ(ρ0(x/N))\kappa_{\Psi(\rho_{0}(x/N))} over sites x𝕋Ndx\in{\mathbb{T}}^{d}_{N}. Sometimes νρ0()N\nu^{N}_{\rho_{0}(\cdot)} is referred to as a ‘local equilibrium’ measure. Again, we will drop the superscript ‘NN’ and write νρ0()=νρ0()N\nu_{\rho_{0}(\cdot)}=\nu^{N}_{\rho_{0}(\cdot)} to simplify notation.

Remark 4.3.3.

We comment that divergence of ρ(Ψ)\rho(\Psi) as Ψlim infg(k)\Psi\uparrow\liminf g(k) allows to define νρ\nu_{\rho} and νρ0()\nu_{\rho_{0}(\cdot)} for any 0ρ<0\leq\rho<\infty and ρ0:𝕋d[0,)\rho_{0}:{\mathbb{T}}^{d}\rightarrow[0,\infty), useful in the formulation of the hydrodynamic limit.

A sufficient condition is that Z(Ψ)Z(\Psi) diverges as Ψlim infg(k)\Psi\uparrow\liminf g(k). This is the case when gg is an increasing function. See Lemma II.3.3 and Section II.3 in [130] for an argument and more discussion.

Exercise 4.3.4.

Suppose g(k)=1(k1)g(k)=1(k\geq 1). Then, lim infg(k)=limg(k)=1\liminf g(k)=\lim g(k)=1. By explicit calculation, show that ρ(Ψ)\rho(\Psi) diverges as Ψ1\Psi\uparrow 1.

4.3.2. Connection with entropy

The next results will be used to bound a certain ‘entropy production’, discussed in Section 5, when starting from νρ0()\nu_{\rho_{0}(\cdot)}. Since here Ω=0𝕋Nd\Omega=\mathbb{N}_{0}^{{\mathbb{T}}_{N}^{d}} is countable but not finite, we now update the results in Subsection 4.2 to this context.

Lemma 4.3.5.

Consider ρ>0\rho>0 and ρ¯=ρ0()\bar{\rho}=\|\rho_{0}(\cdot)\|_{\infty} such that Ψ(ρ),Ψ(ρ¯)<lim infg(k)\Psi(\rho),\Psi(\bar{\rho})<\liminf g(k). Then, νρ0()νρ\nu_{\rho_{0}(\cdot)}\ll\nu_{\rho}, and H(νρ0()Pt|νρ)H(νρ0()|νρ)=O(Nd)H(\nu_{\rho_{0}(\cdot)}P_{t}|\nu_{\rho})\leq H(\nu_{\rho_{0}(\cdot)}|\nu_{\rho})=O(N^{d}) for t0t\geq 0.

Proof.

The absolute continuity follows as νρ(η)>0\nu_{\rho}(\eta)>0 for all ηΩ\eta\in\Omega. The bound H(νρ0()Pt|νρ)H(νρ0()|νρ)H(\nu_{\rho_{0}(\cdot)}P_{t}|\nu_{\rho})\leq H(\nu_{\rho_{0}(\cdot)}|\nu_{\rho}) follows by the proof of Lemma 4.2.1 and Exercise 4.2.2. The last part is left as an exercise. ∎

Exercise 4.3.6.

Prove H(νρ0()|νρ)=O(Nd)H(\nu_{\rho_{0}(\cdot)}|\nu_{\rho})=O(N^{d}) by explicit calculation when ρ=ρ¯=ρ0()\rho=\bar{\rho}=\|\rho_{0}(\cdot)\|_{\infty}. Update to other densities ρ>0\rho>0, by use of the entropy inequality in Lemma 4.1.2 with α=α(ρ,ρ¯)>0\alpha=\alpha(\rho,\bar{\rho})>0 chosen small. Hint: See Remark V.1.2 in [130].

Extend the definition of I()I(\cdot) with respect to (4.2.1) in the current setting:

I(h)=DK(h)=12x,yp(x,y)EνN,K[g(η(x))(h(ηx,y)h(η))2].I(h)=D_{K}\big(\sqrt{h}\big)=\frac{1}{2}\sum_{x,y}p(x,y)E_{\nu_{N,K}}\Big[g(\eta(x))\big(\sqrt{h(\eta^{x,y})}-\sqrt{h(\eta)}\big)^{2}\Big]. (4.3.2)
Lemma 4.3.7.

Under the assumptions of Lemma 4.3.5, we have, for 0rt0\leq r\leq t,

H(νρ0()Pt|νρ)H(νρ0()Pr|νρ)\displaystyle H(\nu_{\rho_{0}(\cdot)}P_{t}|\nu_{\rho})-H(\nu_{\rho_{0}(\cdot)}P_{r}|\nu_{\rho}) =rtdνρ0()Psdνρ,Llogdνρ0()Psdνρνρ𝑑s\displaystyle=\int_{r}^{t}\Big\langle\frac{d\nu_{\rho_{0}(\cdot)}P_{s}}{d\nu_{\rho}},L\log\frac{d\nu_{\rho_{0}(\cdot)}P_{s}}{d\nu_{\rho}}\Big\rangle_{\nu_{\rho}}ds
2rtI(dνρ0()Psdνρ)ds.\displaystyle\leq-2\int_{r}^{t}I\Big(\sqrt{\frac{d\nu_{\rho_{0}(\cdot)}P_{s}}{d\nu_{\rho}}}\Big)ds.
Proof.

By Lemma 4.3.5, νρ0()νρ\nu_{\rho_{0}(\cdot)}\ll\nu_{\rho} and therefore by Lemma 4.1.4, we may write

H(νρ0()Pt|νρ)=ηνρ0()(η)logft(η)<H(\nu_{\rho_{0}(\cdot)}P_{t}|\nu_{\rho})=\sum_{\eta}\nu_{\rho_{0}(\cdot)}(\eta)\log f_{t}(\eta)<\infty

where ft(η)=νρ0()Pt(η)/νρ(η)f_{t}(\eta)={\nu_{\rho_{0}(\cdot)}P_{t}(\eta)}/{\nu_{\rho}(\eta)} for each t0t\geq 0. Decomposing on the number of particles in 𝕋Nd{\mathbb{T}}_{N}^{d}, the entropy H(νρ0()Pt|νρ)H(\nu_{\rho_{0}(\cdot)}P_{t}|\nu_{\rho}) equals

Kνρ(ΩK)ηΩKνN,K(η)ft(η)logft(η)=Kνρ(ΩK)EνN,K[ftlogft].\sum_{K}\nu_{\rho}(\Omega_{K})\sum_{\eta\in\Omega_{K}}\nu_{N,K}(\eta)f_{t}(\eta)\log f_{t}(\eta)=\sum_{K}\nu_{\rho}(\Omega_{K})E_{\nu_{N,K}}\big[f_{t}\log f_{t}\big].

Recall, here ΩK={η:xη(x)=K}\Omega_{K}=\{\eta:\sum_{x}\eta(x)=K\} is a finite set, and νN,K()=νρ(|ΩK)\nu_{N,K}(\cdot)=\nu_{\rho}(\cdot|\Omega_{K}). Let also νρ0,K()=νρ0()(|ΩK)\nu_{\rho_{0},K}(\cdot)=\nu_{\rho_{0}(\cdot)}(\cdot|\Omega_{K}) and ft,K(η)=νρ0,KPt(η)/νN,K(η)f_{t,K}(\eta)=\nu_{\rho_{0},K}P_{t}(\eta)/\nu_{N,K}(\eta).

On ΩK\Omega_{K}, note by mass conservation that νρ0()Pt(η)=νρ0()(ΩK)νρ0,KPt(η)\nu_{\rho_{0}(\cdot)}P_{t}(\eta)=\nu_{\rho_{0}(\cdot)}(\Omega_{K})\nu_{\rho_{0},K}P_{t}(\eta). Then, on ΩK\Omega_{K}, ft(η)=νρ0()(ΩK)νρ(ΩK)ft,K(η)f_{t}(\eta)=\frac{\nu_{\rho_{0}(\cdot)}(\Omega_{K})}{\nu_{\rho}(\Omega_{K})}f_{t,K}(\eta). Therefore, inputting these relations,

EνN,K[ftlogft]\displaystyle E_{\nu_{N,K}}\big[f_{t}\log f_{t}\big] =νρ0()(ΩK)νρ(ΩK)logνρ0()(ΩK)νρ(ΩK)+νρ0()(ΩK)νρ(ΩK)EνN,K[ft,Klogft,K].\displaystyle=\frac{\nu_{\rho_{0}(\cdot)}(\Omega_{K})}{\nu_{\rho}(\Omega_{K})}\log\frac{\nu_{\rho_{0}(\cdot)}(\Omega_{K})}{\nu_{\rho}(\Omega_{K})}+\frac{\nu_{\rho_{0}(\cdot)}(\Omega_{K})}{\nu_{\rho}(\Omega_{K})}E_{\nu_{N,K}}\big[f_{t,K}\log f_{t,K}\big].

Since Kνρ(Ω)[νρ0()(ΩK)νρ(ΩK)logνρ0()(ΩK)νρ(ΩK)]\sum_{K}\nu_{\rho}(\Omega)\big[\frac{\nu_{\rho_{0}(\cdot)}(\Omega_{K})}{\nu_{\rho}(\Omega_{K})}\log\frac{\nu_{\rho_{0}(\cdot)}(\Omega_{K})}{\nu_{\rho}(\Omega_{K})}\big] is itself a relative entropy of the measures μ1(K)=νρ0()(ΩK)\mu_{1}(K)=\nu_{\rho_{0}(\cdot)}(\Omega_{K}) and μ2(K)=νρ(ΩK)\mu_{2}(K)=\nu_{\rho}(\Omega_{K}) on 0\mathbb{N}_{0}, it is nonnegative. Also, the relative entropy EνN,K[ft,Klogft,K]0E_{\nu_{N,K}}\big[f_{t,K}\log f_{t,K}\big]\geq 0 for each K0K\geq 0. Note also that EνN,K[ftlogft]E_{\nu_{N,K}}\big[f_{t}\log f_{t}\big], as ΩK\Omega_{K} is a finite space, is differentiable.

Hence, given finiteness of H(νρ0()Pt|νρ)H(\nu_{\rho_{0}(\cdot)}P_{t}|\nu_{\rho}), we may write it as a sum of two finite, nonnegative terms, one of which, H(μ1|μ2)H(\mu_{1}|\mu_{2}), does not depend on tt. Therefore, we are able to write the difference

H(νρ0()Pt|νρ)H(νρ0()Pr|νρ)\displaystyle H(\nu_{\rho_{0}(\cdot)}P_{t}|\nu_{\rho})-H(\nu_{\rho_{0}(\cdot)}P_{r}|\nu_{\rho}) =Kνρ(ΩK)rtsEνN,K[fslogfs]𝑑s.\displaystyle=\sum_{K}\nu_{\rho}(\Omega_{K})\int_{r}^{t}\partial_{s}E_{\nu_{N,K}}\big[f_{s}\log f_{s}\big]ds.

The right-hand side, by the arguments of Lemmas 4.2.3 and 4.2.7, since νN,K\nu_{N,K} is an invariant measure on ΩK\Omega_{K}, is evaluated as

Kνρ(ΩK)rtEνN,K[fsLlogfs]𝑑s\displaystyle\sum_{K}\nu_{\rho}(\Omega_{K})\int_{r}^{t}E_{\nu_{N,K}}\big[f_{s}L\log f_{s}\big]ds 2Kνρ(ΩK)rtDK(fs)ds.\displaystyle\leq-2\sum_{K}\nu_{\rho}(\Omega_{K})\int_{r}^{t}D_{K}\big(\sqrt{f_{s}}\big)ds.

Since the summands, as DK()0D_{K}(\cdot)\geq 0, are all negative, we may interchange the sum on KK and the integral. The right-hand side above equals rt2D(fs)ds\int_{r}^{t}-2D\big(\sqrt{f_{s}}\big)ds. We obtain the desired statement as I(fs)=D(fs)I(f_{s})=D\big(\sqrt{f_{s}}\big). ∎

Remark 4.3.8.

Since PtP_{t} and so ftf_{t} is continuous in tt, by Fatou’s lemma, one may bound the upper derivative:

lim supδ01δ[H(νρ0()Pt+δ|νρ)H(νρ0()Pt|νρ)]2I(ft).\limsup_{\delta\downarrow 0}\frac{1}{\delta}\big[H(\nu_{\rho_{0}(\cdot)}P_{t+\delta}|\nu_{\rho})-H(\nu_{\rho_{0}(\cdot)}P_{t}|\nu_{\rho})\big]\leq-2I\big(\sqrt{f_{t}}\big).

See also discussion in Appendix I.1.9 in [130].

4.4. Basic coupling

We discuss a useful coupling in the context of zero-range processes when gg is an increasing function. First, we define the notion of ‘stochastic domination’ on the partially ordered set Ω\Omega. We say two probability measures μ1\mu_{1}, μ2\mu_{2} on a countable set Ω\Omega are ordered, μ1μ2\mu_{1}\ll\mu_{2}, if Eμ1[f]Eμ2[f]E_{\mu_{1}}[f]\leq E_{\mu_{2}}[f] for all coordinatewise increasing functions f:Ωf:\Omega\rightarrow\mathbb{R}.

There is an interesting characterization of ordered measures for whose proof we refer to [147][Theorem II.2.4].

Proposition 4.4.1.

We have μ1μ2\mu_{1}\ll\mu_{2} exactly when there is a bivariate distribution on Ω×Ω\Omega\times\Omega such that marginally variables η\eta and ξ\xi are distributed according to μ1\mu_{1} and μ2\mu_{2} and P(ηξ)=1P(\eta\leq\xi)=1.

In this next result, gg does not have to be increasing.

Lemma 4.4.2.

Let α,β<lim infg(k)\alpha,\beta<\liminf g(k). The marginals κακβ\kappa_{\alpha}\ll\kappa_{\beta} exactly when αβ\alpha\leq\beta.

Proof.

If κακβ\kappa_{\alpha}\ll\kappa_{\beta}, since f(η)=η(0)f(\eta)=\eta(0) is increasing, we have ρ(α)ρ(β)\rho(\alpha)\leq\rho(\beta) from which one deduces αβ\alpha\leq\beta.

For the converse, since linear combinations of 1(η[L,))1(\eta\in[L,\infty)) are dense in the set of increasing functions, it is enough to show that

Pκβ(ηL)Pκα(ηL)P_{\kappa_{\beta}}(\eta\geq L)\ \geq\ P_{\kappa_{\alpha}}(\eta\geq L)

for all L0L\geq 0. This is equivalent, after cancellation, to showing

kLβkg(1)g(k)Z(α)kLαkg(1)g(k)Z(β)\sum_{k\geq L}\frac{\beta^{k}}{g(1)\cdots g(k)}Z(\alpha)\ \geq\ \sum_{k\geq L}\frac{\alpha^{k}}{g(1)\cdots g(k)}Z(\beta)

which is equivalent to

kLL1βkαg(k)!g()!kLL1αkβg(k)!g()!.\sum_{k\geq L}\sum_{\ell\leq L-1}\frac{\beta^{k}\alpha^{\ell}}{g(k)!g(\ell)!}\ \geq\ \sum_{k\geq L}\sum_{\ell\leq L-1}\frac{\alpha^{k}\beta^{\ell}}{g(k)!g(\ell)!}.

The last inequality will be shown if term by term the inequality is true. But, βkααkβ\beta^{k}\alpha^{\ell}\geq\alpha^{k}\beta^{\ell} since kk\geq\ell.∎

We now show the existence of the so-called ‘basic coupling’ for the zero-range process when gg is increasing. Another name for such an existence is that the zero-range process is ‘attractive’.

Proposition 4.4.3.

When gg is increasing, there is a joint process (ηt,ξt)(\eta_{t},\xi_{t}) on Ω×Ω\Omega\times\Omega, starting from μ1×μ2\mu_{1}\times\mu_{2} where μ1μ2\mu_{1}\ll\mu_{2}, such that at all later times t0t\geq 0, ηt\eta_{t} and ξt\xi_{t} marginally are the zero-range processes starting from μ1\mu_{1} and μ2\mu_{2} respectively and ηtξt\eta_{t}\leq\xi_{t} a.s.

Proof.

Let μ¯=μ1×μ2\bar{\mu}=\mu_{1}\times\mu_{2} be the joint probability on Ω×Ω\Omega\times\Omega such that η0ξ0\eta_{0}\leq\xi_{0} a.s. (Proposition 4.4.1). Consider the Markov process on Ω×Ω\Omega\times\Omega with initial distribution μ¯\bar{\mu} and generator

(L¯N)f(η,ξ)\displaystyle(\bar{L}_{N})f(\eta,\xi) =\displaystyle= x,y𝕋Ndp(y)min{g(η(x)),g(ξ(x))}[f(ηx,x+y,ξx,x+y)f]\displaystyle\sum_{x,y\in{\mathbb{T}}^{d}_{N}}p(y)\min\{g(\eta(x)),g(\xi(x))\}\big[f(\eta^{x,x+y},\xi^{x,x+y})-f\big]
+x,y𝕋Ndp(y)(g(η(x))g(ξ(x)))+[f(ηx,x+y,ξ)f]\displaystyle\ +\ \sum_{x,y\in{\mathbb{T}}^{d}_{N}}p(y)\big(g(\eta(x))-g(\xi(x))\big)_{+}\big[f(\eta^{x,x+y},\xi)-f\big]
+x,y𝕋Ndp(y)(g(ξ(x))g(η(x)))+[f(η,ξx,x+y)f].\displaystyle\ +\ \sum_{x,y\in{\mathbb{T}}^{d}_{N}}p(y)\big(g(\xi(x))-g(\eta(x))\big)_{+}\big[f(\eta,\xi^{x,x+y})-f\big].

One can see, by inserting a function of coordinate η\eta only or of coordinate ξ\xi only, that the marginal processes are as desired.

To check that ηtξt\eta_{t}\leq\xi_{t} a.s., recall the joint process is a continuous time Markov chain on a countable state space. At time t=0t=0, we have arranged that η0ξ0\eta_{0}\leq\xi_{0}. At the next jump time τ\tau, by the specification of the rates, we see that still ητξτ\eta_{\tau}\leq\xi_{\tau}. Hence, the joint process remains ordered for all time t0t\geq 0. ∎

Exercise 4.4.4.

There is another way to show that ηtξt\eta_{t}\leq\xi_{t} for all t0t\geq 0 a.s. (cf. Theorem II.5.2 in [130]). Compute that L¯N1(ηξ)0\bar{L}_{N}1(\eta\leq\xi)\geq 0. Then, with E¯μ¯\bar{E}_{\bar{\mu}} denoting the process expectation starting from μ¯\bar{\mu}, E¯μ¯[1(ηtξt)]\bar{E}_{\bar{\mu}}[1(\eta_{t}\leq\xi_{t})] is increasing in tt: tE¯μ¯[1(ηtξt)]=E¯μ¯[L¯N1(ηtξt)]0\partial_{t}\bar{E}_{\bar{\mu}}[1(\eta_{t}\leq\xi_{t})]=\bar{E}_{\bar{\mu}}[\bar{L}_{N}1(\eta_{t}\leq\xi_{t})]\geq 0. Hence,

1E¯μ¯[1(ηtξt)]E¯μ¯[1(η0ξ0)]= 1.1\geq\bar{E}_{\bar{\mu}}[1(\eta_{t}\leq\xi_{t})]\ \geq\ \bar{E}_{\bar{\mu}}[1(\eta_{0}\leq\xi_{0})]\ =\ 1.

The next exercise will be useful in the later proof of hydrodynamics. Recall that νρ\nu_{\rho} and νρ0()\nu_{\rho_{0}(\cdot)} are well-defined when gg is increasing by Remark 4.3.3.

Exercise 4.4.5.

Let ρ¯=ρ0()\bar{\rho}=\|\rho_{0}(\cdot)\|_{\infty}. Show that νρ0()νρ¯\nu_{\rho_{0}(\cdot)}\ll\nu_{\bar{\rho}}, and consequently νρ0()νρ¯\mathbb{P}_{\nu_{\rho_{0}(\cdot)}}\ll\mathbb{P}_{\nu_{\bar{\rho}}}, when gg is increasing.

We will also need later an estimate on Ψ(ρ)=Eνρ[g(η(0))]\Psi(\rho)=E_{\nu_{\rho}}[g(\eta(0))] if gg is a Lipschitz function, |g(k)g(l)|C|kl||g(k)-g(l)|\leq C|k-l| for all k,l0k,l\geq 0.

Lemma 4.4.6.

If gg is Lipschitz, then Ψ\Psi is also Lipschitz.

Proof.

Let δβ\delta\geq\beta. Then, by the basic coupling,

Ψ(δ)Ψ(β)\displaystyle\Psi(\delta)-\Psi(\beta) =Eνδ[g]Eνβ[g]\displaystyle=E_{\nu_{\delta}}[g]-E_{\nu_{\beta}}[g]
=E¯[g(η(0))g(ξ(0))]\displaystyle=\bar{E}[g(\eta(0))-g(\xi(0))]
E¯[|η(0)ξ(0)|]\displaystyle\leq\bar{E}\big[|\eta(0)-\xi(0)|\big]
=E¯[η(0)ξ(0)]=δβ.\displaystyle=\bar{E}[\eta(0)-\xi(0)]\ =\ \delta-\beta.\qed

As we have seen, the zero-range model allows several ‘closed form’ calculations. The following is another one of these. We will not use this exercise in the sequel.

Exercise 4.4.7.

Calculate that Ψ(ρ)=Ψ(ρ)/σ2(ρ)\Psi^{\prime}(\rho)=\Psi(\rho)/\sigma^{2}(\rho) where σ2(ρ)\sigma^{2}(\rho) is the variance of η(0)\eta(0) under νρ\nu_{\rho}.

4.5. What is the hydrodynamical equation?

We will start the process from initial configurations distributed according to μN=νρ0()\mu^{N}=\nu_{\rho_{0}(\cdot)}. Denote, as before, for fixed T<T<\infty, that νρ0()\mathbb{P}_{\nu_{\rho_{0}(\cdot)}} and 𝔼νρ0()\mathbb{E}_{\nu_{\rho_{0}(\cdot)}} are the distribution of {ηt:t[0,T]}\{\eta_{t}:t\in[0,T]\} and its expectation, when η0\eta_{0} is governed by μ\mu.

We now informally compute the generator action to guess the hydrodynamic behavior. Recall πtN\pi^{N}_{t} stands for the empirical measure

πtN=1Ndx𝕋Ndηt(x)δx/N.\pi^{N}_{t}\ =\ \frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}\eta_{t}(x)\delta_{x/N}.

For a smooth G:𝕋dG:{\mathbb{T}}^{d}\rightarrow\mathbb{R}, consider the equation

G,πv(N)tN=G,π0N+v(N)0tLG,πv(N)sN𝑑s+MtN(G)\langle G,\pi^{N}_{v(N)t}\rangle\ =\ \langle G,\pi^{N}_{0}\rangle+v(N)\int_{0}^{t}L\langle G,\pi^{N}_{v(N)s}\rangle ds+M^{N}_{t}(G)

where MtN(G)M^{N}_{t}(G) is a martingale. One may compute the quadratic variation,

MN(G)t=v(N)0t[L(G,πv(N)sN)22G,πv(N)tNLG,πv(N)sN]𝑑s\displaystyle\langle M^{N}(G)\rangle_{t}=v(N)\int_{0}^{t}\Big[L\big(\langle G,\pi^{N}_{v(N)s}\rangle\big)^{2}-2\langle G,\pi^{N}_{v(N)t}\rangle L\langle G,\pi^{N}_{v(N)s}\rangle\Big]ds
=v(N)N2d+20tx,y(x,x+yNG)2g(ηv(N)s(x))p(y)𝑑s=O(v(N)tNd2),\displaystyle\quad=\frac{v(N)}{N^{2d+2}}\int_{0}^{t}\sum_{x,y}\big(\nabla^{N}_{x,x+y}G\big)^{2}g(\eta_{v(N)s}(x))p(y)ds=O(v(N)tN^{-d-2}),

which shows, easily if gg is bounded, that the martingale is negligible in the limit.

We now compute

v(N)LG,πv(N)tN\displaystyle v(N)L\langle G,\pi^{N}_{v(N)t}\rangle =\displaystyle= v(N)Nd+1x,yg(η(x))p(y)[N(G(x+y/N)G(x/N))].\displaystyle\frac{v(N)}{N^{d+1}}\sum_{x,y}g(\eta(x))p(y)\big[N(G(x+y/N)-G(x/N))\big].

Here, again v(N)=N2v(N)=N^{2} when pp is symmetric (or mean-zero), and v(N)=Nv(N)=N otherwise.

When pp is symmetric, similar to symmetric exclusion, one can change yy to y-y and average. The right-side equals

v(N)2Nd+2x,yg(η(x))p(y)x,yNG.\displaystyle\frac{v(N)}{2N^{d+2}}\sum_{x,y}g(\eta(x))p(y)\triangle^{N}_{x,y}G.

where we recall x,yNG=N2[G(x+y/N)2G(x/N)+G(xy/N)]\triangle^{N}_{x,y}G=N^{2}[G(x+y/N)-2G(x/N)+G(x-y/N)].

The trouble now is that this weighted average of functions g(η(x))g(\eta(x)) does not close in terms of the empirical measure. The main point of ‘hydrodynamics’ is to approximate this average by a function of the empirical measure.

What should it be? In the microscopic scale, near point x𝕋Ndx\in{\mathbb{T}}^{d}_{N} there is lots of local particle movement. One expects the distribution of particles in an NϵN\epsilon neighborhood of xx at time N2tN^{2}t to be in ‘local’ equilibrium given by the nearby density, such as νηN2tNϵ(x)\nu_{\eta_{N^{2}t}^{N\epsilon}(x)} where

η(x)=1(2+1)d|yx|η(x)\eta^{\ell}(x)=\frac{1}{(2\ell+1)^{d}}\sum_{|y-x|\leq\ell}\eta(x) (4.5.1)

and ϵ>0\epsilon>0 is a small parameter.

Then, one might expect that

v(N)2Nd+2x,yg(η(x))p(y)x,x+yNG12Ndx,yΨ(ηN2tNϵ(x))p(y)x,x+yNG\frac{v(N)}{2N^{d+2}}\sum_{x,y}g(\eta(x))p(y)\triangle^{N}_{x,x+y}G\ \sim\ \frac{1}{2N^{d}}\sum_{x,y}\Psi\big(\eta_{N^{2}t}^{N\epsilon}(x)\big)p(y)\triangle^{N}_{x,x+y}G

where we recall Ψ(ρ)=Eνρ[g(η(0))]\Psi(\rho)=E_{\nu_{\rho}}[g(\eta(0))].

Now, this ‘local’ density, for ϵ>0\epsilon>0, can be re-expressed in terms of the empirical measure:

ηN2tNϵ(x)=(2ϵ)dNd(2Nϵ+1)d(2ϵ)d1([x/Nϵ,x/N+ϵ]d),πN2tN\eta^{N\epsilon}_{N^{2}t}(x)\ =\ \frac{(2\epsilon)^{d}N^{d}}{(2N\epsilon+1)^{d}}\big\langle(2\epsilon)^{-d}1([x/N-\epsilon,x/N+\epsilon]^{d}),\pi^{N}_{N^{2}t}\big\rangle (4.5.2)

which if πN2tN(x)π(t,u)du\pi^{N}_{N^{2}t}(x)\sim\pi(t,u)du is further approximated by

1(2ϵ)d1[ϵ,ϵ]d(ux/N)π(t,u)𝑑u.\frac{1}{(2\epsilon)^{d}}\int 1_{[-\epsilon,\epsilon]^{d}}(u-x/N)\pi(t,u)du.

Putting this together, one ‘closes’ the equation and obtains, after first NN\uparrow\infty and then ϵ0\epsilon\downarrow 0, that

𝕋dG(u)π(t,u)𝑑u=𝕋dG(u)ρ0(u)𝑑u+120tCG(u)Ψ(π(t,u))𝑑u\int_{{\mathbb{T}}^{d}}G(u)\pi(t,u)du\ =\ \int_{{\mathbb{T}}^{d}}G(u)\rho_{0}(u)du+\frac{1}{2}\int_{0}^{t}\triangle_{C}G(u)\Psi(\pi(t,u))du

which is the weak formulation of

tρ(t,u)=12CΨ(ρ(t,u))andρ(0,u)=ρ0(u)\partial_{t}\rho(t,u)\ =\ \frac{1}{2}\triangle_{C}\Psi\big(\rho(t,u)\big)\ \ \ {\rm and\ \ \ }\rho(0,u)=\rho_{0}(u)

where C\triangle_{C} is as defined before, C=ii,jdCi,j2xixj\triangle_{C}=\sum_{i\leq i,j\leq d}C_{i,j}\frac{\partial^{2}}{\partial_{x_{i}}\partial_{x_{j}}} and Ci,j=zzizjp(z)C_{i,j}=\sum_{z}z_{i}z_{j}p(z).

4.6. Assumptions and statement of hydrodynamics

We will make the following assumptions to help simplify the proof and introduce main ideas. We remark however that hydrodynamics has been shown for much more general zero-range processes; see the later Notes for details on extensions.

We will assume that gg is a Lipschitz function, bounded and increasing, with invariant measures at all densities ρ0\rho\geq 0:

  • |g(k+1)g(k)|a0|g(k+1)-g(k)|\ \leq\ a_{0} for k0k\geq 0

  • g=supk0g(k)a1\|g\|_{\infty}=\sup_{k\geq 0}g(k)\ \leq\ a_{1},

  • g(k+1)g(k)fork0g(k+1)\geq g(k)\ {\rm for\ }k\geq 0.

Note by Remark 4.3.3 that ρ(Ψ)\rho(\Psi)\uparrow\infty as Ψlimg(k)\Psi\uparrow\lim g(k), and so νρ\nu_{\rho} is defined for all densities 0ρ<0\leq\rho<\infty.

A standard example is g(k)=1(k1)g(k)=1(k\geq 1), under which κΨ\kappa_{\Psi} is Geometric, that is κΨ(k)=(1Ψ)Ψk\kappa_{\Psi}(k)=(1-\Psi)\Psi^{k} for k0k\geq 0 and Ψ[0,1)\Psi\in[0,1).

Also, to reduce notation, we assume pp is nearest-neighbor and symmetric:

  • p(e)=(2d)1p(e)\ =\ (2d)^{-1} for coordinate unit vectors ee, so that C=1d\triangle_{C}=\frac{1}{d}\triangle.

Recall that μ\mathbb{P}_{\mu} stands for the process measure when starting in μ\mu.

Theorem 4.6.1.

We have for all GC2(𝕋d)G\in C^{2}({\mathbb{T}}^{d}) and δ>0\delta>0 that

limNνρ0()[|G,πN2tN𝕋dG(u)ρ(t,u)du|>δ]= 0\lim_{N\uparrow\infty}\mathbb{P}_{\nu_{\rho_{0}(\cdot)}}\Big[\Big|\langle G,\pi^{N}_{N^{2}t}\rangle-\int_{{\mathbb{T}}^{d}}G(u)\rho(t,u)du\Big|>\delta\Big]\ =\ 0

where ρ\rho is the unique weak solution of the hydrodynamic equation

tρ=12dΨ(ρ)andρ(0,u)=ρ0(u).\partial_{t}\rho\ =\ \frac{1}{2d}\triangle\Psi(\rho)\ \ \ {\rm and\ \ \ }\rho(0,u)\ =\ \rho_{0}(u).

4.6.1. Strategy

We now separate the proof into two rough steps.

Step 1. We will again consider the measures QNQ^{N} which govern the trajectories of empirical distributions πN2tN\pi^{N}_{N^{2}t} on D([0,T],M+(𝕋d))D([0,T];M_{+}({\mathbb{T}}^{d})). The first task is to show that {QN}\{Q^{N}\} is tight, and all limit points are concentrated on trajectories of measures with densities π(t,u)du\pi(t,u)du.

Step 2. We show that all limit points are supported on weak solutions to the hydrodynamical equation in L2([0,T]×𝕋d)L^{2}([0,T]\times{\mathbb{T}}^{d}). It is a result in PDE that such weak solutions are unique. Hence, the measures QNQ^{N} converge to a single limit point. One concludes convergence at a fixed time, as for simple exclusion processes. The development on entropy, Dirichlet forms, and coupling will be useful in proving Step 2 in Section 5.

4.7. Notes

The zero-range process was introduced in [205]; see also [5], [68]. It has been a good vehicle to study a variety of phenomena, beyond hydrodynamics, such as condensation and metastability (cf. [8], [17], [136], [137], [154]).

Much of the development of entropy and its use in various applications, including hydrodynamics, stems from the work of Guo, Papanicolaou, and Varadhan (GPV) [106]. On the other hand the basic coupling, and its use in particle systems analysis was advanced by Liggett [147].

In terms of hydrodynamics, one may weaken the assumptions on gg. In particular, the increasing or boundedness assumptions are not needed when pp is mean-zero; see [130] and the Notes of Section 5. See the Notes of Section 6 for remarks when pp is asymmetric and not mean-zero.

There are at least five different proofs of the hydrodynamic behavior when pp say is symmetric. One way, the ‘entropy’ method [106], to be outlined in Section 5, shows that the limiting hydrodynamic density satisfies a weak form of hydrodynamical PDE. Another way, the ‘relative entropy’ method [221], assumes that a classical, smooth solution ρ=ρ(t,u)\rho=\rho(t,u) exists, and then shows that the relative entropy of νρ0()\nu_{\rho_{0}(\cdot)} with respect to νρ()\nu_{\rho(\cdot)} vanishes; see Section 6. One may use a Hopf-Lax formula, and the basic coupling, to prove in d=1d=1 the hydrodynamical limit for systems with drift [189], [6], [10]. A method using a logarithmic Sobolev inequality and compensated compactness ideas can be employed in d=1d=1 [80], [81]. Also, the hydrodynamic limit may be seen as a ‘gradient flow’, and found via Gamma convergence methods [61], [71], [101]. The first two methods are also discussed in [130]. See also [58] for a treatment of the GPV ‘entropy’ method, and [83], [213] for treatments of the ‘relative entropy’ method.

Section 5 Entropy method for hydrodynamics of zero-range processes

A rigorous proof of hydrodynamics (Theorem 4.6.1) is given for a class of zero-range models through the ‘entropy’ method of [106]. The main idea is that the drift computed from the generator action, an average of a nonlinear function of the occupation variables, may be understood in the scaling limit as a function of the limiting empirical density.

This sort of ergodic theorem, which proceeds in two replacement steps, the ‘1-block’ and ‘2-block’ lemmas which introduce additional scales, is facilitated by estimates on the Dirichlet form of a nonstationary Radon-Nikodym density function, and local central limit theorem asymptotics.

5.1. Proof of Step 1: Tightness and absolute continuity

Recall the notation from the Section 4, in particular the development and assumptions from Subsections 4.5 and 4.6. As before EμE_{\mu} stands for the expectation under μ\mu, and μ\mathbb{P}_{\mu} and 𝔼μ\mathbb{E}_{\mu} denote the process measure and expectation when starting in μ\mu.

Analogously as for simple exclusion, the first step can be divided into the tasks:

  • Show that the measures QNQ^{N} on D([0,T],+(𝕋d))D([0,T];\mathcal{M}_{+}({\mathbb{T}}^{d})) which govern πN2t:t[0,T]\langle\pi_{N^{2}t}:t\in[0,T]\rangle starting from local equilibrium νρ0()\nu_{\rho_{0}(\cdot)} are tight.

  • Show that all limit points of {QN}\{Q_{N}\} are supported on trajectories with densities π(t,u)du\pi(t,u)du.

Lemma 5.1.1.

{QN}\{Q^{N}\} is tight.

Proof.

Considering Proposition 3.2.7, we need only show items (1) for each t[0,T]t\in[0,T] that G,πN2tN\langle G,\pi^{N}_{N^{2}t}\rangle is tight on \mathbb{R}, and

(2)limγ0limNνρ0()(sup|ts|γ|G,πN2tNG,πN2sN|>ϵ)= 0.{\rm(2^{\prime})\ \ }\lim_{\gamma\downarrow 0}\lim_{N\uparrow\infty}\mathbb{P}_{\nu_{\rho_{0}(\cdot)}}\Big(\sup_{|t-s|\leq\gamma}\big|\langle G,\pi^{N}_{N^{2}t}\rangle-\langle G,\pi^{N}_{N^{2}s}\rangle\big|>\epsilon\Big)\ =\ 0.

Now, by the basic coupling and Exercise 4.4.5, we have that νρ0()νρ¯\nu_{\rho_{0}(\cdot)}\ll\nu_{\bar{\rho}} where ρ¯=ρ0\bar{\rho}=\|\rho_{0}\|_{\infty}. Hence, (1) follows as the first moments, 𝔼νρ0()[ηN2t(x)]Eνρ¯[η(0)]\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}[\eta_{N^{2}t}(x)]\leq E_{\nu_{\bar{\rho}}}[\eta(0)], are uniformly bounded:

𝔼νρ0()|G,πN2tN|1Ndx𝕋Nd|G(x/N)|Eνρ¯[η(0)]C(G,ρ¯).\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}|\langle G,\pi^{N}_{N^{2}t}\rangle|\ \leq\ \frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}|G(x/N)|E_{\nu_{\bar{\rho}}}[\eta(0)]\ \leq\ C(G,\bar{\rho}).

To establish (2’), we consider, as we did for the exclusion process, the drift and martingale terms separately. For the drift term, since gg is bounded, we have the uniform bound on NN,

sup|ts|γv(N)st|LG,πN2uN|𝑑u\displaystyle\sup_{|t-s|\leq\gamma}v(N)\int_{s}^{t}\big|L\langle G,\pi^{N}_{N^{2}u}\rangle\big|du γv(N)2Nd+2x,yp(y)(x,x+yNG)g\displaystyle\leq\gamma\frac{v(N)}{2N^{d+2}}\sum_{x,y}p(y)\big(\triangle^{N}_{x,x+y}G\big)\|g\|_{\infty}
γNC(R,g,p).\displaystyle\leq\gamma{N}C(R,g,p).

Noting the form of the quadratic variation MN(G)t\langle M^{N}(G)\rangle_{t} with v(N)=N2v(N)=N^{2} in Subsection 4.5, the proof is similar to that as for exclusion processes. ∎

We now establish the following characterization of limit points.

Lemma 5.1.2.

All limit points QQ of {QN}\{Q^{N}\} are supported on trajectories with densities π(t,u)du\pi(t,u)du such that, for a constant C=C(ρ¯)C=C(\bar{\rho}),

EQ[0Tπ(t,u)2𝑑u𝑑t]<C.E_{Q}\Big[\int_{0}^{T}\int\pi(t,u)^{2}dudt\Big]\ <\ C.

Before beginning the proof, we remark that absolute continuity of the limit trajectories means that particles cannot pile up to form point masses. Given the process is ‘attractive’, that is the basic coupling holds, one can bound the probability of large piles in terms of νρ¯\nu_{\bar{\rho}} estimates where ρ¯\bar{\rho} is an absolute bound on the hydrodynamic density. Without attractiveness, the proof is harder and we refer to [130] for a general argument.

Proof.

We show first that the trajectories are absolutely continuous under a limit point QQ. Let G:[0,T]×𝕋dG:[0,T]\times{\mathbb{T}}^{d}\rightarrow\mathbb{R} be a smooth function. Note, for A>0A>0 and for all large NN, by attractiveness and truncation bounds, that

0T1Ndx𝕋NdG(s,x/N)ηN2s(x)𝑑s\displaystyle\int_{0}^{T}\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}_{N}^{d}}G(s,x/N)\eta_{N^{2}s}(x)ds
(A+Eνρ¯[η(0)1(η(0)>A)])GL1([0,T]×)\displaystyle\ \ \leq\ \big(A+E_{\nu_{\bar{\rho}}}[\eta(0)1(\eta(0)>A)]\big)\|G\|_{L^{1}([0,T]\times\mathbb{R})}
+0T1Ndx𝕋Nd|G(s,x/N)|(ηN2s(x)1(ηN2s(x)>A)Eνρ¯[η(0)1(η(0)>A)]).\displaystyle\ \ +\int_{0}^{T}\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}_{N}^{d}}|G(s,x/N)|\big(\eta_{N^{2}s}(x)1(\eta_{N^{2}s}(x)>A)-E_{\nu_{\bar{\rho}}}[\eta(0)1(\eta(0)>A)]\big).

The last term is an increasing function of ηN2s\eta_{N^{2}s}, which we will show is small. The role of AA is to introduce a truncation. Let ϕ(ηN2s(x))=ηN2s(x)1(ηN2s>A)Eνρ¯[η(0)1(η(0)>A)\phi(\eta_{N^{2}s}(x))=\eta_{N^{2}s}(x)1(\eta_{N^{2}s}>A)-E_{\nu_{\bar{\rho}}}[\eta(0)1(\eta(0)>A). Therefore, by the basic coupling, Chebychev’s inequality and invariance of νρ¯\nu_{\bar{\rho}}, for ϵ>0\epsilon>0, we have

νρ0()(0T1Ndx|G(s,x/N)|ϕ(ηN2s(x))>ϵ)\displaystyle\mathbb{P}_{\nu_{\rho_{0}(\cdot)}}\Big(\int_{0}^{T}\frac{1}{N^{d}}\sum_{x}|G(s,x/N)|\phi(\eta_{N^{2}s}(x))>\epsilon\Big)
νρ¯(0T1Ndx|G(s,x/N)|ϕ(ηN2s(x))>ϵ)\displaystyle\ \ \ \ \ \ \ \leq\ \mathbb{P}_{\nu_{\bar{\rho}}}\Big(\int_{0}^{T}\frac{1}{N^{d}}\sum_{x}|G(s,x/N)|\phi(\eta_{N^{2}s}(x))>\epsilon\Big)
2TGL2Ndϵ2Varνρ¯(η(0)1(η(0)>A))=O(Nd).\displaystyle\ \ \ \ \ \ \ \leq\ \frac{2T\|G\|_{L^{2}}}{N^{d}\epsilon^{2}}{\rm Var}_{\nu_{\bar{\rho}}}\big(\eta(0)1(\eta(0)>A)\big)\ =\ O(N^{-d}).

Hence, by simple estimates,

QN(0TG(s,),πs𝑑s(A+Eνρ¯[η(0)1(η(0)>A)])GL1+ϵ) 1O(Nd)Q^{N}\Big(\int_{0}^{T}\langle G(s,\cdot),\pi_{s}\rangle ds\leq\big(A+E_{\nu_{\bar{\rho}}}[\eta(0)1(\eta(0)>A)]\big)\|G\|_{L^{1}}+\epsilon\Big)\ \geq\ 1-O(N^{-d})

and by weak convergence, since the function 0TG(s,),πs𝑑s\int_{0}^{T}\langle G(s,\cdot),\pi_{s}\rangle ds is continuous in the Skorohod topology and Q(F)limQN(F)Q(F)\geq\lim Q^{N}(F) for closed sets,

Q(0TG(s,),πs𝑑s(A+Eνρ¯[η(0)1(η(0)>A)])GL1+ϵ)= 1.Q\Big(\int_{0}^{T}\langle G(s,\cdot),\pi_{s}\rangle ds\leq\big(A+E_{\nu_{\bar{\rho}}}[\eta(0)1(\eta(0)>A)]\big)\|G\|_{L^{1}}+\epsilon\Big)\ =\ 1.

Since ϵ>0\epsilon>0 is arbitrary, we have a.s. under QQ that all trajectories satisfy

0TG(s,),πs𝑑sCGL1.\int_{0}^{T}\langle G(s,\cdot),\pi_{s}\rangle ds\ \leq\ C\|G\|_{L^{1}}.

Now, note by the tightness estimate (2’) already proven in the previous lemma that all trajectories under QQ are continuous in time in the underlying topology (e.g. tH,πtt\mapsto\langle H,\pi_{t}\rangle is continuous for HC2(𝕋d)H\in C^{2}({\mathbb{T}}^{d})). Then, by choosing GG to approximate δ11(t,t+δ)1(B)\delta^{-1}1(t,t+\delta)1(B) for B𝕋dB\subset{\mathbb{T}}^{d}, we obtain πt(B)C|B|\pi_{t}(B)\leq C|B|, that is πt\pi_{t} is absolutely continuous for each t[0,T]t\in[0,T].

To show the display in the lemma, recall (4.5.1) and consider the bound

supN1𝔼νρ0()[0Tdu1Ndx𝕋Nd(ηN2sNϵ(x))2]TEνρ¯[η(0)2],\sup_{N\geq 1}\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\Big[\int_{0}^{T}du\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}\big(\eta_{N^{2}s}^{N\epsilon}(x)\big)^{2}\Big]\ \leq\ TE_{\nu_{\bar{\rho}}}[\eta(0)^{2}],

via the basic coupling and Schwarz inequality

(ηNϵ(x))21(2Nϵ+1)d|yx|Nϵη(y)2.\big(\eta^{N\epsilon}(x)\big)^{2}\leq\frac{1}{(2N\epsilon+1)^{d}}\sum_{|y-x|\leq N\epsilon}\eta(y)^{2}.

Hence, as QQ is a limit point, by Fatou’s lemma again, we have

EQ[0Tds𝕋ddx((2ϵ)dB(u,ϵ)π(s,v)𝑑v)2]C(T,ρ¯)E_{Q}\Big[\int_{0}^{T}ds\int_{{\mathbb{T}}^{d}}dx\Big((2\epsilon)^{-d}\int_{B(u,\epsilon)}\pi(s,v)dv\Big)^{2}\Big]\ \leq\ C(T,\bar{\rho})

where B(u,ϵ)B(u,\epsilon) is the ball of radius ϵ\epsilon around uu. Taking limit on ϵ0\epsilon\downarrow 0, and another application of Fatou’s lemma along with Lebesgue’s differentiation theorem (a.e. uu is a Lebesgue point), we finish the proof. ∎

5.2. Proof of Step 2: Identification given replacement homogenization

We now supply, modulo a replacement estimate, the proof of Theorem 4.6.1. Note that Ψ(ρ)=Eνρ[g(η(0))]\Psi(\rho)=E_{\nu_{\rho}}[g(\eta(0))] is a bounded function as gg is bounded. Recall also the notation η(x)\eta^{\ell}(x) in (4.5.1). Let τx\tau_{x} be the shift operator, (τxη)(y)=η(x+y)(\tau_{x}\eta)(y)=\eta(x+y) and τxf(η)=f(τxη)\tau_{x}f(\eta)=f(\tau_{x}\eta).

Theorem 5.2.1 (Replacement).

For JC([0,T]×𝕋d)J\in C([0,T]\times{\mathbb{T}}^{d}), we have that

lim supϵ0lim supN𝔼νρ0()[|0T1Ndx𝕋NdJ(s,x/N)τxVNϵ(ηN2s)𝑑s|]= 0\limsup_{\epsilon\downarrow 0}\limsup_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\Big[\Big|\int_{0}^{T}\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}J(s,x/N)\tau_{x}V_{N\epsilon}(\eta_{N^{2}s})ds\Big|\Big]\ =\ 0

where

V(η)=g(η(0))Ψ(η(0)).V_{\ell}(\eta)\ =\ g(\eta(0))-\Psi(\eta^{\ell}(0)).

Notice that VV_{\ell} is a bounded function as gg is bounded.

Let us now see how this replacement allows to finish the proof of hydrodynamics.

5.2.1. Proof of Theorem 4.6.1

First, we establish an equation that the densities π(t,u)\pi(t,u) under a limit point QQ must satisfy. Let GC2([0,T]×𝕋d)G\in C^{2}([0,T]\times{\mathbb{T}}^{d}). Then, following the derivation when GG did not depend on time in Subsection 4.5, we obtain

G(t,),πN2tN=G(0,),π0N\displaystyle\langle G(t,\cdot),\pi^{N}_{N^{2}t}\rangle\ =\ \langle G(0,\cdot),\pi^{N}_{0}\rangle
+0tN2Nd+2x𝕋Nd[sG(s,x/N)ηN2s(x)+12dG(s,x/N)g(ηN2s(x))]ds\displaystyle\ \ \ \ +\int_{0}^{t}\frac{N^{2}}{N^{d+2}}\sum_{x\in{\mathbb{T}}^{d}_{N}}\Big[\partial_{s}G(s,x/N)\eta_{N^{2}s}(x)+\frac{1}{2d}\triangle G(s,x/N)g(\eta_{N^{2}s}(x))\Big]ds
+MtN(G)+o(1)\displaystyle\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ +M^{N}_{t}(G)+o(1)

where by Doob’s inequality,

𝔼νρ0()[supt[0,T](MtN(G))2]𝔼νρ0()[(MTN(G))2]=O(N2TNd2)\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\big[\sup_{t\in[0,T]}\big(M^{N}_{t}(G)\big)^{2}\big]\ \leq\ \mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\big[\big(M^{N}_{T}(G)\big)^{2}\big]\ =\ O(N^{2}TN^{-d-2})

since gg is bounded.

On the other hand, by Theorem 5.2.1, since G\triangle G is continuous, we have

limϵ0limN𝔼νρ0()[|0T1Ndx𝕋NdG(s,x/N){g(ηN2s(x))Ψ(ηN2sNϵ(x))}𝑑s|]= 0.\lim_{\epsilon\downarrow 0}\lim_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\Big[\Big|\int_{0}^{T}\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}^{d}_{N}}\triangle G(s,x/N)\Big\{g(\eta_{N^{2}s}(x))-\Psi\big(\eta_{N^{2}s}^{N\epsilon}(x)\big)\Big\}ds\Big|\Big]\ =\ 0.

Putting this together, noting (4.5.2), we have

limϵ0limN𝔼νρ0()[|G(T,),πN2TNG(0,),π0N0TsG(s,),πN2sNds\displaystyle\lim_{\epsilon\downarrow 0}\lim_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\Big[\Big|\langle G(T,\cdot),\pi^{N}_{N^{2}T}\rangle-\langle G(0,\cdot),\pi^{N}_{0}\rangle-\int_{0}^{T}\Big\langle\partial_{s}G(s,\cdot),\pi^{N}_{N^{2}s}\Big\rangle ds
12d0t𝕋dG(s,u)Ψ(πs(N,ϵ)(u))ds|]= 0\displaystyle\ \ \ \ \ \ \ \ \ \ \ \ \ \ -\frac{1}{2d}\int_{0}^{t}\int_{{\mathbb{T}}^{d}}\triangle G(s,u)\Psi(\pi^{(N,\epsilon)}_{s}(u))ds\Big|\Big]\ =\ 0 (5.2.1)

where πs(N,ϵ)(u)=(2ϵ)d1[ϵ,ϵ]d(u),πN2sN\pi^{(N,\epsilon)}_{s}(u)=\big\langle(2\epsilon)^{-d}1_{[-\epsilon,\epsilon]^{d}}(\cdot-u),\pi^{N}_{N^{2}s}\big\rangle.

Now, again the quantity in absolute value in (5.2.1) is a continuous function of π\pi in the Skorohod topology. Hence, any limit point QQ, by Fatou’s lemma, satisfies

limϵ0EQ[|G,πTG,π00TsG,πsds\displaystyle\lim_{\epsilon\downarrow 0}E_{Q}\Big[\Big|\langle G,\pi_{T}\rangle-\langle G,\pi_{0}\rangle-\int_{0}^{T}\Big\langle\partial_{s}G,\pi_{s}\Big\rangle ds
12d0T𝕋dG(s,u)Ψ(πs(ϵ)(u))duds|]= 0,\displaystyle\ \ \ \ \ \ \ \ \ \ \ \ -\frac{1}{2d}\int_{0}^{T}\int_{{\mathbb{T}}^{d}}\triangle G(s,u)\Psi(\pi^{(\epsilon)}_{s}(u))duds\Big|\Big]\ =\ 0,

where πs(ϵ)(u)=(2ϵ)d1[ϵ,ϵ]d(u),πs\pi^{(\epsilon)}_{s}(u)=\big\langle(2\epsilon)^{-d}1_{[-\epsilon,\epsilon]^{d}}(\cdot-u),\pi_{s}\big\rangle.

But, since trajectories have densities under QQ, and Ψ\Psi is bounded and continuous, by Lebesgue’s differentiation theorem and dominated convergence,

limϵ0EQ[0T𝕋d|Ψ(πs(ϵ)(u))Ψ(π(u,s))|𝑑u𝑑s]= 0.\lim_{\epsilon\downarrow 0}E_{Q}\Big[\int_{0}^{T}\int_{{\mathbb{T}}^{d}}\big|\Psi(\pi^{(\epsilon)}_{s}(u))-\Psi(\pi(u,s))\big|duds\Big]\ =\ 0.

Finally, we obtain therefore QQ is supported on trajectories satisfying

G(T,),πT=G(0,),π0+0TGs,πs𝑑s+12d0T𝕋dG(s,u)Ψ(π(s,u))𝑑u𝑑s\langle G(T,\cdot),\pi_{T}\rangle=\langle G(0,\cdot),\pi_{0}\rangle+\int_{0}^{T}\langle G_{s},\pi_{s}\rangle ds+\frac{1}{2d}\int_{0}^{T}\int_{{\mathbb{T}}^{d}}\triangle G(s,u)\Psi(\pi(s,u))duds

which are weak solutions to

tρ=12dΨ(ρ)ρ(0,u)=ρ0(u).\partial_{t}\rho\ =\ \frac{1}{2d}\triangle\Psi(\rho)\ \ \ {\rm\ \ }\rho(0,u)=\rho_{0}(u).

At this point, it is known in PDE that weak solutions with L2L^{2} integrable densities are unique (cf. [130, Appendix 2.4]). Hence, following now the same argument as for simple exclusion, we obtain Theorem 4.6.1. ∎

5.3. Proof of the replacement homogenization

After preliminaries and some reductions, we prove Theorem 5.2.1 at the end of this subsection. Since we start out of a stationary distribution, we have to understand the nonstationary contribution. Controlling the entropy and Dirichlet form of the associated Radon-Nikodym probability density is the first step.

For ρ¯=ρ0()<\bar{\rho}=\|\rho_{0}(\cdot)\|_{\infty}<\infty, let νρ¯\nu_{\bar{\rho}} be a reference measure throughout the rest of Section 5. Let also ftN=dνρ0()PN2t/dνρ¯f^{N}_{t}=d\nu_{\rho_{0}(\cdot)}P_{N^{2}t}/d\nu_{\bar{\rho}} be the Radon-Nikodym density at macroscopic time t0t\geq 0. Let H(ftN)=H(νρ0()PN2t|νρ¯)H(f^{N}_{t})=H(\nu_{\rho_{0}(\cdot)}P_{N^{2}t}|\nu_{\bar{\rho}}). By Lemma 4.3.5, we know H(f0N)CNdH(f^{N}_{0})\leq CN^{d} for some constant C<C<\infty. Since the time scaling is v(N)=N2v(N)=N^{2}, we have by Lemma 4.3.7 for each t[0,T]t\in[0,T] that

H(ftN)+2N20tI(fsN)𝑑sH(f0N)CNd.H(f^{N}_{t})+2N^{2}\int_{0}^{t}I(f^{N}_{s})ds\ \leq\ H(f^{N}_{0})\ \leq\ CN^{d}.

Let f¯tN=1t0tfsN𝑑s\bar{f}^{N}_{t}=\frac{1}{t}\int_{0}^{t}f^{N}_{s}ds. Then, by convexity of the entropy and Dirichlet form, we have

H(f¯tN)CNdandI(f¯tN)C(2t)1Nd2.H\left(\bar{f}^{N}_{t}\right)\leq CN^{d}\ \ {\rm and\ \ }I\left(\bar{f}^{N}_{t}\right)\leq C(2t)^{-1}N^{d-2}. (5.3.1)

For later reference, the following estimate will allow to introduce a truncation corresponding to the number of particles in a region.

Lemma 5.3.1.

For 1\ell\geq 1, we have

supx,y𝕋Nd,t[0,T]𝔼νρ0()[ηN2t(x)1(ηN2t(y)>A)]A1Eνρ¯[η2(0)].\sup_{x,y\in{\mathbb{T}}^{d}_{N},t\in[0,T]}\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\Big[\eta_{N^{2}t}^{\ell}(x)1\big(\eta_{N^{2}t}^{\ell}(y)>A\big)\Bigg]\ \leq\ A^{-1}E_{\nu_{\bar{\rho}}}[\eta^{2}(0)].
Proof.

By Markov’s inequality, the basic coupling as η(x)η(y)\eta^{\ell}(x)\eta^{\ell}(y) is an increasing function, and Schwarz inequality, we have the left-hand side is bounded by

supx,y𝕋Nd,t[0,T]A1𝔼νρ0()[(ηN2t(x))2]1/2𝔼νρ0()[(ηN2t(y))2]1/2A1Eνρ¯[η2(0)].\sup_{x,y\in{\mathbb{T}}^{d}_{N},t\in[0,T]}A^{-1}\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\Big[\big(\eta_{N^{2}t}^{\ell}(x)\big)^{2}\Big]^{1/2}\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\Big[\big(\eta_{N^{2}t}^{\ell}(y)\big)^{2}\Big]^{1/2}\ \leq\ A^{-1}E_{\nu_{\bar{\rho}}}[\eta^{2}(0)].\qed

5.3.1. Reductions

Consider the following bound of the integrand in Theorem 5.2.1, by adding and subtracting terms. Write

1NdxJ(xN)τxVNϵ(η)\displaystyle\frac{1}{N^{d}}\sum_{x}J\Big(\frac{x}{N}\Big)\ \tau_{x}V^{N\epsilon}(\eta)
=1NdxJ(xN){g(η(x))1(2+1)d|z|g(η(z+x))}\displaystyle=\ \frac{1}{N^{d}}\sum_{x}J\Big(\frac{x}{N}\Big)\ \Big\{g(\eta(x))-\frac{1}{(2\ell+1)^{d}}\sum_{|z|\leq\ell}g(\eta(z+x))\Big\}
+1NdxJ(xN){1(2+1)d|z|g(η(z+x))Ψ(η()(x))}\displaystyle+\ \frac{1}{N^{d}}\sum_{x}J\Big(\frac{x}{N}\Big)\ \Big\{\frac{1}{(2\ell+1)^{d}}\sum_{|z|\leq\ell}g(\eta(z+x))-\Psi\big(\eta^{(\ell)}(x)\big)\Big\}
+1NdxJ(xN){Ψ(η()(x))Ψ(η(Nϵ)(x))}.\displaystyle+\ \frac{1}{N^{d}}\sum_{x}J\Big(\frac{x}{N}\Big)\ \Big\{\Psi\big(\eta^{(\ell)}(x)\big)-\Psi\big(\eta^{(N\epsilon)}(x)\big)\Big\}. (5.3.2)

The first term on the right-hand side introduces the scale \ell and more averaging: As gg is bounded and JJ is uniformly continuous, it vanishes when NN\uparrow\infty and \ell\uparrow\infty. If JJ were C1C^{1}, it would be of order O(/N)O(\ell/N).

The second term, bringing an absolute value inside the sum, is bounded by JNdxτx|V(η)|\frac{\|J\|_{\infty}}{N^{d}}\sum_{x}\tau_{x}|V_{\ell}(\eta)| where we observe

|V(η)|=|1(2+1)d|y|g(η(y))Ψ(η(0))|2g.|V_{\ell}(\eta)|=\Big|\frac{1}{(2\ell+1)^{d}}\sum_{|y|\leq\ell}g(\eta(y))-\Psi(\eta^{\ell}(0))\Big|\leq 2\|g\|_{\infty}.

Moreover, we may introduce a truncation by Lemma 5.3.1, so that what remains to bound is for A>0A>0 the expectation of

1Ndxτx(|V(η)|1(η(0)A)).\frac{1}{N^{d}}\sum_{x}\tau_{x}\Big(|V_{\ell}(\eta)|1(\eta^{\ell}(0)\leq A)\Big).

In the third term, as Ψ\Psi is Lipschitz, we bound it by

JNdx|Ψ(η(x))Ψ(ηNϵ(x))|JNdx|η(x)ηNϵ(x)|.\displaystyle\frac{\|J\|_{\infty}}{N^{d}}\sum_{x}\Big|\Psi(\eta^{\ell}(x))-\Psi(\eta^{N\epsilon}(x))\Big|\leq\frac{\|J\|_{\infty}}{N^{d}}\sum_{x}\big|\eta^{\ell}(x)-\eta^{N\epsilon}(x)\Big|.

We may further write the NϵN\epsilon-window term ηNϵ(x)\eta^{N\epsilon}(x) in terms of an average of disjoint \ell-window terms η(x+zi)\eta^{\ell}(x+z_{i}) for 1iM:=(2Nϵ+1)d/(2+1)d1\leq i\leq M:=\lfloor(2N\epsilon+1)^{d}/(2\ell+1)^{d}\rfloor as

ηNϵ(x)=1Mi=1Mη(x+zi)+1(2Nϵ+1)djη(x+j),\eta^{N\epsilon}(x)=\frac{1}{M}\sum_{i=1}^{M}\eta^{\ell}(x+z_{i})+\frac{1}{(2N\epsilon+1)^{d}}\sum_{j}\eta(x+j),

where {zi}\{z_{i}\} are centers of the cubes in the decomposition and the last sum is over at most (2Nϵ+1)d(2+1)d(2Nϵ+1)d/(2+1)dO((Nϵ)d1(2+1)d)(2N\epsilon+1)^{d}-(2\ell+1)^{d}\lfloor(2N\epsilon+1)^{d}/(2\ell+1)^{d}\rfloor\leq O\big((N\epsilon)^{d-1}(2\ell+1)^{d}\big) variables in possibly uncompleted \ell-windows. One may also add into this sum the contributions from the \ell-windows neighboring xx, say those with centers within 22\ell of xx. Then, noting the d\ell^{d}-overcount of these ‘edge’ items, the third term is further bounded by

JNd1Mi=1M1(2|zi|Nϵ)x|η(x)η(x+zi)|\displaystyle\frac{\|J\|_{\infty}}{N^{d}}\frac{1}{M}\sum_{i=1}^{M}1(2\ell\leq|z_{i}|\leq N\epsilon)\sum_{x}\Big|\eta^{\ell}(x)-\eta^{\ell}(x+z_{i})\Big|
+CJd(Nϵ)d1(Nϵ)d1Ndxη(x).\displaystyle\quad\quad\quad+\frac{C\|J\|_{\infty}\ell^{d}(N\epsilon)^{d-1}}{(N\epsilon)^{d}}\frac{1}{N^{d}}\sum_{x}\eta(x).

The νρ0()N\nu^{N}_{\rho_{0}(\cdot)}-process expectation of the last term is of order O(d/(Nϵ))O\big(\ell^{d}/(N\epsilon)\big) since by the basic coupling 𝔼νρ0()N[ηN2t(x)]Eνρ¯[η(0)]=ρ¯\mathbb{E}_{\nu^{N}_{\rho_{0}(\cdot)}}\big[\eta_{N^{2}t}(x)\big]\leq E_{\nu_{\bar{\rho}}}\big[\eta(0)\big]=\bar{\rho}. We may also introduce truncations, for A>0A>0 by Lemma 5.3.1, so that we need only bound the expectation of

1Nd1Mi=1M1(2|zi|2Nϵ)x|η(x)η(x+zi)|1(η(x)+η(x+zi)A).\displaystyle\frac{1}{N^{d}}\frac{1}{M}\sum_{i=1}^{M}1(2\ell\leq|z_{i}|\leq 2N\epsilon)\sum_{x}\Big|\eta^{\ell}(x)-\eta^{\ell}(x+z_{i})\Big|1(\eta^{\ell}(x)+\eta^{\ell}(x+z_{i})\leq A). (5.3.3)

5.3.2. Statements of 11 and 22-block lemmas

Recall the definition of the density f¯tN\bar{f}^{N}_{t} near (5.3.1). By the development in the previous subsection, to bound the second term in (5.3.1), it is enough to estimate

𝔼νρ0()[0T1Ndxτx{|V(ηN2s)|1(ηN2s(0)A)}𝑑s]\displaystyle\mathbb{E}_{\nu_{\rho_{0}(\cdot)}}\Big[\int_{0}^{T}\frac{1}{N^{d}}\sum_{x}\tau_{x}\big\{|V_{\ell}(\eta_{N^{2}s})|1(\eta_{N^{2}s}^{\ell}(0)\leq A)\big\}ds\Big]
=TEνρ¯[f¯TN(η)1Ndxτx{|V(η)|1(η(0)A)}].\displaystyle\quad\quad=TE_{\nu_{\bar{\rho}}}\Big[\bar{f}^{N}_{T}(\eta)\frac{1}{N^{d}}\sum_{x}\tau_{x}\big\{|V_{\ell}(\eta)|1(\eta^{\ell}(0)\leq A)\big\}\Big].

Since we know I(f¯TN)=O(Nd2)I(\bar{f}^{N}_{T})=O\big(N^{d-2}\big) from (5.3.1), choosing A>ρ¯A>\bar{\rho}, it will be sufficient to show the following.

Proposition 5.3.2 (1-block lemma).

We have for all A>ρ¯A>\bar{\rho} that

limlimNsupI(f)C0Nd2Eνρ¯[f(η)1Ndx𝕋Ndτx|V(η)|1(η(0)A)]= 0\lim_{\ell\uparrow\infty}\lim_{N\uparrow\infty}\sup_{I(f)\leq C_{0}N^{d-2}}E_{\nu_{\bar{\rho}}}\Big[f(\eta)\frac{1}{N^{d}}\sum_{x\in{\mathbb{T}}_{N}^{d}}\tau_{x}|V_{\ell}(\eta)|1(\eta^{\ell}(0)\leq A)\Big]\ =\ 0

where the supremum is over nonnegative densities ff with fL1(νρ¯)=1\|f\|_{L^{1}(\nu_{\bar{\rho}})}=1.

The third term in (5.3.1) is handled similarly. Noting the formulation in (5.3.3), it is enough to show the following limit.

Proposition 5.3.3 (2-block lemma).

We have for A>ρ¯A>\bar{\rho} that

limlimϵ0limNsupI(f)C0Nd2sup2<|y|2Nϵ\displaystyle\lim_{\ell\uparrow\infty}\lim_{\epsilon\downarrow 0}\lim_{N\uparrow\infty}\sup_{I(f)\leq C_{0}N^{d-2}}\sup_{2\ell<|y|\leq 2N\epsilon}
Eνρ¯[f(η)1Ndx|η(x)η(x+y)|1(η(x)+η(x+y)A)]= 0.\displaystyle\ \ \ \ \ \ E_{\nu_{\bar{\rho}}}\Big[f(\eta)\frac{1}{N^{d}}\sum_{x}\big|\eta^{\ell}(x)-\eta^{\ell}(x+y)\big|1(\eta^{\ell}(x)+\eta^{\ell}(x+y)\leq A)\Big]\ =\ 0.

Proof of Theorem 5.2.1. With the 11 and 22-block replacements Propositions 5.3.2, 5.3.3 in hand, the proof follows from the reductions in Subsection 5.3.1. ∎

5.4. Proof of 1-block lemma

To prove Proposition 5.3.2, the main idea is that the Dirichlet form of the density ff vanishes as NN\uparrow\infty. In some sense, the optimal density ff is almost constant. Things then reduce to a standard ergodic theorem or law of large numbers associated with i.i.d. random variables distributed according to κρ¯\kappa_{\bar{\rho}}.

To make this strategy precise, define

Av(f)=1Ndxτxf(η).{\rm Av}(f)\ =\ \frac{1}{N^{d}}\sum_{x}\tau_{x}f(\eta).

Then, by translation-invariance of νρ¯\nu_{\bar{\rho}},

Eνρ¯[f(η)1Ndxτx|V(η)|1(η(0)A)]\displaystyle E_{\nu_{\bar{\rho}}}\Big[f(\eta)\frac{1}{N^{d}}\sum_{x}\tau_{x}|V_{\ell}(\eta)|1(\eta^{\ell}(0)\leq A)\Big]
=Eνρ¯[Av(f)|V(η)|1(η(0)A)].\displaystyle\quad\quad\quad=\ E_{\nu_{\bar{\rho}}}\Big[{\rm Av}(f)|V_{\ell}(\eta)|1(\eta^{\ell}(0)\leq A)\Big]. (5.4.1)

Observe that Av(f){\rm Av}(f) is a translation-invariant density.

Let now

Λ={,,}dand=σ{η(x):xΛ}.\Lambda_{\ell}=\{-\ell,\ldots,\ell\}^{d}\ \ {\rm and\ \ }\mathcal{F}_{\ell}=\sigma\{\eta(x):x\in\Lambda_{\ell}\}.

Denote f=Eνρ¯[Av(f)|]f_{\ell}=E_{\nu_{\bar{\rho}}}[{\rm Av}(f)|\mathcal{F}_{\ell}]. Since |V(η)|1(η(0)A)|V_{\ell}(\eta)|1(\eta^{\ell}(0)\leq A) depends only on variables η(x)\eta(x) where xΛx\in\Lambda_{\ell}, we have the right-side of (5.4.1) equals

Eνρ¯[f(η)|V(η)|1(ηA)]=Eνρ¯[f(η)|V(η)|1(ηA)]E_{\nu_{\bar{\rho}}}[f_{\ell}(\eta)|V_{\ell}(\eta)|1(\eta^{\ell}\leq A)]\ =\ E_{\nu^{\ell}_{\bar{\rho}}}[f_{\ell}(\eta)|V_{\ell}(\eta)|1(\eta^{\ell}\leq A)]

where νρ¯\nu^{\ell}_{\bar{\rho}} is the product measure over sites in Λ\Lambda_{\ell} with marginal κΨ(ρ¯)\kappa_{\Psi(\bar{\rho})}.

Now, recall that the Dirichlet form has explicit form (4.3.2). For x,yx,y such that |xy|=1|x-y|=1, let

Ix,x+y(h)=12(2d)Eνρ¯[g(η(x))(h(ηx,x+y)h(η))2].I_{x,x+y}(h)=\frac{1}{2(2d)}E_{\nu_{\bar{\rho}}}\Big[g(\eta(x))\big(\sqrt{h(\eta^{x,x+y})}-\sqrt{h(\eta)}\big)^{2}\Big].

Then, I(h)=x,|y|=1Ix,x+y(h)I(h)=\sum_{x,|y|=1}I_{x,x+y}(h); note there are dNddN^{d} edges in 𝕋Nd{\mathbb{T}}_{N}^{d} .

Define also the Dirichlet form corresponding to the dynamics restricted to Λ\Lambda_{\ell} with invariant measure νρ¯\nu^{\ell}_{\bar{\rho}}.

I(h)=x,x+yΛx,|y|=1Ix,x+y(h);I_{\ell}(h)\ =\ \sum_{\stackrel{{\scriptstyle x,|y|=1}}{{x,x+y\in\Lambda_{\ell}}}}I_{x,x+y}(h);

note there are d(2+1)d1(2)d(2\ell+1)^{d-1}(2\ell) edges in Λ\Lambda_{\ell}.

Lemma 5.4.1.

We have that

I(f)\displaystyle I_{\ell}(f_{\ell}) \displaystyle\leq I(Av(f))\displaystyle I_{\ell}({\rm Av}(f))
=\displaystyle= (2+1)d1(2)NdI(Av(f))\displaystyle(2\ell+1)^{d-1}(2\ell)N^{-d}I({\rm Av}(f))
\displaystyle\leq (2+1)d1(2)NdI(f)\displaystyle(2\ell+1)^{d-1}(2\ell)N^{-d}I(f)
\displaystyle\leq CdN2.\displaystyle C\ell^{d}N^{-2}.
Proof.

Note ff_{\ell} and Av(f){\rm Av}(f) are averages: For instance, ff_{\ell} is a conditional expectation. Then, the first and second inequalities follow as the Dirichlet form is convex. The equality follows as Av(f){\rm Av}(f) and the measure νρ¯\nu_{\bar{\rho}} are translation-invariant: Namely, Ix,x+y(Av(f))=Iz,z+w(Av(f)CLOSEI_{x,x+y}({\rm Av}(f))=I_{z,z+w}({\rm Av}(f) for x,z𝕋Ndx,z\in{\mathbb{T}}_{N}^{d} and |y|=|w|=1|y|=|w|=1. The last line follows from the bound I(f)C0Nd2I(f)\leq C_{0}N^{d-2}. ∎

Now, taking into account (5.4.1) and the display after, and Lemma 5.4.1, we need to show

limlimNsupI(f)CdN2Eνρ¯[f(η)|V(η)|1(η(0)A)]= 0\lim_{\ell\uparrow\infty}\lim_{N\uparrow\infty}\sup_{I_{\ell}(f)\leq C\ell^{d}N^{-2}}E_{\nu^{\ell}_{\bar{\rho}}}\big[f(\eta)|V_{\ell}(\eta)|1(\eta^{\ell}(0)\leq A)\big]\ =\ 0 (5.4.2)

where the supremum is over densities ff with respect to νρ¯\nu^{\ell}_{\bar{\rho}}.

In fact, since νρ¯(ηA)>0\nu^{\ell}_{\bar{\rho}}(\eta^{\ell}\leq A)>0 is uniformly bounded below for all large \ell because A>ρ¯A>\bar{\rho}, in (5.4.2), we may replace the integrating measure νρ¯\nu^{\ell}_{\bar{\rho}} by νρ¯,A=νρ¯(|η(0)A)\nu^{\ell}_{\bar{\rho},A}=\nu^{\ell}_{\bar{\rho}}(\cdot|\eta^{\ell}(0)\leq A) which supports only a finite number of configurations. Also, as

Eνρ¯,A[f]=Eνρ¯[f1(η(0)A)]/ν(η(0)A)1/ν(η(0)A)C,E_{\nu^{\ell}_{\bar{\rho},A}}[f]=E_{\nu^{\ell}_{\bar{\rho}}}[f1(\eta^{\ell}(0)\leq A)]/\nu^{\ell}(\eta^{\ell}(0)\leq A)\leq 1/\nu^{\ell}(\eta^{\ell}(0)\leq A)\leq C,

we may view the supremum as over the collection of nonnegative ff with respect to νρ¯,A\nu^{\ell}_{\bar{\rho},A} which are uniformly bounded fL1(νρ¯,A)C\|f\|_{L^{1}(\nu^{\ell}_{\bar{\rho},A})}\leq C. The corresponding collection of subprobablity measures fdνρ¯,A/Cfd\nu^{\ell}_{\bar{\rho},A}/C, being on a compact space, is tight and has a converging subsequence by a form of Prokhorov’s theorem.

Hence, to evaluate (5.4.2), for fixed \ell, we consider a sequence in NN which approaches the limit supremum. Densities fNf^{N} can be found on which the supremum value is well approximated. By tightness, we can find a subsequence where fNf^{N} converges to ff^{*} for which necessarily I(f)=0I_{\ell}(f^{*})=0. Hence, it is enough to show

limsupI(f)=0Eνρ¯[f(η)|V(η)|1(η(0)A)]= 0.\lim_{\ell\uparrow\infty}\sup_{I_{\ell}(f)=0}E_{\nu^{\ell}_{\bar{\rho}}}\big[f(\eta)|V_{\ell}(\eta)|1(\eta^{\ell}(0)\leq A)\big]\ =\ 0.

Now, given I(f)=0I_{\ell}(f^{*})=0 and η(0)A\eta^{\ell}(0)\leq A, we know that ff^{*} is constant on the configurations such that η(0)=a\eta^{\ell}(0)=a for aAa\leq A. Therefore, as fCf^{*}\leq C, decomposing along such ‘hyperplanes’, it is enough to show that

limsupaAEνρ¯[|V(η)||η(0)=a]= 0.\lim_{\ell\uparrow\infty}\sup_{a\leq A}E_{\nu^{\ell}_{\bar{\rho}}}\big[|V_{\ell}(\eta)|\big|\eta^{\ell}(0)=a\big]\ =\ 0. (5.4.3)

The left-hand side expectation is the same as

Eνρ¯[|1(2+1)d|x|g(η(x))Eνa[g(η(0))]||η(0)=a].E_{\nu_{\bar{\rho}}}\Big[\Big|\frac{1}{(2\ell+1)^{d}}\sum_{|x|\leq\ell}g(\eta(x))-E_{\nu_{a}}\big[g(\eta(0))\big]\Big|\Big|\eta^{\ell}(0)=a\Big].

Here, we removed the restriction of the measure to Λ\Lambda_{\ell} since it does not matter. Notice also that the integrating measure is the canonical measure on Λ\Lambda_{\ell} with a(2+1)da(2\ell+1)^{d} particles. Hence, by the form νρ¯\nu_{\bar{\rho}}, the parameter ρ¯\bar{\rho} of the underlying grand-canonical measure νρ¯\nu_{\bar{\rho}} does not matter, and can be chosen as we like, say aa.

We may rewrite the above display as

1(2+1)dνa(η(0)=a)\displaystyle\frac{1}{\sqrt{(2\ell+1)^{d}}\nu_{a}(\eta^{\ell}(0)=a)} (5.4.4)
×Eνa[|1(2+1)d|x|(g(η(x))Eνa[g(η(0))])1(η(0)=a)].\displaystyle\quad\times E_{\nu_{a}}\Big[\Big|\frac{1}{\sqrt{(2\ell+1)^{d}}}\sum_{|x|\leq\ell}\big(g(\eta(x))-E_{\nu_{a}}\big[g(\eta(0))\big]\big)1\big(\eta^{\ell}(0)=a\big)\Big].

It is an exercise to see that the denominator is bounded away from 00.

Exercise 5.4.2.

Observe by a local central limit theorem, namely an expansion in the characteristic function, that

lim(2+1)dνa(η(0)=a)=(2π)d/2.\lim_{\ell\uparrow\infty}\sqrt{(2\ell+1)^{d}}\nu_{a}(\eta^{\ell}(0)=a)\ =\ (2\pi)^{-d/2}.

Now, the variables g(η(x))Eνa[g(η(0))]g(\eta(x))-E_{\nu_{a}}[g(\eta(0))] in (5.4.4) are mean-zero and in L2(νa)L^{2}(\nu_{a}). Hence, by an application of Schwarz inequality and Exercise 5.4.2 again, we have that (5.4.4) is at most of order O(d/4)O(\ell^{-d/4}) which vanishes.

This concludes the proof of Proposition 5.3.2. ∎

5.5. Proof of 2-block lemma

The argument for the proof of Proposition 5.3.3 is similar to the proof of the ‘1-block Lemma’ Proposition 5.3.2. Now, we have to control the differences of averages in two separated blocks of width 2+12\ell+1. To compare these averages, we need again to show that the localized Dirichlet form of the density function is small. Since the jump probabilities are nearest-neighbor, to localize on the two blocks of width O()O(\ell), we will need to extend the Dirichlet form and dynamics to include a long jump from one block to the other. In this way, the localized system can mix, and the difference in the averages will wash out. There is a cost for this extension which however can be overcome.

As before, with the ‘11-block Lemma’, the first step is to estimate the display in Proposition 5.3.3 in terms of the averaged density over shifts Av(f){\rm Av}(f). We need to show that

limlimϵ0limNsupI(f)C0Nd2sup2<|y|2Nϵ\displaystyle\lim_{\ell\uparrow\infty}\lim_{\epsilon\downarrow 0}\lim_{N\uparrow\infty}\sup_{I(f)\leq C_{0}N^{d-2}}\sup_{2\ell<|y|\leq 2N\epsilon}
Eνρ¯[f(η)|η(0)η(y)|1(|η(0)+η(y)A)]= 0\displaystyle\ \ \ E_{\nu_{\bar{\rho}}}\Big[f(\eta)|\eta^{\ell}(0)-\eta^{\ell}(y)|1(|\eta^{\ell}(0)+\eta^{\ell}(y)\leq A)\Big]\ =\ 0

Here the supremum is over translation invariant densities ff.

Next, we localize to the union of the two blocks Λ\Lambda_{\ell} and Λy=y+Λ\Lambda^{y}_{\ell}=y+\Lambda_{\ell}. Let νρ¯,y\nu^{\ell,y}_{\bar{\rho}} be the product measure over xΛΛyx\in\Lambda_{\ell}\cup\Lambda^{y}_{\ell} with marginal κρ¯\kappa_{\bar{\rho}}. Let also f,y=Eνρ¯,y[f|,y]f^{\ell,y}=E_{\nu^{\ell,y}_{\bar{\rho}}}[f|\mathcal{F}_{\ell,y}] where ,y=σ{η(x):xΛΛy}\mathcal{F}_{\ell,y}=\sigma\{\eta(x):x\in\Lambda_{\ell}\cup\Lambda^{y}_{\ell}\}. Then, as before, the above display reduces to

limlimϵ0limNsupI(f)C0Nd2sup2<|y|2Nϵ\displaystyle\lim_{\ell\uparrow\infty}\lim_{\epsilon\downarrow 0}\lim_{N\uparrow\infty}\sup_{I(f)\leq C_{0}N^{d-2}}\sup_{2\ell<|y|\leq 2N\epsilon}
Eνρ¯,y[f,x(η)|η(0)η(y)|1(|η(0)+η(y)A)]= 0,\displaystyle\ \ \ E_{\nu^{\ell,y}_{\bar{\rho}}}\Big[f^{\ell,x}(\eta)|\eta^{\ell}(0)-\eta^{\ell}(y)|1(|\eta^{\ell}(0)+\eta^{\ell}(y)\leq A)\Big]\ =\ 0,

for say A>2ρ¯A>2\bar{\rho}.

The question now is how to treat the Dirichlet form I(f)I(f). If we use the argument for the ‘11-block Lemma’, then a density in the limit would be constant on each hyperplane {ηΛΛy:η(0)+η(y)=a}\{\eta_{\Lambda_{\ell}\cup\Lambda^{y}_{\ell}}:\eta^{\ell}(0)+\eta^{\ell}(y)=a\} for aAa\leq A where ηB=η(x):xB\eta_{B}=\langle\eta(x):x\in B\rangle. But, the constants could be different on each block!

The trick is to add a (non-local) Dirichlet form bond corresponding to a jump say from 0Λ0\in\Lambda_{\ell} to yΛyy\in\Lambda_{\ell}^{y}. Any such jump from a site in Λ\Lambda_{\ell} to Λy\Lambda^{y}_{\ell} would work. Then, if the Dirichlet form localized to ΛΛy\Lambda_{\ell}\cup\Lambda^{y}_{\ell}, including this extra bond term, vanishes, the density would take the same constant value on both blocks. In terms of dynamics, the zero-range process associated to this modified Dirichlet form is irreducible on configurations in Ωy,={0,1,}ΛΛy\Omega^{y,\ell}=\{0,1,\ldots\}^{\Lambda_{\ell}\cup\Lambda^{y}_{\ell}}.

For h:Ωy,h:\Omega^{y,\ell}\rightarrow\mathbb{R}, define

Ib(h)\displaystyle I_{b}(h) =12Eνρ¯[g(η(0))(h(η0,y)h(η))2]\displaystyle=\frac{1}{2}E_{\nu_{\bar{\rho}}}\Big[g(\eta(0))\big(\sqrt{h(\eta^{0,y})}-\sqrt{h(\eta)}\big)^{2}\Big]
=Ψ(ρ¯)2Eνρ¯[(h(η+δx)h(η+δ0))2],\displaystyle=\frac{\Psi(\bar{\rho})}{2}E_{\nu_{\bar{\rho}}}\Big[\big(\sqrt{h(\eta+\delta_{x})}-\sqrt{h(\eta+\delta_{0})}\big)^{2}\Big],

noting Exercise 4.3.1. By itself, IbI_{b} is the Dirichlet form for the dynamics which moves a particle from 00 to yy and back according to zero-range dynamics, and as such shares all the convexity and other Dirichlet form properties that we used in the proof of the ‘1-block Lemma’.

By the estimate (j=1kqj)2kj=1kqj2\big(\sum_{j=1}^{k}q_{j}\big)^{2}\ \leq\ k\sum_{j=1}^{k}q_{j}^{2} and adding and subtracting several terms,

Ib(h)\displaystyle I_{b}(h) =Ψ(ρ¯)2Eνρ¯[(k=1mxh(η+δqk)h(η+δqk+1))2]\displaystyle=\frac{\Psi(\bar{\rho})}{2}E_{\nu_{\bar{\rho}}}\Big[\Big(\sum_{k=1}^{m_{x}}\sqrt{h(\eta+\delta_{q_{k}})}-\sqrt{h(\eta+\delta_{q_{k+1}})}\Big)^{2}\Big]
C|x|j=1MxIqj,qj+1(h)\displaystyle\leq C|x|\sum_{j=1}^{M_{x}}I_{q_{j},q_{j+1}}(h)

where {qk}\{q_{k}\} corresponds to a nearest-neighbor path from 00 to xx in Mx=O(|x|)M_{x}=O(|x|) steps.

We will apply the above estimate to the translation invariant density ff. Since Iej,ej+1(f)CNdI(f)I_{e_{j},e_{j+1}}(f)\leq CN^{-d}I(f), we have that Ib(f)C|x|2NdI(f)I_{b}(f)\leq C|x|^{2}N^{-d}I(f). Now, if I(f)CNd2I(f)\leq CN^{d-2} and |x|CN2ϵ2|x|\leq CN^{2}\epsilon^{2}, since the separation between 00 and xx is of order O(Nϵ)O(N\epsilon), we conclude Ib(f)Cϵ2I_{b}(f)\leq C\epsilon^{2}.

Let now Iy,(h)=I(h)+Iy(h)+Ib(h)I^{y,\ell}(h)=I_{\ell}(h)+I_{\ell}^{y}(h)+I_{b}(h) where Iy(h)=z,z+wΛyz,|w|=1Iz,z+w(h)I_{\ell}^{y}(h)=\sum_{\stackrel{{\scriptstyle z,|w|=1}}{{z,z+w\in\Lambda^{y}_{\ell}}}}I_{z,z+w}(h). By convexity, we have

Iy,(f,x)Iy,(f) 2CdN2+Cϵ2Cϵ2\displaystyle I^{y,\ell}(f^{\ell,x})\ \leq\ I^{y,\ell}(f)\ \leq\ 2C\ell^{d}N^{-2}+C\epsilon^{2}\ \leq\ C\epsilon^{2} (5.5.1)

for fixed ,ϵ\ell,\epsilon and all large NN.

Hence, it is enough to show for each constant CC that

limlimϵ0limNsupIx,(f)Cϵ2sup2<|y|2Nϵ\displaystyle\lim_{\ell\uparrow\infty}\lim_{\epsilon\downarrow 0}\lim_{N\uparrow\infty}\sup_{I^{x,\ell}(f)\leq C\epsilon^{2}}\sup_{2\ell<|y|\leq 2N\epsilon}
Eνρ¯,x[f(η)|η(0)η(y)|1(|η(0)+η(y)A)]= 0.\displaystyle\ \ \ E_{\nu^{\ell,x}_{\bar{\rho}}}\Big[f(\eta)|\eta^{\ell}(0)-\eta^{\ell}(y)|1(|\eta^{\ell}(0)+\eta^{\ell}(y)\leq A)\Big]\ =\ 0.

Here, the supremum is over densities with respect to νρ¯,x\nu_{\bar{\rho}}^{\ell,x}.

But, at this point, the proof can follow the method as for the ‘11-block Lemma’. We just point out that in the above display that, as η(0)\eta^{\ell}(0) and η(y)\eta^{\ell}(y) share no terms, with respect to νρ¯,x\nu_{\bar{\rho}}^{\ell,x}, they are independent. This was the reason to avoid the nearest-neighbor cubes in the original decomposition of ηNϵ(x)\eta^{N\epsilon}(x) in Subsection 5.3.1. This finishes the proof of Proposition 5.3.3. ∎

5.6. Notes

We have followed the scheme of Chapter V in [130], although there are differences. The reader will have noted that translation invariance is much used in the above derivations. We remark that there are ways to handle non-translation invariant dynamics if the inhomogeneity is ‘slowly varying’; see [52], and [95], [69], [76], [138] when the particles move in a random environment.

Also, we comment that diffusive scaling v(N)=N2v(N)=N^{2} was crucial to prove the ‘22-block’ estimate; see (5.5.1). In asymmetric models, with hyperbolic scaling v(N)=Nv(N)=N, although the ‘11-block’ result still holds, the ‘22-block’ estimate is not generally available. Such a ‘11-block Lemma’ is useful for the ‘relative entropy’ method discussed in Section 6 to deduce hydrodynamics, at least for short times, in asymmetric processes.

Finally, we comment, beyond Zero-range models, the ‘entropy’ method works well in symmetric rate processes (v(N)=N2v(N)=N^{2}) with conserved quantities that is of ‘gradient’ type, e.g. allowing a twice sum-by-parts evaluation

LG,πV(N)tNv(N)2Nd+2x,yh(τxηv(N)t)p(y)x,yNGL\langle G,\pi^{N}_{V(N)t}\rangle\sim\frac{v(N)}{2N^{d+2}}\sum_{x,y}h(\tau_{x}\eta_{v(N)t})p(y)\triangle^{N}_{x,y}G

for some local function hh (depending only on a finite number of variables {η(x)}\{\eta(x)\}) to be homogenized, and invariant measures indexed to the conserved quantities with sufficient decorrelation properties (cf. for instance [85]). As alluded in Subsection 2.4.3, diffusively scaled ‘nongradient’ models can also be analyzed by versions of the ‘entropy’ method (cf. [15], [130], [213]).

Section 6 Relative entropy method and hydrodynamics of TASEP

We discuss the ‘relative entropy’ method in the context of hydrodynamics of the totally asymmetric simple exclusion process (TASEP) in d=1d=1. The underlying notion is to measure how far the distribution μtN\mu^{N}_{t} of the process at time tt is away from a specified product measure νtN\nu^{N}_{t} on 𝕋N{\mathbb{T}}_{N}. If distance, measured in terms of relative entropy, is not so far away, then hydrodynamics will follow from calculations with respect to independent variables governed by νtN\nu^{N}_{t}. Such methods and ideas have proved useful for other processes and in other problems.

6.1. Statement of hydrodynamics and sketch of the argument

Recall the notation in Chaper 2, with respect to asymmetric exclusion processes ηt\eta_{t} on 𝕋Nd{\mathbb{T}}^{d}_{N}. As before, EμE_{\mu} denotes the expectation under μ\mu, and μ\mathbb{P}_{\mu} and 𝔼μ\mathbb{E}_{\mu} the process measure and expectation when starting in μ\mu.

When d=1d=1 and pp allows movement only to the nearest right site, that is p(1)=1p(1)=1 and p(j)=0p(j)=0 for j𝕋Nj\in{\mathbb{T}}_{N} otherwise, the process is known as the totally asymmetric simple exclusion process or TASEP for short. To reduce notation, we will concentrate in the following on TASEP, although calculations may be extended to finite-range asymmetric processes in d1d\geq 1 with non-zero drift.

As mentioned in Section 2, the nontrivial time scaling is when υ(N)=N\upsilon(N)=N, the ‘hyperbolic’ or ‘Euler’ scale, and the hydrodynamic density ρ(t,u)\rho(t,u) satisfies tρ+m[ρ(t,u)(1ρ(t,u))]=0\partial_{t}\rho+m\cdot\nabla\big[\rho(t,u)(1-\rho(t,u))\big]=0. In the context of TASEP, as m=jp(j)=1m=\sum jp(j)=1, the equation simplifies to

tρ+u(ρ(1ρ))=0.\partial_{t}\rho+\partial_{u}\big(\rho(1-\rho)\big)=0. (6.1.1)

Solutions to this one-dimensional Burgers-type hyperbolic conservation law on 𝕋{\mathbb{T}} are not necessarily unique. However, when starting from smooth C1C^{1} initial profile ρ0(u)=ρ(0,u)\rho_{0}(u)=\rho(0,u), bounded above and below on 𝕋{\mathbb{T}},

0<ρρ0(u)ρ+<1,0<\rho_{-}\leq\rho_{0}(u)\leq\rho_{+}<1,

it is known that a unique classical C1C^{1} smooth solution, also bounded above and below by ρ+\rho_{+} and ρ\rho_{-}, with continuous bounded derivatives, exists up to a short time T>0T>0, which we now fix. We mention one may specify uniquely a ‘physical’ (or by other names, ‘entropy’ or ‘viscosity’) solution for all times t0t\geq 0 by imposing that the solution satisfies extra conditions; see [67] as a general reference and for a comprehensive discussion.

Recall the empirical measure on 𝕋N{\mathbb{T}}_{N}:

πtN=1Nx𝕋Nηt(x)δx/N.\pi^{N}_{t}=\frac{1}{N}\sum_{x\in{\mathbb{T}}_{N}}\eta_{t}(x)\delta_{x/N}.

Define, for t[0,T]t\in[0,T], with respect to the hydrodynamic density, the product measures on Ω={0,1}𝕋N\Omega=\{0,1\}^{{\mathbb{T}}_{N}}:

νtN=x𝕋NBern(ρ(t,x/N)).\nu^{N}_{t}=\prod_{x\in{\mathbb{T}}_{N}}{\rm Bern}(\rho(t,x/N)).

Suppose that initially the process η0\eta_{0} is distributed according to μN=ν0N=νρ0()N\mu^{N}=\nu^{N}_{0}=\nu^{N}_{\rho_{0}(\cdot)}. In terms of the process semigroup PtP_{t}, let μtN=μNPNt\mu^{N}_{t}=\mu^{N}P_{Nt} be the distribution of ηNt\eta_{Nt} starting from μN\mu^{N}.

We will show the following form of the hydrodynamic limit.

Theorem 6.1.1.

Let ρ0:𝕋[0,1]\rho_{0}:{\mathbb{T}}\rightarrow[0,1] be a C1C^{1} function. Then, for t[0,T]t\in[0,T], we have the convergence in probability,

limNπNtN,J=1Nx𝕋NJ(x/N)ηNt(x)=𝕋J(u)ρ(t,u)𝑑u\lim_{N\rightarrow\infty}\langle\pi^{N}_{Nt},J\rangle=\frac{1}{N}\sum_{x\in{\mathbb{T}}_{N}}J(x/N)\eta_{Nt}(x)=\int_{{\mathbb{T}}}J(u)\rho(t,u)du

where ρ(t,u)\rho(t,u) satisfies (6.1.1) with ρ(0,u)=ρ0(u)\rho(0,u)=\rho_{0}(u).

Proof.

The sketch of the argument is in a few steps.

Step 1. Since νtN(η)>0\nu^{N}_{t}(\eta)>0 for all ηΩ\eta\in\Omega, we have μtNνtN\mu^{N}_{t}\ll\nu^{N}_{t}. Noting Lemma 4.1.4, we will show that the relative entropy H(μtN|νtN)=EμtN[logμtNνtN]H(\mu^{N}_{t}|\nu^{N}_{t})=E_{\mu^{N}_{t}}\big[\log\frac{\mu^{N}_{t}}{\nu^{N}_{t}}\big] between the distribution μtN\mu^{N}_{t} of ηNt\eta_{Nt} and νtN\nu^{N}_{t} is o(N)o(N). This step is the main part of the proof. It takes the 11-block lemma as input, and is discussed in the next subsection.

Step 2. The entropy inequality (cf. Lemma 4.1.2, Exercise 4.1.3) yields for sets AΩA\subset\Omega that

μtN(A)log(2)+H(μtN|νtN)log(1+1/νtN(A)).\mu^{N}_{t}(A)\leq\frac{\log(2)+H(\mu^{N}_{t}|\nu^{N}_{t})}{\log\big(1+1/\nu^{N}_{t}(A)\big)}.

Let now ϵ>0\epsilon>0 and

A={η:|1Nx𝕋NJ(x/N)[η(x)ρ(t,x/N)]|>ϵ}.A=\Big\{\eta:\big|\frac{1}{N}\sum_{x\in{\mathbb{T}}_{N}}J(x/N)\big[\eta(x)-\rho(t,x/N)\big]\big|>\epsilon\Big\}.

An exponential bound νtN(A)eCN\nu^{N}_{t}(A)\leq e^{-CN} may be found as the variables {ηNt(x):x𝕋N}\{\eta_{Nt}(x):x\in{\mathbb{T}}_{N}\} are independent under νtN\nu^{N}_{t} with means {ρ(t,x/N):x𝕋N}\{\rho(t,x/N):x\in{\mathbb{T}}_{N}\}. Therefore, given the relative entropy estimate in Step 1, the theorem follows. ∎

Exercise 6.1.2.

Show the ‘Chernoff’ exponential bound in Step 2, by computing the moment-generating functions. The inequality 0<ρρ(t,x/N)ρ+<10<\rho_{-}\leq\rho(t,x/N)\leq\rho_{+}<1 will be useful.

6.2. Proof of Step 1: o(N)o(N) entropy estimate

Let ν1/2=x𝕋NBern(1/2)\nu_{1/2}=\prod_{x\in{\mathbb{T}}_{N}}{\rm Bern}(1/2) denote the product invariant measure of TASEP with density 1/21/2. Recall the form of LL in (2.2.1) (in d=1d=1 and p(1)=1p(1)=1, p(j)=0p(j)=0 otherwise). One may compute that the L2(ν1/2)L^{2}(\nu_{1/2})-adjoint operator LN=NLL^{*}_{N}=NL^{*} of LN=NLL_{N}=NL is the generator of the asymmetric exclusion process, speeded up by υ(N)=N\upsilon(N)=N, where particles jumps left, that is when p(1)=1p^{*}(-1)=1 and p(j)=0p^{*}(j)=0 otherwise:

LNh(η)=x𝕋Nη(x)(1η(x1))[h(ηx,x1)h(η)].\displaystyle L_{N}^{*}h(\eta)=\sum_{x\in{\mathbb{T}}_{N}}\eta(x)\big(1-\eta(x-1)\big)\big[h(\eta^{x,x-1})-h(\eta)\big].

The probabilities μtN\mu^{N}_{t} satisfy the forward equation (cf. Exercise 6.2.1),

tμtN=LNμtN.\partial_{t}\mu^{N}_{t}=L^{*}_{N}\mu^{N}_{t}. (6.2.1)

However, μtN\mu^{N}_{t} is no longer a product measure, the process having mixed things up from the initial condition ν0N\nu^{N}_{0}. One feels though from the intuition given in Section 2 that the process may not be far from νtN\nu^{N}_{t}. The relative entropy H(t):=H(μtN|νtN)H(t):=H(\mu^{N}_{t}|\nu^{N}_{t}) is a convenient, and analytically tractable measure of how far apart they are.

Exercise 6.2.1.

Perform the computation of LNL^{*}_{N}. Show also μtN\mu^{N}_{t} satisfies (6.2.1) by differentiating 𝔼ν1/2[h(ηNt)]=Eν1/2[ftN(η)h(η)]=ην1/2(η)ftN(η)h(η)\mathbb{E}_{\nu_{1/2}}\big[h(\eta_{Nt})\big]=E_{\nu_{1/2}}\big[f^{N}_{t}(\eta)h(\eta)\big]=\sum_{\eta}\nu_{1/2}(\eta)f^{N}_{t}(\eta)h(\eta) where the density ftN(η)=μtN(η)ν1/2(η)f^{N}_{t}(\eta)=\frac{\mu^{N}_{t}(\eta)}{\nu_{1/2}(\eta)} and hh is a bounded function. The relation ν1/2(η)(1/2)N\nu_{1/2}(\eta)\equiv(1/2)^{N} for all η{0,1}𝕋N\eta\in\{0,1\}^{{\mathbb{T}}_{N}} will be useful.

Step A. We first update the conclusion of Lemmas 4.2.3 and 4.2.7, one of the differences being that μtN\mu^{N}_{t} is not the invariant measure.

Lemma 6.2.2.

We have

H(t)\displaystyle H^{\prime}(t) ηνtN(η)η(x)(1η(x+1))(μtNνtN(ηx,x+1)μtNνtN(η))2\displaystyle\leq-\sum_{\eta}\nu^{N}_{t}(\eta)\eta(x)\big(1-\eta(x+1)\big)\left(\sqrt{\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta^{x,x+1})}-\sqrt{\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta)}\right)^{2}
+EμtN[1νtN(η)(LNt)νtN(η)].\displaystyle\quad\quad+E_{\mu^{N}_{t}}\Big[\frac{1}{\nu^{N}_{t}(\eta)}\big(L^{*}_{N}-\partial_{t}\big)\nu^{N}_{t}(\eta)\Big].
Proof.

Write

tH(μtN|νtN)\displaystyle\partial_{t}H(\mu^{N}_{t}|\nu^{N}_{t}) =tημtN(η)[logμtN(η)logνtN(η)]\displaystyle=\partial_{t}\sum_{\eta}\mu^{N}_{t}(\eta)\big[\log\mu^{N}_{t}(\eta)-\log\nu^{N}_{t}(\eta)\big]
=ηLNμtN(η)[[logμtN(η)logνtN(η)]\displaystyle=\sum_{\eta}L^{*}_{N}\mu^{N}_{t}(\eta)\big[[\log\mu^{N}_{t}(\eta)-\log\nu^{N}_{t}(\eta)\big]
+ημtN(η)[1μtN(η)tμtN(η)tlogνtN(η)].\displaystyle\quad\quad+\sum_{\eta}\mu^{N}_{t}(\eta)\big[\frac{1}{\mu^{N}_{t}(\eta)}\partial_{t}\mu^{N}_{t}(\eta)-\partial_{t}\log\nu^{N}_{t}(\eta)\big].

Note that tημtN(η)=0\partial_{t}\sum_{\eta}\mu^{N}_{t}(\eta)=0 as ημtN(η)1\sum_{\eta}\mu^{N}_{t}(\eta)\equiv 1. Also,

ηLNμtN(η)logμtN(η)νtN(η)\displaystyle\sum_{\eta}L^{*}_{N}\mu^{N}_{t}(\eta)\log\frac{\mu^{N}_{t}(\eta)}{\nu^{N}_{t}(\eta)} =ην1/2(η)(LNμtN(η)ν1/2(η))logμtN(η)νtN(η)\displaystyle=\sum_{\eta}\nu_{1/2}(\eta)\Big(L^{*}_{N}\frac{\mu^{N}_{t}(\eta)}{\nu_{1/2}(\eta)}\Big)\log\frac{\mu^{N}_{t}(\eta)}{\nu^{N}_{t}(\eta)}
=ην1/2(η)μtN(η)ν1/2(η)(LNlogμtN(η)νtN(η))\displaystyle=\sum_{\eta}\nu_{1/2}(\eta)\frac{\mu^{N}_{t}(\eta)}{\nu_{1/2}(\eta)}\Big(L_{N}\log\frac{\mu^{N}_{t}(\eta)}{\nu^{N}_{t}(\eta)}\Big)
=ημtN(η)LNlogμtN(η)νtN(η).\displaystyle=\sum_{\eta}\mu^{N}_{t}(\eta)L_{N}\log\frac{\mu^{N}_{t}(\eta)}{\nu^{N}_{t}(\eta)}.

Then,

tH(μtN|νtN)\displaystyle\partial_{t}H(\mu^{N}_{t}|\nu^{N}_{t}) =ημtN(η)LNlogμtN(η)νtN(η)ημtN(η)tlogνtN(η).\displaystyle=\sum_{\eta}\mu^{N}_{t}(\eta)L_{N}\log\frac{\mu^{N}_{t}(\eta)}{\nu^{N}_{t}(\eta)}-\sum_{\eta}\mu^{N}_{t}(\eta)\partial_{t}\log\nu^{N}_{t}(\eta). (6.2.2)

Now, consider the relation

a(logbloga) 2a(ba)=(ba)2+(ba),a(\log b-\log a)\ \leq\ 2\sqrt{a}\big(\sqrt{b}-\sqrt{a}\big)\ =\ -\big(\sqrt{b}-\sqrt{a}\big)^{2}+\big(b-a\big),

for a,b>0a,b>0. Then, as Lg(η)=xη(x)(1η(x+1))[g(ηx,x+1)g(η)]Lg(\eta)=\sum_{x}\eta(x)(1-\eta(x+1))\big[g(\eta^{x,x+1})-g(\eta)\big], with a=μtNνtN(η)a=\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta) and b=μtNνtN(ηx,x+1)b=\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta^{x,x+1}), we observe

ημtN(η)LNlogμtN(η)νtN(η)\displaystyle\sum_{\eta}\mu^{N}_{t}(\eta)L_{N}\log\frac{\mu^{N}_{t}(\eta)}{\nu^{N}_{t}(\eta)}
ηνtN(η)xη(x)(1η(x+1))2μtNνtN(η)(μtNνtN(ηx,x+1)μtNνtN(η)),\displaystyle\ \leq\sum_{\eta}\nu^{N}_{t}(\eta)\sum_{x}\eta(x)\big(1-\eta(x+1)\big)\cdot 2\sqrt{\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta)}\left(\sqrt{\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta^{x,x+1})}-\sqrt{\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta)}\right),

which further equals

ηxνtN(η)η(x)(1η(x+1))(μtNνtN(ηx,x+1)μtNνtN(η))2\displaystyle-\sum_{\eta}\sum_{x}\nu^{N}_{t}(\eta)\eta(x)\big(1-\eta(x+1)\big)\left(\sqrt{\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta^{x,x+1})}-\sqrt{\frac{\mu^{N}_{t}}{\nu^{N}_{t}}(\eta)}\right)^{2}
+ηνtN(η)LNμtN(η)νtN(η).\displaystyle\quad\quad\quad+\sum_{\eta}\nu^{N}_{t}(\eta)L_{N}\frac{\mu^{N}_{t}(\eta)}{\nu^{N}_{t}(\eta)}.

We may insert this expression into (6.2.2). Dividing/multiplying by (1/2)Nν1/2(η)(1/2)^{N}\equiv\nu_{1/2}(\eta) again and moving LNL_{N} to LNL^{*}_{N} on the other side, we obtain the expression desired. ∎

We remark that for the ‘relative entropy’ method in the sequel, we will not use the first term, a ‘Dirichlet’ form expression, bounding it above by 00. However, the the full force of Lemma 6.2.2 has been useful in other problems; see the Notes.

Step B. Next, we evaluate the second term on the right-hand side in Lemma 6.2.2. Explicitly,

νtN(η)\displaystyle\nu^{N}_{t}(\eta) =xρ(t,x/N)η(x)(1ρ(t,x/N))1η(x)\displaystyle=\prod_{x}\rho(t,x/N)^{\eta(x)}(1-\rho(t,x/N))^{1-\eta(x)}
=exp{ψN(t,η)},\displaystyle=\exp\big\{\psi_{N}(t,\eta)\big\},

where

ψN(t,η)=x{η(x)logρ(t,x/N)+(1η(x))log(1ρ(t,x/N))}.\psi_{N}(t,\eta)=\sum_{x}\Big\{\eta(x)\log\rho(t,x/N)+(1-\eta(x))\log(1-\rho(t,x/N))\Big\}.

Hence,

1νtN(η)LNνtN(η)\displaystyle\frac{1}{\nu^{N}_{t}(\eta)}L^{*}_{N}\nu^{N}_{t}(\eta)
=Nxη(x+1)(1η(x))\displaystyle\quad\quad=N\sum_{x}\eta(x+1)(1-\eta(x))
[1exp{ψN(t,η)}(exp{ψN(t,ηx,x+1)}exp{ψN(t,η)})]\displaystyle\quad\quad\quad\quad\quad\cdot\Big[\frac{1}{\exp\big\{\psi_{N}(t,\eta)\big\}}\Big(\exp\big\{\psi_{N}(t,\eta^{x,x+1})\big\}-\exp\big\{\psi_{N}(t,\eta)\big\}\Big)\Big]
=Nxη(x+1)(1η(x))[exp{ψN(t,ηx,x+1)ψN(t,η)}1].\displaystyle\quad\quad=N\sum_{x}\eta(x+1)(1-\eta(x))\Big[\exp\big\{\psi_{N}(t,\eta^{x,x+1})-\psi_{N}(t,\eta)\big\}-1\Big].

Observe

ψN(t,ηx,x+1)ψN(t,η)\displaystyle\psi_{N}(t,\eta^{x,x+1})-\psi_{N}(t,\eta)
={η(x+1)logρ(t,x/N)+(1η(x+1))log(1ρ(t,x/N))\displaystyle\quad=\Big\{\eta(x+1)\log\rho(t,x/N)+(1-\eta(x+1))\log(1-\rho(t,x/N))
+η(x)logρ(t,(x+1)/N)+(1η(x))log(1ρ(t,(x+1)/N))}\displaystyle\quad\quad\quad+\eta(x)\log\rho(t,(x+1)/N)+(1-\eta(x))\log(1-\rho(t,(x+1)/N))\Big\}
{η(x)logρ(t,x/N)+(1η(x))log(1ρ(t,x/N))\displaystyle\quad-\Big\{\eta(x)\log\rho(t,x/N)+(1-\eta(x))\log(1-\rho(t,x/N))
+η(x+1)logρ(t,(x+1)/N)+(1η(x+1))logρ(t,(x+1)/N)}.\displaystyle\quad\quad\quad+\eta(x+1)\log\rho(t,(x+1)/N)+(1-\eta(x+1))\log\rho(t,(x+1)/N)\Big\}.

Hence, under the condition η(x+1)=1\eta(x+1)=1 and η(x)=0\eta(x)=0, corresponding to η(x+1)(1η(x))=1\eta(x+1)(1-\eta(x))=1, we have by Taylor approximation that

exp{ψN(t,ηx,x+1)ψN(t,η)}1\displaystyle\exp\big\{\psi_{N}(t,\eta^{x,x+1})-\psi_{N}(t,\eta)\big\}-1
=exp{logρ(t,x/N)logρ(t,(x+1)/N)\displaystyle\quad=\exp\big\{\log\rho(t,x/N)-\log\rho(t,(x+1)/N)
+log(1ρ(t,(x+1)/N))log(1ρ(t,x/N))}1\displaystyle\quad\quad\quad+\log(1-\rho(t,(x+1)/N))-\log(1-\rho(t,x/N))\big\}-1
=exp{1Nρρ(t,x/N)1Nρ1ρ(t,x/N)+o(1/N)}1\displaystyle\quad=\exp\big\{-\frac{1}{N}\frac{\rho^{\prime}}{\rho}(t,x/N)-\frac{1}{N}\frac{\rho^{\prime}}{1-\rho}(t,x/N)+o(1/N)\big\}-1
=1Nρ(t,x/N)ρ(1ρ)(t,x/N)+o(1/N).\displaystyle\quad=\frac{-1}{N}\frac{\rho^{\prime}(t,x/N)}{\rho(1-\rho)(t,x/N)}+o(1/N).

Therefore, cancelling the ‘NN’, we obtain

1νtN(η)LNνtN(η)\displaystyle\frac{1}{\nu^{N}_{t}(\eta)}L^{*}_{N}\nu^{N}_{t}(\eta) =xη(x+1)(1η(x))ρ(t,x/N)ρ(1ρ)(t,x/N)+o(N).\displaystyle=-\sum_{x}\eta(x+1)(1-\eta(x))\frac{\rho^{\prime}(t,x/N)}{\rho(1-\rho)(t,x/N)}+o(N).

On the other hand,

1νtN(η)tνtN(η)\displaystyle-\frac{1}{\nu^{N}_{t}(\eta)}\partial_{t}\nu^{N}_{t}(\eta) =1exp{ψN(t)}texp{ψN(t)}=tψN(t)\displaystyle=-\frac{1}{\exp\big\{\psi_{N}(t)\big\}}\partial_{t}\exp\big\{\psi_{N}(t)\big\}\ =\ -\partial_{t}\psi_{N}(t)
=xη(x)tρρ(t,x/N)+x(1η(x))tρρ(t,x/N).\displaystyle=-\sum_{x}\eta(x)\frac{\partial_{t}\rho}{\rho}(t,x/N)+\sum_{x}(1-\eta(x))\frac{\partial_{t}\rho}{\rho}(t,x/N).

Recall tρ=u(ρ(1ρ))=(2ρ1)uρ\partial_{t}\rho=-\partial_{u}\big(\rho(1-\rho)\big)=(2\rho-1)\partial_{u}\rho. Then, by Lemma 6.2.2, dropping the negative ‘Dirichlet’ term, and dividing by NN, we conclude

1NH(t)\displaystyle\frac{1}{N}H^{\prime}(t) EμtN[1Nx{η(x+1)(1η(x))uρρ(1ρ)(t,x/N)\displaystyle\leq E_{\mu^{N}_{t}}\Big[\frac{1}{N}\sum_{x}\Big\{\eta(x+1)(1-\eta(x))\frac{-\partial_{u}\rho}{\rho(1-\rho)}(t,x/N)
η(x)(2ρ1)uρρ(1,x/N)+(1η(x))(2ρ1)uρ1ρ(t,x/N)}]+o(1).\displaystyle\quad-\eta(x)\frac{(2\rho-1)\partial_{u}\rho}{\rho}(1,x/N)+(1-\eta(x))\frac{(2\rho-1)\partial_{u}\rho}{1-\rho}(t,x/N)\Big\}\Big]+o(1).

Step C. Now, we invoke a form of the 11-block lemma in Section 5. We state it in d=1d=1 in the context of TASEP, although it can be generalized to d1d\geq 1 and other processes. Recall that η(x)=12+1|yx|η(y)\eta^{\ell}(x)=\frac{1}{2\ell+1}\sum_{|y-x|\leq\ell}\eta(y).

Proposition 6.2.3.

Let G:[0,T]×𝕋G:[0,T]\times{\mathbb{T}}\rightarrow\mathbb{R} be continuous. Let hh be a local function and h~(ρ)=Eνρ[h]\tilde{h}(\rho)=E_{\nu_{\rho}}[h]. Then, for t[0,T]t\in[0,T],

limlimN𝔼μN[|0t1NxG(s,x/N)τx[h(ηNs)h~(ηNs(0))]𝑑s|]=0.\lim_{\ell\rightarrow\infty}\lim_{N\rightarrow\infty}\mathbb{E}_{\mu^{N}}\Big[\Big|\int_{0}^{t}\frac{1}{N}\sum_{x}G(s,x/N)\tau_{x}\big[h(\eta_{Ns})-\tilde{h}(\eta^{\ell}_{Ns}(0))\big]ds\Big|\Big]=0.
Sketch of proof.

Consider the 11-block shown in Section 5, namely Theorem 5.2.1 with time-dependent G(s,x/N)G(s,x/N) replacing J(x/N)J(x/N), VV_{\ell} replacing VNϵV_{N\epsilon}, and limits limlimN\lim_{\ell\uparrow\infty}\lim_{N\uparrow} replacing limϵ0limN\lim_{\epsilon\downarrow 0}\lim_{N\uparrow\infty}. The same scheme can be followed here: With respect to the first two terms on the right-hand side of (5.3.1), continuity of G(s,x/N)G(s,x/N) in the space variable handles the first term, and as it is Proposition 5.3.2 takes care of the second term.

A difference is that the time scaling previously was v(N)=N2v(N)=N^{2}. Although this was important for the later 22-block estimate Proposition 5.3.3, for the 11-block estimate, the Euler scale v(N)=Nv(N)=N suffices. Indeed, we will now obtain the Dirichlet form of the density is of order O(Nd1)O(N^{d-1}), instead of O(Nd2)O(N^{d-2}) when v(N)=N2v(N)=N^{2}. Such an O(Nd1)O(N^{d-1}) estimate is enough to obtain the 11-block limit. These computations are left to the reader. ∎

By Proposition 6.2.3, applied with h(η)=η(1)(1η(0)CLOSEh(\eta)=\eta(1)(1-\eta(0), η(0)\eta(0), and 1η(0)1-\eta(0), and GG in terms of ρ(t,u)\rho(t,u), we may bound

1NH(t)1NH(0)\displaystyle\frac{1}{N}H(t)-\frac{1}{N}H(0)
0tEμsN[1Nx{η(x)(1η(x))uρρ(1ρ)(s,x/N)\displaystyle\quad\leq\int_{0}^{t}E_{\mu^{N}_{s}}\Big[\frac{1}{N}\sum_{x}\Big\{\eta^{\ell}(x)(1-\eta^{\ell}(x))\frac{-\partial_{u}\rho}{\rho(1-\rho)}(s,x/N)
η(x)(2ρ1)uρρ(s,x/N)+(1η(x))(2ρ1)uρ1ρ(s,x/N)}]ds+o(1)\displaystyle\quad\quad\quad-\eta^{\ell}(x)\frac{(2\rho-1)\partial_{u}\rho}{\rho}(s,x/N)+(1-\eta^{\ell}(x))\frac{(2\rho-1)\partial_{u}\rho}{1-\rho}(s,x/N)\Big\}\Big]ds+o(1)
=0tEμsN[1Nxuρ(s,x/N)F(η(x),ρ(t,x/N))]𝑑s+o(1)\displaystyle\quad=\int_{0}^{t}E_{\mu^{N}_{s}}\Big[\frac{1}{N}\sum_{x}\partial_{u}\rho(s,x/N)F\Big(\eta^{\ell}(x),\rho(t,x/N)\Big)\Big]ds+o(1) (6.2.3)

where, for m,ρ[0,1]m,\rho\in[0,1],

F(m,ρ)=m(1m)ρ(1ρ)m(2ρ1)ρ+(1m)(2ρ1)1ρ.F(m,\rho)=-\frac{m(1-m)}{\rho(1-\rho)}-\frac{m(2\rho-1)}{\rho}+\frac{(1-m)(2\rho-1)}{1-\rho}.

Observe that

mF(m,ρ)=12mρ(1ρ)2ρ1ρ2ρ11ρ\partial_{m}F(m,\rho)=-\frac{1-2m}{\rho(1-\rho)}-\frac{2\rho-1}{\rho}-\frac{2\rho-1}{1-\rho}

and that it vanishes when m=ρm=\rho. Hence,

|F(m,ρ)F(ρ,ρ)|C|mρ|2\big|F(m,\rho)-F(\rho,\rho)\big|\leq C\big|m-\rho\big|^{2}

with respect to a constant CC.

Subtracting and adding terms F(ρ(s,x/N),ρ(s,x/N))1F(\rho(s,x/N),\rho(s,x/N))\equiv-1 in the summation (6.2) is negligible: Indeed,

1Nxuρ(s,x/N)F(ρ(s,x/N),ρ(s,x/N))\displaystyle\frac{1}{N}\sum_{x}\partial_{u}\rho(s,x/N)F\Big(\rho(s,x/N),\rho(s,x/N)\Big)
=1Nxuρ(s,x/N)\displaystyle\quad\quad=-\frac{1}{N}\sum_{x}\partial_{u}\rho(s,x/N)
=1Nx[N(ρ(s,(x+1)/N)ρ(t,x/N))+O(1/N)]=O(1/N).\displaystyle\quad\quad=-\frac{1}{N}\sum_{x}\Big[N\big(\rho(s,(x+1)/N)-\rho(t,x/N)\big)+O(1/N)\Big]=O(1/N).

Therefore, we have that

1NH(t)1NH(0)\displaystyle\frac{1}{N}H(t)-\frac{1}{N}H(0)
0tEμsN[1Nxuρ(s,x/N)\displaystyle\quad\quad\leq\int_{0}^{t}E_{\mu^{N}_{s}}\Big[\frac{1}{N}\sum_{x}\partial_{u}\rho(s,x/N)
×{F(η(x),ρ(s,x/N))F(ρ(s,x/N),ρ(s,x/N))}]ds+o(1)\displaystyle\quad\quad\quad\quad\times\Big\{F\Big(\eta^{\ell}(x),\rho(s,x/N)\Big)-F\Big(\rho(s,x/N),\rho(s,x/N)\Big)\Big\}\Big]ds+o(1)
0tEμsN[CuρNx|η(x)ρ(s,x/N)|2]𝑑s+o(1).\displaystyle\quad\quad\leq\int_{0}^{t}E_{\mu^{N}_{s}}\Big[\frac{C\|\partial_{u}\rho\|_{\infty}}{N}\sum_{x}\big|\eta^{\ell}(x)-\rho(s,x/N)\big|^{2}\Big]ds+o(1).

Step D. We now estimate the expectation above, via use of the entropy inequality (Lemma 4.1.2): Let C=Cuρ(s,x/N)C=C\|\partial_{u}\rho(s,x/N)\|_{\infty}. Then, with δ>0\delta>0,

EμsN[CNx|η(x)ρ(s,x/N)|2]\displaystyle E_{\mu^{N}_{s}}\Big[\frac{C}{N}\sum_{x}\big|\eta^{\ell}(x)-\rho(s,x/N)\big|^{2}\Big]
CδNH(s)+CδNlogEνsN[exp{δx|η(x)ρ(s,x/N)|2}].\displaystyle\quad\quad\leq\frac{C}{\delta N}H(s)+\frac{C}{\delta N}\log E_{\nu^{N}_{s}}\Big[\exp\Big\{\delta\sum_{x}\big|\eta^{\ell}(x)-\rho(s,x/N)\big|^{2}\Big\}\Big].

The variables {η(x):x𝕋N}\{\eta^{\ell}(x):x\in{\mathbb{T}}_{N}\} are 2+12\ell+1-dependent. To gain some independence, divide the interval {0,,N1}\{0,\ldots,N-1\} into N/(2+1)\lceil N/(2\ell+1)\rceil blocks of width 2+12\ell+1, where the possible last block may be of length less than 2+12\ell+1. We may separate the sum over x𝕋Nx\in{\mathbb{T}}_{N} as a sum over zz such that |z||z|\leq\ell and wΠN,z,w\in\Pi_{N,z,\ell} where ΠN,z,\Pi_{N,z,\ell} refers to the set {z+(2+1)r:r=0,,N/(2+1)1}\{z+(2\ell+1)r:r=0,\ldots,\lfloor N/(2\ell+1)\rfloor-1\}, and also a sum over the remaining O()O(\ell) indices in the possible overflow block Π\Pi^{\prime}.

Let qx=|η(x)ρ(s,x/N)|2q_{x}=\big|\eta^{\ell}(x)-\rho(s,x/N)\big|^{2}. The sum corresponding to the overflow block can be bounded xΠqxC1\sum_{x\in\Pi^{\prime}}q_{x}\leq C_{1}\ell. We may also center qx2|η(x)ρ(s,x/N)|2+2|ρ(s,x/N)ρ(s,x/N)|2q_{x}\leq 2\big|\eta^{\ell}(x)-\rho^{\ell}(s,x/N)\big|^{2}+2\big|\rho^{\ell}(s,x/N)-\rho(s,x/N)\big|^{2} where ρ(s,x/N)=(2+1)1|y|ρ(s,(y+x)/N)\rho^{\ell}(s,x/N)=(2\ell+1)^{-1}\sum_{|y|\leq\ell}\rho(s,(y+x)/N). Note |ρ(s,(x+y)/N)ρ(s,x/N)|Cuρ/N|\rho(s,(x+y)/N)-\rho(s,x/N)|\leq C\|\partial_{u}\rho\|_{\infty}\ell/N for |y||y|\leq\ell.

Then, for each |z||z|\leq\ell, since {qw:wΠN,z,}\{q_{w}:w\in\Pi_{N,z,\ell}\} are independent, by Hölder’s inequality,

1NlogEνsN[exp{δxqx}]\displaystyle\frac{1}{N}\log E_{\nu^{N}_{s}}\Big[\exp\Big\{\delta\sum_{x}q_{x}\Big\}\Big]
1N|z|wΠ(N,z,)logEνsN[exp{2δ|η(w)ρ(s,w)|2}]\displaystyle\quad\leq\frac{1}{N\ell}\sum_{|z|\leq\ell}\sum_{w\in\Pi(N,z,\ell)}\log E_{\nu^{N}_{s}}\Big[\exp\Big\{2\delta\ell\big|\eta^{\ell}(w)-\rho^{\ell}(s,w)\big|^{2}\Big\}\Big]
+C1δN+C(uρ)δN.\displaystyle\quad\quad\quad+\frac{C_{1}\delta\ell}{N}+\frac{C(\|\partial_{u}\rho\|_{\infty})\delta\ell}{N}.

Step E. We now apply a concentration inequality for subgaussian random variables. We say XX is σ2\sigma^{2}-subgaussian if

logE[eθX]σ2θ2/2\log E\big[e^{\theta X}\big]\leq\sigma^{2}\theta^{2}/2

for all θ\theta\in\mathbb{R}.

Lemma 6.2.4.

Let XX be σ2\sigma^{2}-subgaussian. Then, if γ(4σ2)1\gamma\leq(4\sigma^{2})^{-1},

E[eγX2]3.E\big[e^{\gamma X^{2}}\big]\leq 3.

In our context, the variable Xw:=(η(w)ρ(s,w/N))X_{w}:=\sqrt{\ell}\big(\eta^{\ell}(w)-\rho^{\ell}(s,w/N)\big), with respect to νsN\nu^{N}_{s}, is subgaussian with parameter

σ2(w)=2(2l+1)|yw|lρ(s,y/N)(1ρ(s,y/N)).\sigma^{2}(w)=\frac{2}{(2l+1)}\sum_{|y-w|\leq l}\rho(s,y/N)\big(1-\rho(s,y/N)\big).
Exercise 6.2.5.

Show Lemma 6.2.4. Also, show that XwX_{w} is subgaussion with respect to σ2(w)\sigma^{2}(w). Hint: This is Proposition E.7 in [123].

Since 0<ρρ(s,u)ρ+<10<\rho_{-}\leq\rho(s,u)\leq\rho_{+}<1 on [0,T]×𝕋[0,T]\times{\mathbb{T}}, we have 0<2ρ(1ρ+)σ2(w)2ρ+(1ρ)<10<2\rho_{-}\big(1-\rho_{+})\leq\sigma^{2}(w)\leq 2\rho_{+}\big(1-\rho_{-}\big)<1. Then,

EνsN[exp{2δl|η(w)ρ(s,w/N)|2}]3E_{\nu^{N}_{s}}\Big[\exp\Big\{2\delta l\big|\eta^{\ell}(w)-\rho^{\ell}(s,w/N)\big|^{2}\Big\}\Big]\leq 3

when 2δ<1/[8ρ+(1ρ)]2\delta<1/[8\rho_{+}(1-\rho_{-})].

Hence, for such a δ\delta,

1δNlogEνsN[exp{δxqx}]\displaystyle\frac{1}{\delta N}\log E_{\nu^{N}_{s}}\Big[\exp\Big\{\delta\sum_{x}q_{x}\Big\}\Big] ϵ(N,,δ):=Cδ+CN,\displaystyle\leq\epsilon(N,\ell,\delta):=\frac{C}{\delta\ell}+\frac{C\ell}{N},

which vanishes as NN\uparrow\infty and then \ell\uparrow\infty.

Step F. Putting things together, we observe that the entropy is bounded as

1N(H(t)H(0))CNδ0tH(s)𝑑s+ϵ(N,,δ)t.\displaystyle\frac{1}{N}\big(H(t)-H(0)\big)\leq\frac{C}{N\delta}\int_{0}^{t}H(s)ds+\epsilon(N,\ell,\delta)t.

We have taken the initial distribution to be ν0N\nu^{N}_{0}, in which case H(0)=0H(0)=0 (an estimate H(0)=o(N)H(0)=o(N) with respect to the initial condition would also suffice). By Gronwall’s bound, we conclude as desired that

1NH(t)(δ/C)eCδ1Tϵ(N,,δ)T=o(1)\frac{1}{N}H(t)\leq(\delta/C)e^{C\delta^{-1}T}\epsilon(N,\ell,\delta)T=o(1)

as NN\uparrow\infty and ll\uparrow\infty. ∎

6.3. Notes

We have followed the scheme in [213], although there are differences; see also Chapter VI in [130]. The hydrodynamic limit presented in Theorem 6.1.1 may be extended to all times t0t\geq 0, by different methods, where ρ(t,u)\rho(t,u) is the ‘physical’ solution mentioned earlier. See for instance [182], when starting from a ‘step’ initial profile u0=1(u0)u_{0}=1(u\leq 0), and [10], [179] for general initial data.

However, in general, hydrodynamics for all times has not been shown for processes with drift in Euler scale υ(N)=N\upsilon(N)=N that do not satisfy the ‘basic coupling’ or are not ‘attractive’ in the sense given in Subsection 4.4. It is an open problem to show such hydrodynamics. Here, TASEP can be verified to be ‘attractive’, used in [10], [179]. See also [199] for hydrodynamics of long-range asymmetric exclusion and other processes.

The ‘relative entropy’ method is due to H.T. Yau [221]. Other treatments of the method in different contexts may be found in [130], [83]. Instead of using the concentration inequality for the last argument, one may invoke large deviations bounds as in [130] for instance.

While the ‘entropy’ method of Guo-Papanicolaou-Varadhan [106] presented in Section 5 yields existence of a weak solution to the hydrodynamic partial differential equation, the ‘relative entropy’ method shows uniqueness of classical solutions of the hydrodynamic equation: Although a requirement for the method is that a priori some smoothness of the hydrodynamic PDE solution is known.

Interestingly, explicit knowledge of the invariant measures of the process is not needed for the relative entropy method, as Lemma 6.2.2 holds generally with respect to a reference measure ν\nu_{*} (we used ν1/2\nu_{1/2} here for convenience) and approximations νtN\nu^{N}_{t} of μtN\mu^{N}_{t}; see [123][Lemma A.1] for the original derivation.

The relative entropy method has been helpful in several other problems, from deriving mean-curvature flows [89], [64], [87], [88], [84] to non-equilibrium fluctuations [53], [123]. Here, the negative Dirichlet term in Lemma 6.2.2 is useful in the estimations.

Section 7 Construction of particle systems in infinite volume

We construct, using the method of Liggett and Spitzer [151] and Andjel [5], zero-range particle systems on d\mathbb{Z}^{d}. The approach is to take a limit of the processes restricted to large but finite sets. Such a construction would also hold for exclusion and related models. Other construction techniques are mentioned in the Notes subsection.

7.1. What does it mean to construct a process?

In Section 1, on finite or countable state spaces Ω\Omega, ‘construction of the process’ meant determining the transition probabilities Pt(x,y)=P(η(t)=y|η(0)=x)P_{t}(x,y)=P(\eta(t)=y|\eta(0)=x) of a Markov chain, in terms of infinitesimal rates, from which probabilities P(η(t)A|η(0)=x)P(\eta(t)\in A|\eta(0)=x) could be found for AΩA\subset\Omega. One could then write down then the semigroup operator PtP_{t}, acting on bounded functions, and understand its connection to the generator LL in terms of backward and forward equations.

On more exotic spaces Ω\Omega, to construct a Markov process usually means building a semigroup PtP_{t}, that is an operator, with the ‘Chapman-Kolmogorov’ property Pt+s=PtPsP_{t+s}=P_{t}P_{s} for s,t0s,t\geq 0, acting on a collection of functions on Ω\Omega, and relating PtP_{t} to a generator LL via backward and forward evolution equations. In this context, one can usually associate, by Kolmogorov’s extension theorem, a probability Pη[η(t)dζ]P^{\eta}[\eta(t)\in d\zeta], with initial condition η\eta, on the Borel sets in Ω\Omega. Sometimes, we will want the semigroup PtP_{t} to have certain properties, such as ‘strong continuity’ or the ‘Feller property’, but this is not guaranteed (cf. [145][p. 247]).

For the particle systems we have studied, exclusion and zero-range models, we would like to extend the background space 𝕋Nd{\mathbb{T}}^{d}_{N} to d\mathbb{Z}^{d}. Then, the configuration space would be Ω={0,1}d\Omega=\{0,1\}^{{\mathbb{Z}^{d}}} for exclusion systems, and Ω=0d\Omega=\mathbb{N}_{0}^{{\mathbb{Z}^{d}}} for zero-range models. With respect to exclusion systems, Ω\Omega is compact, which is helpful and allows different ways to construct the process. However, for zero-range models, since Ω\Omega is not compact, some care must be taken and assumptions on the parameters, namely the rate function gg and transition probability pp, should be made.

Interestingly, if gg is in general unbounded, but Lipschitz, not all configurations ηΩ\eta\in\Omega may be ‘allowed‘. In other words, we will construct the zero-range process on a strict subset ΩΩ\Omega^{\prime}\subset\Omega, so that once begun in Ω\Omega^{\prime}, the process will stay in Ω\Omega^{\prime}. Part of the reason for this restriction is that if the rate function is large, particles jump faster, and the process may be influenced from particles at ‘infinity’; see the end of Section 2 in [5] for an example.

On the other hand, if gg is bounded, then the process can be constructed on the full Ω\Omega by a different method [111].

7.2. Zero-range model and statement of results

We will assume in the following that g:0+g:\mathbb{N}_{0}\rightarrow\mathbb{R}_{+} satisfies g(0)=0g(0)=0 and g(k)>0g(k)>0 for k1k\geq 1, and gg is Lipschitz: There is a constant a0a_{0} such that

  • (LIP)

    supk0|g(k+1)g(k)|a0.\sup_{k\geq 0}|g(k+1)-g(k)|\ \leq\ a_{0}.

In particular, we do not assume in this Section 7 that gg is increasing.

Also, we will take the jump probability pp on d{\mathbb{Z}^{d}} (p(x,y)0p(x,y)\geq 0 and ydp(x,y)=1\sum_{y\in{\mathbb{Z}^{d}}}p(x,y)=1) to be irreducible and such that limxp(x,y)=0\lim_{x\rightarrow\infty}p(x,y)=0 for all ydy\in{\mathbb{Z}^{d}}. Note that we do not assume that pp is translation-invariant, e.g. p(x,y)=p(0,yx)=p(yx)p(x,y)=p(0,y-x)=p(y-x), or that pp is finite-range, that is when p(x)=0p(x)=0 for |x|>R|x|>R for some R<R<\infty.

We now specify the allowed configuration space Ω\Omega^{\prime}. For xdx\in{\mathbb{Z}^{d}}, let

β(x)=n0p(n)(x,0)2n\beta(x)\ =\ \sum_{n\geq 0}\frac{p^{(n)}(x,0)}{2^{n}}

where p(n)(x,y)p^{(n)}(x,y) is the probability that a single particle reaches ydy\in{\mathbb{Z}^{d}} in nn steps from xx. Observe that

ydp(x,y)β(y) 2β(x).\sum_{y\in{\mathbb{Z}^{d}}}p(x,y)\beta(y)\ \leq\ 2\beta(x). (7.2.1)
Exercise 7.2.1.

Show (7.2.1).

Define for η,ζΩ=0d\eta,\zeta\in\Omega=\mathbb{N}_{0}^{\mathbb{Z}^{d}} the norm

ηζ=xd|η(x)ζ(x)|β(x).\|\eta-\zeta\|\ =\ \sum_{x\in{\mathbb{Z}^{d}}}|\eta(x)-\zeta(x)|\beta(x).

The collection of allowed configurations will be

Ω={ηΩ|η=xdη(x)β(x)<}.\Omega^{\prime}\ =\ \Big\{\eta\in\Omega|\|\eta\|=\sum_{x\in{\mathbb{Z}^{d}}}\eta(x)\beta(x)<\infty\Big\}. (7.2.2)

Examples of configurations in Ω\Omega^{\prime} include those with only a finite number of particles, for instance: We say a configuration η\eta is finite if the number of particles xdη(x)<\sum_{x\in{\mathbb{Z}^{d}}}\eta(x)<\infty.

We now define a class of ‘Lipschitz’ functions on which we construct the process. We say that f:Ωf:\Omega^{\prime}\rightarrow\mathbb{R} is Lipschitz if there is a constant cc such that

|f(η)f(ζ)|cηζ|f(\eta)-f(\zeta)|\ \leq\ c\|\eta-\zeta\|

for all η,ζΩ\eta,\zeta\in\Omega^{\prime}. Let c(f)c(f) be the smallest such constant cc.

Denote by \mathcal{L} the collection of all Lipschitz functions on Ω\Omega^{\prime}. Note that \mathcal{L} includes ‘simple’ functions, those say depending on a finite number of variables η(x)\eta(x) and taking on a finite number of values. Moreover, trivially, f(η)=ηf(\eta)=\|\eta\| belongs to \mathcal{L} with c(f)=1c(f)=1.

Define the operator LL, which we will identify later as our generator, on functions in \mathcal{L} and ηΩ\eta\in\Omega^{\prime} by

(Lf)(η)=x,ydp(y)g(η(x))[f(ηx,x+y)f(η(x))].(Lf)(\eta)\ =\ \sum_{x,y\in{\mathbb{Z}^{d}}}p(y)g(\eta(x))\big[f(\eta^{x,x+y})-f(\eta(x))\big].
Lemma 7.2.2.

The operator LL is well defined for ff\in\mathcal{L} and ηΩ\eta\in\Omega^{\prime}, and

|Lf(η)| 3a0c(f)η.|Lf(\eta)|\ \leq\ 3a_{0}c(f)\|\eta\|.
Proof.

Note that ηx,x+yη=β(x+y)+β(x)\|\eta^{x,x+y}-\eta\|=\beta(x+y)+\beta(x). The desired estimate follows from

|Lf(η)|\displaystyle|Lf(\eta)| \displaystyle\leq x,yp(x,x+y)g(η(x))|f(ηx,x+y)f(η)|\displaystyle\sum_{x,y}p(x,x+y)g(\eta(x))\big|f(\eta^{x,x+y})-f(\eta)\big|
\displaystyle\leq c(f)x,yp(x,x+y)g(η(x))(β(x+y)β(x))\displaystyle c(f)\sum_{x,y}p(x,x+y)g(\eta(x))\big(\beta(x+y)-\beta(x)\big)
\displaystyle\leq a0c(f)x,yp(x,x+y)η(x)(β(x+y)+β(x))\displaystyle a_{0}c(f)\sum_{x,y}p(x,x+y)\eta(x)\big(\beta(x+y)+\beta(x)\big)
\displaystyle\leq 3a0c(f)η\displaystyle 3a_{0}c(f)\|\eta\|

using (LIP), and (7.2.1) in the last step. ∎

We now come to the main theorems.

Theorem 7.2.3.

There exists a semigroup PtP_{t} on \mathcal{L}, which has specification Ptf(η)=Eη[f(ηt)]P_{t}f(\eta)=E^{\eta}[f(\eta_{t})] for ff\in\mathcal{L} and finite configurations η\eta in terms of the countable-state process.

Moreover, for η,ζΩ\eta,\zeta\in\Omega^{\prime} and ff\in\mathcal{L}, the semigroup satisfies

|Ptf(η)Ptf(ζ)|c(f)e4a0tηζ\big|P_{t}f(\eta)-P_{t}f(\zeta)\big|\ \leq\ c(f)e^{4a_{0}t}\|\eta-\zeta\|

and c(Ptf)c(f)e4a0tc(P_{t}f)\leq c(f)e^{4a_{0}t}. Also,

Ptf(η)=f(η)+0tLPsf(η)𝑑s.P_{t}f(\eta)\ =\ f(\eta)+\int_{0}^{t}LP_{s}f(\eta)ds.

We observe, when there are only a finite number of particles in the system, PtP_{t} and LL are the semigroup and generator of a countable state Markov chain.

More properties are given in the following result.

Theorem 7.2.4.

We have for ff\in\mathcal{L} and ηΩ\eta\in\Omega^{\prime} that

  • (i)

    |LPsf(η)|3c(f)e4a0sη|LP_{s}f(\eta)|\leq 3c(f)e^{4a_{0}s}\|\eta\| and |Ptf(η)f(η)|(4a0)1c(f)η(e4a0t1)|P_{t}f(\eta)-f(\eta)|\leq(4a_{0})^{-1}c(f)\|\eta\|(e^{4a_{0}t}-1)

  • (ii)

    limt0t1[Ptf(η)f(η)]=Lf(η)\lim_{t\downarrow 0}t^{-1}\big[P_{t}f(\eta)-f(\eta)\big]=Lf(\eta)

  • (iii)

    LPtf(η)=PtLf(η)LP_{t}f(\eta)=P_{t}Lf(\eta).

We prove Theorems 7.2.3 and 7.2.4 in Subsections 7.4.1, and 7.4.2.

7.2.1. The meaning of Theorem 7.2.3

Recall that ‘simple’ or cylinder functions, f(η)=j=1k1Aj(η(xj))f(\eta)=\prod_{j=1}^{k}1_{A_{j}}(\eta(x_{j})) for Aj0A_{j}\subset\mathbb{N}_{0} and {xj}j=1kd\{x_{j}\}_{j=1}^{k}\subset{\mathbb{Z}^{d}}, k<k<\infty, are Lipschitz functions. Since, for a given ηΩ\eta\in\Omega^{\prime}, one may approximate η\eta by finite configurations ζn\zeta^{n} such that ηζn0\|\eta-\zeta^{n}\|\downarrow 0 as nn\uparrow\infty, by Theorem 7.2.3, the semigroup Ptf(η)P_{t}f(\eta) may be computed from that of countable state Markov chains: Ptf(η)=limPtf(ζn)=limEζn[f(ηt]P_{t}f(\eta)=\lim P_{t}f(\zeta^{n})=\lim E^{\zeta^{n}}[f(\eta_{t}]. Therefore, the finite dimensional distributions of (ηt(x),t0,xd)(\eta_{t}(x),t\geq 0,x\in{\mathbb{Z}^{d}}) for a given initial configuration ηΩ\eta\in\Omega^{\prime} may be identified.

Then, by Kolmogorov’s extension theorem, there exists a probability measure Pη[η(t)dζ]P^{\eta}[\eta(t)\in d\zeta] on Borel sets in Ω\Omega (not necessarily for the moment on Ω\Omega^{\prime}!) for each t0t\geq 0 and ηΩ\eta\in\Omega^{\prime} such that

Ptf(η)=Pη[ηtdζ]f(ζ)=Eη[f(ηt)]P_{t}f(\eta)\ =\ \int P^{\eta}[\eta_{t}\in d\zeta]f(\zeta)\ =\ E^{\eta}[f(\eta_{t})] (7.2.3)

for cylinder functions ff.

Lemma 7.2.5.

For ηΩ\eta\in\Omega^{\prime}, we have Eη[ηt]<E^{\eta}\big[\|\eta_{t}\|\big]<\infty, and therefore the measure Pη[ηtdζ]P^{\eta}[\eta_{t}\in d\zeta] concentrates on Ω\Omega^{\prime}.

Proof.

We apply Theorem 7.2.3 to the function f(η)=ηf(\eta)=\|\eta\| belonging to \mathcal{L} with c(f)=1c(f)=1. Hence,

e4a0tη|Ptf(η)|=|Eη[f(ηt)]|=Eη[ηt]e^{4a_{0}t}\|\eta\|\ \geq\ |P_{t}f(\eta)|\ =\ |E^{\eta}[f(\eta_{t})]|\ \ =\ E^{\eta}\big[\|\eta_{t}\|\big]

and so ηt<\|\eta_{t}\|<\infty a.s. starting from η\eta. ∎

Lemma 7.2.6.

For ηΩ\eta\in\Omega^{\prime}, we may identify for f0f\geq 0 or ff\in\mathcal{L} that

Ptf(η)=Pη[ηtdζ]f(ζ)=Eη[f(ηt)].P_{t}f(\eta)\ =\ \int P^{\eta}[\eta_{t}\in d\zeta]f(\zeta)\ =\ E^{\eta}[f(\eta_{t})].
Proof.

When f0f\geq 0, one can approximate ff by nonnegative simple functions (belonging to \mathcal{L}). Then, by monotone convergence, one may take a limit in (7.2.3), and define Ptf(η)P_{t}f(\eta) in this way.

When ff\in\mathcal{L}, however, not necessarily positive, we may still approximate f(η)f(\eta) by simple functions in \mathcal{L}, dominated by |f(η)||f(\eta)| pointwise for ηΩ\eta\in\Omega^{\prime}. Since |f(η)|c(f)η+|f(0)||f(\eta)|\leq c(f)\|\eta\|+|f(0)| when ηΩ\eta\in\Omega^{\prime}, the point is that, by Lemma 7.2.5 ηη\eta\mapsto\|\eta\| is integrable, and so we can pass to the limit in (7.2.3) to define Ptf(η)P_{t}f(\eta). ∎

7.3. Construction estimates on a finite cube

The strategy to construct an infinite volume semigroup PtP_{t} is first to obtain estimates on the semigroup and generator which are well defined when the space is finite, and then use these estimates to define PtP_{t} as the volume grows. Throughout this subsection, the underlying space will be a cube of width 2L+12L+1:

AL={x:|xi|L,1id}.A_{L}\ =\ \big\{x:|x_{i}|\leq L,1\leq i\leq d\big\}.

Let Pt=Pt(A)P_{t}=P_{t}^{(A)} and ηt=ηt(A)\eta_{t}=\eta_{t}^{(A)} be the (countable-state) zero-range process corresponding to a transition probability p(x,y)=pA(x,y)p(x,y)=p_{A}(x,y) on A=ALA=A_{L}, with no transitions from AA to AcA^{c}.

We now bound the means of such a process at times t0t\geq 0.

Lemma 7.3.1.

For t0t\geq 0, and yAy\in A, we have

Eη[ηt(y)]xAη(x)=0(a0t)!p()(x,y).E^{\eta}[\eta_{t}(y)]\ \leq\ \sum_{x\in A}\eta(x)\sum_{\ell=0}^{\infty}\frac{(a_{0}t)^{\ell}}{\ell!}p^{(\ell)}(x,y).

Here, p()(x,y)p^{(\ell)}(x,y) is the \ell-step transition probability from xx to yy.

Proof.

The argument is by coupling the zero-range process to a continuous-time multitype branching process ηt+\eta^{+}_{t} on 0A\mathbb{N}_{0}^{A} with generator

L+f(η+)=x,ya0η(x)p(x,x+y)[f(η++δx+y)f(η+)].L^{+}f(\eta^{+})\ =\ \sum_{x,y}a_{0}\eta(x)p(x,x+y)\big[f(\eta^{+}+\delta_{x+y})-f(\eta^{+})\big].

Here, η++δz\eta^{+}+\delta_{z} is the configuration which adds a particle at site zz to η+\eta^{+}. Note also the sum is over x,yx,y where x,x+yAx,x+y\in A. An inspection of the formula reveals that ηt+\eta_{t}^{+} is such that each particle at xx gives birth to a new particle at rate a0a_{0}. This new particle is then displaced by yy with probability p(x,x+y)p(x,x+y). Alternatively, each particle gives birth to two new particles before it dies; one is kept at the birth location xx, and the other is displaced by yy.

The coupling of ηt\eta_{t} and ηt+\eta^{+}_{t} as follows: Since by (LIP), g(η(x))a0η(x)g(\eta(x))\leq a_{0}\eta(x), whenever a zero-range particle displaces from xx to x+yx+y, one may arrange also that the branching process gives birth at xx and creates a new particle at x+yx+y. In this way, if the two processes are started from the same initial configuration, then ηt(x)ηt+(x)\eta_{t}(x)\leq\eta_{t}^{+}(x) for all xAx\in A and t0t\geq 0.

In particular, when ηη+\eta\leq\eta^{+} coordinatewise, we have Eη[ηt(x)]Eη+[ηt+(x)]E^{\eta}[\eta_{t}(x)]\leq E^{\eta^{+}}[\eta^{+}_{t}(x)] for all xAx\in A.

To finish, we need only calculate Eη+[ηt+(x)]E^{\eta^{+}}[\eta^{+}_{t}(x)]. Observe that

ddtEη+[ηt+(x)]\displaystyle\frac{d}{dt}E^{\eta^{+}}[\eta^{+}_{t}(x)] =Eη+[L+ηt+(x)]\displaystyle=E^{\eta^{+}}\big[L^{+}\eta^{+}_{t}(x)\big]
=za0Eη+[ηt+(z)]p(z,x).\displaystyle=\sum_{z}a_{0}E^{\eta^{+}}[\eta_{t}^{+}(z)]p(z,x).

Then, wt:=(Eη+[ηt+(y)]:yA)\vec{w}_{t}:=\big(E^{\eta^{+}}[\eta_{t}^{+}(y)]:y\in A\big) satisfies w˙t=a0wtP\dot{\vec{w}}_{t}=a_{0}\vec{w}_{t}P where P=(p(z,x))P=\big(p(z,x)\big) is the transition matrix. Hence, wt=w0ea0Pt\vec{w}_{t}=\vec{w}_{0}e^{a_{0}Pt}. In particular,

Eη+[ηt+(y)]=\displaystyle E^{\eta^{+}}[\eta^{+}_{t}(y)]= xAη(x)=0(a0t)!p()(x,y).\displaystyle\sum_{x\in A}\eta(x)\sum_{\ell=0}^{\infty}\frac{(a_{0}t)^{\ell}}{\ell!}p^{(\ell)}(x,y).\qed
Lemma 7.3.2.

For t0t\geq 0 and ff\in\mathcal{L}, we have PtfP_{t}f\in\mathcal{L} and c(Ptf)c(f)e3a0tc(P_{t}f)\leq c(f)e^{3a_{0}t}.

Proof.

Consider the basic coupling in Subsection 4.4, the joint Markov process on (0A)2(\mathbb{N}_{0}^{A})^{2} generated by

L¯ϕ(η,ζ)=\displaystyle\bar{L}\phi(\eta,\zeta)= x,x+yAmin{g(η(x)),g(ζ(x))}p(x,x+y)[ϕ(ηx,x+y,ζx,x+y)ϕ(η,ζ)]\displaystyle\sum_{x,x+y\in A}\min\{g(\eta(x)),g(\zeta(x))\}p(x,x+y)\big[\phi(\eta^{x,x+y},\zeta^{x,x+y})-\phi(\eta,\zeta)\big]
+x,x+yA(g(η(x))g(ζ(x)))+p(x,x+y)[ϕ(ηx,x+y,ζ)ϕ(η,ζ)]\displaystyle\ +\ \sum_{x,x+y\in A}\big(g(\eta(x))-g(\zeta(x))\big)_{+}p(x,x+y)\big[\phi(\eta^{x,x+y},\zeta)-\phi(\eta,\zeta)\big]
+x,x+yA(g(ζ(x))g(η(x)))+p(x,x+y)[ϕ(η,ζx,x+y)ϕ(η,ζ)].\displaystyle\ +\ \sum_{x,x+y\in A}\big(g(\zeta(x))-g(\eta(x))\big)_{+}p(x,x+y)\big[\phi(\eta,\zeta^{x,x+y})-\phi(\eta,\zeta)\big].

Let P¯t\bar{P}_{t} be the coupled process semigroup. Both marginals are zero-range process, and if initially ηζ\eta\leq\zeta, then the coordinatewise ordering is preserved, η(t)ζ(t)\eta(t)\leq\zeta(t).

Now write

|Ptf(η)Pt(ζ)|=|P¯t(f(η)f(ζ)|c(f)P¯tηζCLOSE.\displaystyle|P_{t}f(\eta)-P_{t}(\zeta)|\ =\ |\bar{P}_{t}(f(\eta)-f(\zeta)|\ \leq\ c(f)\bar{P}_{t}\|\eta-\zeta\|.

We give now an estimate of the derivative of the right-hand side. Note

ηx,x+yζηζ\displaystyle\|\eta^{x,x+y}-\zeta\|-\|\eta-\zeta\| =ηζx,x+yηζ\displaystyle=\|\eta-\zeta^{x,x+y}\|-\|\eta-\zeta\|
=β(x+y)+β(x)\displaystyle=\ \beta(x+y)+\beta(x)

and ηx,x+yζx,x+yηζ=0\|\eta^{x,x+y}-\zeta^{x,x+y}\|-\|\eta-\zeta\|=0. Then, adding together the positive and negative parts of g(η(x))g(ζ(x))g(\eta(x))-g(\zeta(x)), with an application of (7.2.1), we obtain

L¯ηζ\displaystyle\bar{L}\|\eta-\zeta\| \displaystyle\leq a0x,x+yA|η(x)ζ(x)|p(x,x+y)(β(x+y)+β(x))\displaystyle a_{0}\sum_{x,x+y\in A}|\eta(x)-\zeta(x)|p(x,x+y)\big(\beta(x+y)+\beta(x)\big)
\displaystyle\leq 3a0ηζ.\displaystyle 3a_{0}\|\eta-\zeta\|.

Hence, since ddtP¯tηζ=P¯tL¯ηζ\frac{d}{dt}\bar{P}_{t}\|\eta-\zeta\|=\bar{P}_{t}\bar{L}\|\eta-\zeta\|, by comparison, we obtain

|Ptf(η)Ptf(ζ)|c(f)e3a0tηζ,|P_{t}f(\eta)-P_{t}f(\zeta)|\ \leq\ c(f)e^{3a_{0}t}\|\eta-\zeta\|,

which finishes the proof. ∎

Let now (Pt1,L1)(P^{1}_{t},L_{1}) and (Pt2,L2)(P^{2}_{t},L_{2}) be zero-range processes on AA according to jump probabilities p1p_{1} and p2p_{2} that do not allow transitions from AA to AcA^{c}.

Lemma 7.3.3.

For ff\in\mathcal{L}, we have

|(L1L2)f(η)|\displaystyle|(L_{1}-L_{2})f(\eta)|
a0c(f)x,x+yAη(x)|p1(x,x+y)p2(x,x+y)|(β(x)+β(x+y)).\displaystyle\quad\ \leq\ a_{0}c(f)\sum_{x,x+y\in A}\eta(x)|p_{1}(x,x+y)-p_{2}(x,x+y)|\big(\beta(x)+\beta(x+y)\big).
Lemma 7.3.4.

We have

Pt1f(η)Pt2f(η)=0tPs1[L1L2]Pts2f(η)𝑑s.P^{1}_{t}f(\eta)-P^{2}_{t}f(\eta)\ =\ \int_{0}^{t}P^{1}_{s}\big[L_{1}-L_{2}\big]P^{2}_{t-s}f(\eta)ds.
Exercise 7.3.5.

Prove, using previous estimates, Lemma 7.3.3. Prove also Lemma 7.3.4, noting that it is a standard inequality which holds generally for a pair of Markov processes.

Lemma 7.3.6.

For ff\in\mathcal{L}, we have

|Pt1f(η)Pt2f(η)|\displaystyle|P^{1}_{t}f(\eta)-P^{2}_{t}f(\eta)| (7.3.1)
a0c(f)0te3a0(ts)x,yPs1η(x)\displaystyle\leq\ a_{0}c(f)\int_{0}^{t}e^{3a_{0}(t-s)}\sum_{x,y}P^{1}_{s}\eta(x)
|p1(x,x+y)p2(x,x+y)|(β(x)+β(x+y))ds\displaystyle\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \cdot|p_{1}(x,x+y)-p_{2}(x,x+y)|\big(\beta(x)+\beta(x+y)\big)ds
a0c(f)0te3a0(ts)x,y[zAη(z)0(a0s)!p1()(z,x)]\displaystyle\leq\ a_{0}c(f)\int_{0}^{t}e^{3a_{0}(t-s)}\sum_{x,y}\Big[\sum_{z\in A}\eta(z)\sum_{\ell\geq 0}\frac{(a_{0}s)^{\ell}}{\ell!}p_{1}^{(\ell)}(z,x)\Big]
|p1(x,x+y)p2(x,x+y)|(β(x)+β(x+y))ds.\displaystyle\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ |p_{1}(x,x+y)-p_{2}(x,x+y)|\big(\beta(x)+\beta(x+y)\big)ds.
Proof.

The inequalities follow by applying Lemma 7.3.4, Lemma 7.3.3, and then Lemmas 7.3.2 and 7.3.1. ∎

7.4. Extension to d\mathbb{Z}^{d} and proofs of the construction theorems

Let A=ALA=A_{L} increase to L1AL=d\cup_{L\geq 1}A_{L}=\mathbb{Z}^{d}. For a transition probability pp on d\mathbb{Z}^{d}, define the modified transition probabilities:

qL(x,z)={p(x,z)ifx,zAL,xz1ifx=zALp(x,x)+wALp(x,w)ifx=zAL.q_{L}(x,z)\ =\ \left\{\begin{array}[]{rl}p(x,z)&{\rm if\ }x,z\in A_{L},x\neq z\\ 1&{\rm if\ }x=z\not\in A_{L}\\ p(x,x)+\sum_{w\not\in A_{L}}p(x,w)&{\rm if\ }x=z\in A_{L}.\end{array}\right.

Note that qLq_{L} does not allow transitions from ALA_{L} to ALcA_{L}^{c}.

It will be useful to observe that qL(x,z)p(x,z)+1(x=z)q_{L}(x,z)\leq p(x,z)+1(x=z). Hence, qLq_{L} satisfies (7.2.1) with constant 33 instead of 22.

Let Pt(L)P^{(L)}_{t} and L(A)L^{(A)} be the zero-range semigroup and generator corresponding to qLq_{L} on A=ALA=A_{L}.

Proposition 7.4.1.

For ff\in\mathcal{L} and ηΩ\eta\in\Omega^{\prime}, we have limLPt(L)f(η)\lim_{L\uparrow\infty}P^{(L)}_{t}f(\eta) converges uniformly on sets of bounded tt, sets of η\eta with bounded η\|\eta\|, and sets of functions with bounded c(f)c(f).

Proof.

We show that {Pt(L)f(η)}L1\{P^{(L)}_{t}f(\eta)\}_{L\geq 1} forms a Cauchy sequence with the uniformity properties. Consider p1=qLp_{1}=q_{L} and p2=qLp_{2}=q_{L^{\prime}}, where LLL\leq L^{\prime}. Both p1,p2p_{1},p_{2} are transition probabilities on ALA_{L^{\prime}}. We have that the integrand in (7.3.1) is bounded by

e3a0(ts)xAL[zALη(z)0(a0s)!qL()(z,x)](2+23)β(x)\displaystyle e^{3a_{0}(t-s)}\sum_{x\in A_{L^{\prime}}}\Big[\sum_{z\in A_{L^{\prime}}}\eta(z)\sum_{\ell\geq 0}\frac{(a_{0}s)^{\ell}}{\ell!}q_{L}^{(\ell)}(z,x)\Big](2+2\cdot 3)\beta(x)
8e3a0(ts)zALη(z)0(3a0s)!β(z) 8e3a0tη.\displaystyle\ \ \leq\ 8e^{3a_{0}(t-s)}\sum_{z\in A_{L^{\prime}}}\eta(z)\sum_{\ell\geq 0}\frac{(3a_{0}s)^{\ell}}{\ell!}\beta(z)\ \leq\ 8e^{3a_{0}t}\|\eta\|.

Here, we used (7.2.1) several times.

Hence, the integrand is dominated. Given |p1(x,x+y)p2(x,x+y)|wALp(x,w)+wALp(x,w)|p_{1}(x,x+y)-p_{2}(x,x+y)|\leq\sum_{w\not\in A_{L}}p(x,w)+\sum_{w\not\in A_{L^{\prime}}}p(x,w) vanishes, the integrand vanishes pointwise for each 0st0\leq s\leq t, as L,LL,L^{\prime}\uparrow\infty.

Plugging into (7.3.1), we see that the convergence is uniform as desired. ∎

7.4.1. Proof of Theorem 7.2.3.

By Proposition 7.4.1, we may now define, for ff\in\mathcal{L} and ηΩ\eta\in\Omega^{\prime} that

Ptf(η)=limLPt(L)f(η).P_{t}f(\eta)\ =\ \lim_{L\uparrow\infty}P^{(L)}_{t}f(\eta).

Moreover, by Lemma 7.3.2, since qLq_{L} satisfies (7.2.1) with constant 33, we have

c(Pt(L)f)c(f)e4a0t.c(P^{(L)}_{t}f)\ \leq\ c(f)e^{4a_{0}t}.

Consider now the two properties stated in Theorem 7.2.3. We first establish the semigroup property for PtP_{t}: Namely, PtPs=Pt+sP_{t}P_{s}=P_{t+s} for s,t0s,t\geq 0. Already this property holds for Pt(L)P^{(L)}_{t}. It is sufficient to show for ff\in\mathcal{L} and ηΩ\eta\in\Omega^{\prime} that

limL[PtPt(L)]Ps(L)f(η)=0andlimLPt[Ps(L)Ps]f(η)=0.\lim_{L\uparrow\infty}[P_{t}-P^{(L)}_{t}]P^{(L)}_{s}f(\eta)=0\ \ {\rm and}\ \ \lim_{L\uparrow\infty}P_{t}[P^{(L)}_{s}-P_{s}]f(\eta)=0.

The first limit follows from the uniform convergence in Proposition 7.4.1, given c(Ps(L)f)c(f)e4a0sc(P^{(L)}_{s}f)\leq c(f)e^{4a_{0}s} uniformly in LL.

For the second limit, for fixed tt and ηΩ\eta\in\Omega^{\prime}, by construction, we may find by Kolmogorov’s extension theorem (as discussed in Subsection 7.2.1) a probability μ:=Pη(ηtdζ)\mu:=P^{\eta}(\eta_{t}\in d\zeta) on Ω\Omega such that ζμ(𝑑ζ)<\int\|\zeta\|\mu(d\zeta)<\infty and, for hh\in\mathcal{L},

Pth(η)=h(ζ)μ(𝑑ζ).P_{t}h(\eta)\ =\ \int h(\zeta)\mu(d\zeta).

Now observe

|Ps(L)f(η)Psf(η)|=|Ps(L)(f(η)f(0))Ps(f(η)f(0))| 2c(f)e4a0sη.|P^{(L)}_{s}f(\eta)-P_{s}f(\eta)|\ =\ |P^{(L)}_{s}(f(\eta)-f(0))-P_{s}(f(\eta)-f(0))|\ \leq\ 2c(f)e^{4a_{0}s}\|\eta\|.

Hence, by dominated convergence,

Pt[Ps(L)Ps]f(η)=[Ps(L)f(ζ)Psf(ζ)]μ(𝑑ζ) 0.P_{t}[P^{(L)}_{s}-P_{s}]f(\eta)=\int[P^{(L)}_{s}f(\zeta)-P_{s}f(\zeta)]\mu(d\zeta)\ \rightarrow\ 0.

To establish the integral property, note that it holds for the finite-volume semigroup Pt(L)P^{(L)}_{t} and generator L(AL)L^{(A_{L})}:

Pt(L)f(η)f(η)=0tL(AL)Ps(L)f(η)𝑑s.P^{(L)}_{t}f(\eta)-f(\eta)\ =\ \int_{0}^{t}L^{(A_{L})}P^{(L)}_{s}f(\eta)ds.

We can already pass to the limit on the left-hand side. To pass on the right-hand side we need to show that

L(AL)Ps(L)f(η)LPsf(η) 0L^{(A_{L})}P^{(L)}_{s}f(\eta)-LP_{s}f(\eta)\ \rightarrow\ 0 (7.4.1)

and that the the integrand is dominated. Domination holds as

|L(AL)Ps(L)f(η)| 3a0c(f)e4a0sη.|L^{(A_{L})}P^{(L)}_{s}f(\eta)|\ \leq\ 3a_{0}c(f)e^{4a_{0}s}\|\eta\|. (7.4.2)

We leave to the reader to show (7.4.1). ∎

Exercise 7.4.2.

Show (7.4.1) using estimates developed, and the explicit form of LL. Hint: See the argument of Lemma 2.12 in [151].

7.4.2. Proof of Theorem 7.2.4

We will use the previous estimates to show the items in Theorem 7.2.4.

Proof of (i). From Lemma 7.2.2 and Theorem 7.2.3 (see also (7.4.1) and (7.4.2)), we have that

|LPsf(η)| 3c(f)e4a0sη.|LP_{s}f(\eta)|\ \leq\ 3c(f)e^{4a_{0}s}\|\eta\|.

Now, plugging into the integral expression in Theorem 7.2.3, and integrating, we complete (i).

Proof of (ii). If we can show that LPsf(η)LP_{s}f(\eta) is continuous at t=0t=0, then (ii) follows from the integral formula in Theorem 7.2.3. Now, from part (i), PtP_{t} is continuous at t=0t=0. Write

LPsf(η)=x,x+yg(η(x))p(x,x+y)[Psf(ηx,x+y)Psf(η)].LP_{s}f(\eta)\ =\ \sum_{x,x+y}g(\eta(x))p(x,x+y)\big[P_{s}f(\eta^{x,x+y})-P_{s}f(\eta)\big].

To show continuity of LPsf(η)LP_{s}f(\eta), we dominate

|Psf(ηx,x+y)Psf(η)|c(Psf)|ηx,x+yη|c(f)e3a0t[β(x+y)+β(x)].|P_{s}f(\eta^{x,x+y})-P_{s}f(\eta)|\ \leq\ c(P_{s}f)\|\eta^{x,x+y}-\eta\|\ \leq\ c(f)e^{3a_{0}t}[\beta(x+y)+\beta(x)].

The right-hand side bound is summable:

x,x+yg(η(x))p(x,x+y)[β(x+y)+β(x)] 3a0η.\sum_{x,x+y}g(\eta(x))p(x,x+y)[\beta(x+y)+\beta(x)]\ \leq\ 3a_{0}\|\eta\|.

Hence, the desired continuity follows from dominated convergence.

Proof of (iii). Write

LPtf(η)\displaystyle LP_{t}f(\eta) =\displaystyle= lims0s1[PsPtf(η)Ptf(η)]\displaystyle\lim_{s\downarrow 0}s^{-1}\big[P_{s}P_{t}f(\eta)-P_{t}f(\eta)\big]
=\displaystyle= lims0PtPsffs(η)\displaystyle\lim_{s\downarrow 0}P_{t}\frac{P_{s}f-f}{s}(\eta)
=\displaystyle= PtLf(η).\displaystyle P_{t}Lf(\eta).

The first equality is from part (ii). The second equation is from the semigroup property proved in Theorem 7.2.3. The third equality is from dominated convergence and Lemma 7.2.6, writing Pth(η)=Eη[h(ηt)]P_{t}h(\eta)=E^{\eta}[h(\eta_{t})] for h=[Psff]/sh=[P_{s}f-f]/s. To justify these steps, we note the pointwise convergence is established already in part (ii). The domination and hh belonging to \mathcal{L} follows from part (i): For 0<s10<s\leq 1, using |ez1||z|e|z||e^{z}-1|\leq|z|e^{|z|},

|s1[Psff](η)|(4a0)1c(f)ηs1|e4a0s1|2c(f)e4a0η.\big|s^{-1}\big[P_{s}f-f\big](\eta)\big|\ \leq\ (4a_{0})^{-1}c(f)\|\eta\|s^{-1}|e^{4a_{0}s}-1|\leq 2c(f)e^{4a_{0}}\|\eta\|.

This completes the argument. ∎

7.5. Notes

The material follows [5] which is almost always cited when working with zero-range processes. On the other hand, other construction methods exist. For instance, if gg is bounded, one can construct the semigroup by the Hille-Yosida theorem as in [111]. [145] gives another way, along the lines developed above, with different estimates, to construct the semigroup. See also [14] for yet another construction.

The exclusion process can also be constructed on d\mathbb{Z}^{d} in the way above, but can be done also using the Hille-Yosida theorem; see [147]. In this setting, local functions, those which depend on a finite number of variables {η(x):xd}\{\eta(x):x\in\mathbb{Z}^{d}\}, provide a natural core for the generator.

Section 8 Invariant measures: ergodicity and extremality

We consider the invariant measures in zero-range processes on d\mathbb{Z}^{d}. Given the mass-conservative dynamics, there are several invariant measures corresponding to different particle densities. To determine them, since the set of invariant measures is a convex set, it is useful to identify extreme points of this set. In particular, if an invariant measure is an extreme point, the process run under it has interesting ergodic properties; see Subsection 8.3.

Our focus here will be to show that a class of product invariant measures νρ\nu_{\rho} are extreme points. With respect to zero-range models, many things are known, but there are still several open questions.

8.1. Invariant measures for zero-range processes

To simplify the discussion, we will assume in the remainder of Section 8 that pp is translation-invariant, but not necessarily finite-range. However, a good theory exists when pp is not translation-invariant, remarked upon in the Notes subsection. We will also keep the assumptions on gg made in Section 7: Namely, g(0)=0g(0)=0, g(k)>0g(k)>0 for k1k\geq 1, and the (LIP) condition, |g(k+1)g(k)|a0|g(k+1)-g(k)|\leq a_{0} for k0k\geq 0.

Recall the discussion of invariant measures for the zero-range process on a torus 𝕋Nd{\mathbb{T}}^{d}_{N} in Subsection 4.3. Our initial goal will be to extend these notions to d\mathbb{Z}^{d}. Recall the marginal κΨ\kappa_{\Psi} where

κΨ(k)={1Z(Ψ)Ψkg(k)!fork11Z(Ψ)fork=0\kappa_{\Psi}(k)\ =\ \left\{\begin{array}[]{rl}\frac{1}{Z(\Psi)}\frac{\Psi^{k}}{g(k)!}&\ {\rm for\ }k\geq 1\\ \frac{1}{Z(\Psi)}&\ {\rm for\ }k=0\end{array}\right.

for 0Ψ<lim infg(k)0\leq\Psi<\liminf g(k), and form the measure

ν¯Ψ=xdκΨ.\bar{\nu}_{\Psi}\ =\ \prod_{x\in\mathbb{Z}^{d}}\kappa_{\Psi}.

As before, ρ=ρ(Ψ)=Eν¯Ψ[η(0)]\rho=\rho(\Psi)=E_{\bar{\nu}_{\Psi}}[\eta(0)] is a strictly increasing function of Ψ\Psi, and hence the inverse exists. One then defines

νρ=ν¯Ψ(ρ)\nu_{\rho}\ =\ \bar{\nu}_{\Psi(\rho)}

for ρ<ρ:=limΨlim infg(k)ρ(Ψ)\rho<\rho^{*}:=\lim_{\Psi\uparrow\liminf g(k)}\rho(\Psi).

Recall Ω=0d\Omega=\mathbb{N}_{0}^{\mathbb{Z}^{d}}, and from Section 7, the norm η=xdη(x)β(x)\|\eta\|=\sum_{x\in\mathbb{Z}^{d}}\eta(x)\beta(x) where β(x)=n0p(n)(x,0)/2n\beta(x)=\sum_{n\geq 0}p^{(n)}(x,0)/2^{n}, and subset Ω={ηΩ:η<}\Omega^{\prime}=\{\eta\in\Omega:\|\eta\|<\infty\}.

Lemma 8.1.1.

We have Eνρ[η]<E_{\nu_{\rho}}\big[\|\eta\|\big]<\infty and hence the measure νρ\nu_{\rho} fully charges Ω\Omega^{\prime}, that is

νρ(Ω)= 1.\nu_{\rho}(\Omega^{\prime})\ =\ 1. (8.1.1)

Moreover, we have Eνρ[η2]<E_{\nu_{\rho}}\big[\|\eta\|^{2}\big]<\infty.

Proof.

Write

Eνρ[η]=xdEνρ[η(x)]β(x)=ρxdβ(x),E_{\nu_{\rho}}\big[\|\eta\|\big]\ =\ \sum_{x\in\mathbb{Z}^{d}}E_{\nu_{\rho}}[\eta(x)]\beta(x)\ =\ \rho\sum_{x\in\mathbb{Z}^{d}}\beta(x),

where xdβ(x)=xdn0p(n)(x,0)2n=2\sum_{x\in\mathbb{Z}^{d}}\beta(x)=\sum_{x\in\mathbb{Z}^{d}}\sum_{n\geq 0}\frac{p^{(n)}(x,0)}{2^{n}}=2, since p(n)(x,0)=p(n)(0,x)p^{(n)}(x,0)=p^{(n)}(0,-x) by translation-invariance of pp.

Moreover, by Schwarz inequality,

Eνρ[η2]\displaystyle E_{\nu_{\rho}}\big[\|\eta\|^{2}\big] =Eνρ[(xη(x)β(x))2]\displaystyle=E_{\nu_{\rho}}\Big[\Big(\sum_{x}\eta(x)\beta(x)\Big)^{2}\Big]
xβ(x)xEνρ[(η(x))2]β(x)\displaystyle\leq\sum_{x}\beta(x)\cdot\sum_{x}E_{\nu_{\rho}}\big[(\eta(x))^{2}\big]\beta(x)
4Eνρ[(η(0))2].\displaystyle\leq 4E_{\nu_{\rho}}\big[(\eta(0))^{2}\big].\qed

We now update the finite-volume definition of an invariant measure to d\mathbb{Z}^{d}. Recall the Lipschitz functions \mathcal{L} and the semigroup PtP_{t} of the process on \mathcal{L} from Section 7. We will say that a probability measure μ\mu on Ω\Omega^{\prime} is an invariant measure if

Ptf𝑑μ=f𝑑μ\int P_{t}fd\mu\ =\ \int fd\mu

for all bounded Lipschitz functions ff\in\mathcal{L}. Let \mathcal{I} denote the convex set of invariant measures for the process on d\mathbb{Z}^{d}.

Our first main theorem is the following infinite volume invariance.

Theorem 8.1.2 (Invariance).

For ρ<ρ\rho<\rho^{*}, we have νρ\nu_{\rho}\in\mathcal{I}.

8.2. Proof of the invariance of νρ\nu_{\rho} in infinite volume

It will be convenient to give a generator characterization of invariance of a measure.

Proposition 8.2.1.

Let μ\mu be a probability measure on Ω\Omega such that Eμ[η]<E^{\mu}\big[\|\eta\|\big]<\infty. Then, the following are equivalent:

  • (1)

    Lf𝑑μ=0\int Lfd\mu=0 for all bounded ff\in\mathcal{L}

  • (2)

    μ\mu\in\mathcal{I}.

In what follows, we will only use that ‘(1) implies (2)’, and so we will prove this part of the result.

Proof of Proposition 8.2.1: (1) \Rightarrow (2).

For bounded ff\in\mathcal{L}, we have by Theorem 7.2.3 that

[Ptff]𝑑μ=[0tLPsf𝑑s]𝑑μ.\int\Big[P_{t}f-f\Big]d\mu\ =\ \int\Big[\int_{0}^{t}LP_{s}fds\Big]d\mu.

Since Eμ[η]<E^{\mu}\big[\|\eta\|\big]<\infty, we have μ\mu is supported on Ω\Omega^{\prime}. For ff\in\mathcal{L} and ηΩ\eta\in\Omega^{\prime}, by Lemma 7.2.2 and Theorem 7.2.3 we have c(Psf)c(f)e4a0sc(P_{s}f)\leq c(f)e^{4a_{0}s} and

|LPsf(η)|\displaystyle|LP_{s}f(\eta)| \displaystyle\leq 3a0c(f)e4a0sη.\displaystyle 3a_{0}c(f)e^{4a_{0}s}\|\eta\|.

Moreover, as ff is bounded, PsfP_{s}f is a bounded, Lipschitz function.

By the domination, we may interchange the integrals by Fubini’s theorem. Then, given (1), we have

[0tLPsf𝑑s]𝑑μ=0t[LPsf𝑑μ]𝑑s=0\int\Big[\int_{0}^{t}LP_{s}fds\Big]d\mu\ =\ \int_{0}^{t}\Big[\int LP_{s}fd\mu\Big]ds\ =0

and so conclude (2). ∎

Remark 8.2.2.

To prove the converse, ‘(2) implies (1)’, we refer the reader to [5][Lemma 2.9].

We now assert that

νρn:=xAnκΨ(ρ)\nu^{n}_{\rho}:=\prod_{x\in A_{n}}\kappa_{\Psi(\rho)} (8.2.1)

is an invariant measure of the process with translation-invariant transition probability restricted to the finite set AnA_{n}. Indeed, this follows immediately from (the proof of) Lemma 4.3.2 in Section 4.

Proof of Theorem 8.1.2.

For a transition probability pp on d\mathbb{Z}^{d}, define the ‘truncation’ (different than in the Section 7),

pn(x,y)\displaystyle p_{n}(x,y)
={1ifx=yAnp(x,y)+Qn1[zAnp(x,z)][zAnp(z,y)]ifx,yAn0otherwise\displaystyle=\left\{\begin{array}[]{ll}1&\ {\rm if\ }x=y\not\in A_{n}\\ p(x,y)+Q_{n}^{-1}\big[\sum_{z\not\in A_{n}}p(x,z)\big]\big[\sum_{z\not\in A_{n}}p(z,y)\big]&\ {\rm if\ }x,y\in A_{n}\\ 0&\ {\rm otherwise}\end{array}\right.

where

Qn\displaystyle Q_{n} =zAn,yAnp(z,y)=zAn[1yAnp(z,y)]\displaystyle=\sum_{z\in A_{n},y\not\in A_{n}}p(z,y)=\sum_{z\in A_{n}}\Big[1-\sum_{y\in A_{n}}p(z,y)\Big]
=|An|z,yAnp(z,y)=yAn,zAnp(z,y).\displaystyle=|A_{n}|-\sum_{z,y\in A_{n}}p(z,y)=\sum_{y\in A_{n},z\not\in A_{n}}p(z,y).

We observe the following properties of pnp_{n}:

(a). First, pnp_{n} is a transition probability: ypn(x,y)=1\sum_{y}p_{n}(x,y)=1 for all xdx\in\mathbb{Z}^{d}. If xAnx\not\in A_{n}, it is trivial. If xAnx\in A_{n}, noting that Qn=zAn,yAnp(z,y)Q_{n}=\sum_{z\not\in A_{n},y\in A_{n}}p(z,y), we have ypn(x,y)=yAnp(x,y)+yAnp(x,y)=1\sum_{y}p_{n}(x,y)=\sum_{y\in A_{n}}p(x,y)+\sum_{y\not\in A_{n}}p(x,y)=1. Moreover, pnp_{n} has no transitions from AnA_{n} to its complement.

(b). In addition, xpn(x,y)=1\sum_{x}p_{n}(x,y)=1 for all ydy\in\mathbb{Z}^{d}: If yAny\not\in A_{n}, the claim is trivial. If yAny\in A_{n}, write

xpn(x,y)\displaystyle\sum_{x}p_{n}(x,y) =xAnp(x,y)+Qn1[xAn,zAnp(x,z)][zAnp(z,y)]=xp(x,y).\displaystyle=\sum_{x\in A_{n}}p(x,y)+Q_{n}^{-1}\big[\sum_{x\in A_{n},z\not\in A_{n}}p(x,z)\big]\big[\sum_{z\not\in A_{n}}p(z,y)\big]=\sum_{x}p(x,y).

The last quantity equals 11 if pp is doubly-stochastic, the case if pp is translation-invariant.

(c). Also, pnpp_{n}\rightarrow p for all x,yZdx,y\in Z^{d}. Eventually, x,yAnx,y\in A_{n}. The claim follows as Qn1zAnp(z,y)1Q_{n}^{-1}\sum_{z\not\in A_{n}}p(z,y)\leq 1.

Now, by the comments near (8.2.1), as nothing moves away from AnA_{n} when starting in AnA_{n}, we have νρ\nu_{\rho} restricted to AnA_{n} is invariant. Then, we have Eνρ[Lnf]=0E_{\nu_{\rho}}[L_{n}f]=0 for bounded ff\in\mathcal{L} where LnL_{n} is the generator for the zero-range process on AnA_{n} according to transition probability pnp_{n}. Therefore, to show Eνρ[Lf]=0E_{\nu_{\rho}}[Lf]=0, it is enough to show

Eνρ[|LnfLf|] 0.E_{\nu_{\rho}}\big[|L_{n}f-Lf|\big]\ \rightarrow\ 0.

One may write, noting (LIP), ff\in\mathcal{L}, ηx,yη=β(x)+β(y)\|\eta^{x,y}-\eta\|=\beta(x)+\beta(y) when η(x)1\eta(x)\geq 1 and xyx\neq y, and f(ηx,y)=f(η)f(\eta^{x,y})=f(\eta) for x=yx=y, that

Eνρ[|LnfLf|]\displaystyle E_{\nu_{\rho}}\big[|L_{n}f-Lf|\big] \displaystyle\leq a0c(f)xdEνρ[η(x)]yx|p(x,y)pn(x,y)|(β(x)+β(y))\displaystyle a_{0}c(f)\sum_{x\in\mathbb{Z}^{d}}E_{\nu_{\rho}}[\eta(x)]\sum_{y\neq x}|p(x,y)-p_{n}(x,y)|\big(\beta(x)+\beta(y)\big)
=\displaystyle= a0c(f)ρxdyx|p(x,y)pn(x,y)|(β(x)+β(y)).\displaystyle a_{0}c(f)\rho\sum_{x\in\mathbb{Z}^{d}}\sum_{y\neq x}|p(x,y)-p_{n}(x,y)|\big(\beta(x)+\beta(y)\big).

For fixed xyx\neq y,

|p(x,y)pn(x,y)|1(x,yAn)QnzAnp(x,z)zAnp(z,y).|p(x,y)-p_{n}(x,y)|\leq\frac{1(x,y\in A_{n})}{Q_{n}}\sum_{z\not\in A_{n}}p(x,z)\sum_{z\not\in A_{n}}p(z,y).

Hence, since zβ(z)<\sum_{z}\beta(z)<\infty and pp is doubly stochastic, the penultimate display vanishes as nn\uparrow\infty by dominated convergence. ∎

8.3. Extremality, harmonicity and ergodicity

We digress for the moment to an abstract L2L^{2} setting. Let Θ\Theta be a space with Borel sets \mathcal{B}. Let ηt\eta_{t} be a Markov process on Θ\Theta with process semigroup Ttf(η)=Eη[f(ηt)]T_{t}f(\eta)=E^{\eta}[f(\eta_{t})], acting on bounded functions ff (and well-defined extensions). We say here that QQ is an invariant measure if for all bounded functions ff on Θ\Theta (and therefore L2(Q)L^{2}(Q) functions) and t0t\geq 0, we have Ttf𝑑Q=f𝑑Q\int T_{t}fdQ=\int fdQ. Let Q\mathbb{P}_{Q} be the process measure on the path space with initial distribution QQ.

Definition 8.3.1.

We say QQ is an extremal invariant measure if the the following property holds. When for 0<ϵ<10<\epsilon<1 and invariant probability measures Q1Q_{1} and Q2Q_{2} we have Q=ϵQ1+(1ϵ)Q2Q=\epsilon Q_{1}+(1-\epsilon)Q_{2}, then Q=Q1=Q2Q=Q_{1}=Q_{2}.

We note if the process has only one invariant measure QQ, then of course it is extremal. The import of the definition comes when the process is reducible in some way. For instance, in finite state Markov chains, with exactly two irreducible components C1C_{1} and C2C_{2}, the extreme invariant measures are exactly the unique invariant measures supported on C1C_{1} and C2C_{2} respectively.

One might ask why is it useful to know when an invariant measure is extremal. It turns out there is an interesting connection with harmonic functions and shift-ergodicity.

Exercise 8.3.2.

With respect to invariant measure QQ, noting the representation Ttf(η)=Eη[f(ηt)]T_{t}f(\eta)=E^{\eta}\big[f(\eta_{t})\big], show that TtT_{t} is an L2(Q)L^{2}(Q) contraction. Let TtT^{*}_{t} be the L2(Q)L^{2}(Q) adjoint of TtT_{t}. Show also that TtT^{*}_{t} is an L2(Q)L^{2}(Q) contraction for each t0t\geq 0.

We will say that ff is harmonic, if Ttf=fT_{t}f=f for all t0t\geq 0.

Lemma 8.3.3.

The space L2(Q)L^{2}(Q) is the direct sum of I0={gL2(Q):Ttg=g,t0}I_{0}\ =\ \big\{g\in L^{2}(Q):T_{t}g=g,t\geq 0\big\} and the closure of I1={Tthh:hL2(Q),t0}I_{1}\ =\ \big\{T_{t}h-h:h\in L^{2}(Q),t\geq 0\big\}.

Proof.

Let ff be perpendicular to all functions in I¯1\bar{I}_{1}, the closure of I1I_{1}. Then, f,TthhQ=0\langle f,T_{t}h-h\rangle_{Q}=0 for all hh and t0t\geq 0. This means Ttf=fT^{*}_{t}f=f for all t0t\geq 0. Therefore, as TtT_{t} is a L2(Q)L^{2}(Q) contraction, EQ[(Ttff)2]=EQ[(Ttf)2]2EQ[f(Ttf)]+EQ[f2]2EQ[f2]2EQ[(Ttf)f]=0E_{Q}\big[(T_{t}f-f)^{2}\big]=E_{Q}\big[(T_{t}f)^{2}\big]-2E_{Q}\big[f(T_{t}f)\big]+E_{Q}\big[f^{2}\big]\leq 2E_{Q}\big[f^{2}\big]-2E_{Q}\big[(T^{*}_{t}f)f\big]=0. Hence, Ttf=fT_{t}f=f and fI0f\in I_{0} or (I¯1)I0(\bar{I}_{1})^{\perp}\subset I_{0}.

On the other hand, let fI0f\in I_{0}. Then, f,TthhQ=Ttff,hQ\langle f,T_{t}h-h\rangle_{Q}=\langle T^{*}_{t}f-f,h\rangle_{Q}. Since fI0f\in I_{0}, by a similar argument as above, we conclude EQ[(Ttff)2]0E_{Q}\big[(T^{*}_{t}f-f)^{2}\big]\leq 0 and so Ttf=fT^{*}_{t}f=f and f,TthhQ=0\langle f,T_{t}h-h\rangle_{Q}=0. Hence, I0(I¯1)I_{0}\subset(\bar{I}_{1})^{\perp}. ∎

We have the following ergodic theorem due to Von Neumann.

Proposition 8.3.4.

Let fL2(Q)f\in L^{2}(Q) and define f^L2(Q)\hat{f}\in L^{2}(Q) to be the projection onto the subspace H0H_{0}. In other words, f^\hat{f} is the conditional expectation f^=E[f|𝒯]\hat{f}=E[f|\mathcal{T}] with respect to the time-shift invariant sets 𝒯\mathcal{T}.

Then, we have the L2(Q)L^{2}(Q) convergence as tt\rightarrow\infty,

1t0tTsf𝑑sf^.\frac{1}{t}\int_{0}^{t}T_{s}f\;ds\ \rightarrow\ \hat{f}.
Proof.

Decompose f=f^+gf=\hat{f}+g where gI¯1g\in\bar{I}_{1}. Clearly, Ttf^=f^T_{t}\hat{f}=\hat{f}. Since g¯I¯1\bar{g}\in\bar{I}_{1} can be approximated by gI1g\in I_{1} in L2(Q)L^{2}(Q), we need to understand the contribution of the term gg, in form g=Tuhhg=T_{u}h-h for some hL2(Q)h\in L^{2}(Q) and u0u\geq 0. We see

1t0tTsg𝑑s=1t[tt+uTsh𝑑s0uTsh𝑑s]=O(t1)\frac{1}{t}\int_{0}^{t}T_{s}g\;ds\ =\ \frac{1}{t}\Big[\int^{t+u}_{t}T_{s}h\;ds-\int^{u}_{0}T_{s}h\;ds\Big]\ =\ O(t^{-1})

in L2(Q)L^{2}(Q) from Hölder’s inequality as TtT_{t} is an L2(Q)L^{2}(Q) contraction. ∎

We come now to the main result of the subsection. Recall Q\mathbb{P}_{Q} stands for the process measure when starting in QQ.

Proposition 8.3.5.

Let QQ be an invariant measure. All are equivalent:

  • (a)

    For sets AA\in\mathcal{B}, TtI(A)=I(A)T_{t}I(A)=I(A) QQ a.s. Q(A)=0or 1\Rightarrow Q(A)=0{\rm\ or\ }1.

  • (b)

    Q\mathbb{P}_{Q} is ergodic: For each fL2(Q)f\in L^{2}(Q), f^=EQ[f]\hat{f}=E_{Q}[f], QQ a.s.

  • (c)

    QQ is extremal.

Note that part (b) is the same as ‘time-shift ergodicity’ or in other words that the shift invariant σ\sigma-field 𝒯\mathcal{T} is trivial: Sets Λ𝒯\Lambda\in\mathcal{T} satisfy Q(Λ)=0\mathbb{P}_{Q}(\Lambda)=0 or 11.

Proof.

‘b\Rightarrowc’ Let QQ be an invariant measure whose path measure is ergodic. Write Q=ϵQ1+(1ϵ)Q2Q=\epsilon Q_{1}+(1-\epsilon)Q_{2} for 0<ϵ<10<\epsilon<1 and invariant measures Q1Q_{1} and Q2Q_{2}. Let now ff be a bounded function. Then, by (b), as tt\rightarrow\infty, 1t0t(Tsf)𝑑s\frac{1}{t}\int_{0}^{t}(T_{s}f)ds converges to EQ[f]E_{Q}[f] in L2(Q)L^{2}(Q) and therefore also in L2(Q1)L^{2}(Q_{1}). Moreover, by Proposition 8.3.4, 1t0t(Tsf)𝑑s\frac{1}{t}\int_{0}^{t}(T_{s}f)ds converges to f^\hat{f} in L2(Q1)L^{2}(Q_{1}). Hence, f^=EQ[f]\hat{f}=E_{Q}[f] Q1Q_{1} a.s. and taking expectation, EQ1[f]=EQ[f^]=EQ[f]E_{Q_{1}}[f]=E_{Q}[\hat{f}]=E_{Q}[f]. This gives Q1(B)=Q(B)Q_{1}(B)=Q(B) for BB\in\mathcal{B} and therefore Q1=QQ_{1}=Q.

‘a\Rightarrowb’ Let QQ be an invariant measure and suppose that Q\mathbb{P}_{Q} is not ergodic. Then there exists an fL2(Q)f\in L^{2}(Q) such that f^\hat{f} is not constant QQ-a.s. Let cc be such that Q(A)=ϵQ(A)=\epsilon, 0<ϵ<10<\epsilon<1 where A={f^>c}A=\{\hat{f}>c\}.

Now, as Ttf^=f^T_{t}\hat{f}=\hat{f} QQ-a.s. and TtT_{t} is a positive contraction taking 11 to 11, we have that TtI(A)=I(A)T_{t}I(A)=I(A) QQ-a.s.: Indeed, first, as TtT_{t} is a positive operator, |f^|=|Ttf^|Tt|f^||\hat{f}|=|T_{t}\hat{f}|\leq T_{t}|\hat{f}|, so that, as TtT_{t} is an L2L^{2} contraction, we have (Tt|f^||f^|)2Tt|f^|2+|f^|22|f^|Tt|f^|Tt|f^|2+|f^|22|f^|2\big(T_{t}|\hat{f}|-|\hat{f}|\big)^{2}\leq T_{t}|\hat{f}|^{2}+|\hat{f}|^{2}-2|\hat{f}|T_{t}|\hat{f}|\leq T_{t}|\hat{f}|^{2}+|\hat{f}|^{2}-2|\hat{f}|^{2}. Note also EQ[Tt|f^|2]=EQ[|f^|2]E_{Q}\big[T_{t}|\hat{f}|^{2}\big]=E_{Q}\big[|\hat{f}|^{2}\big]. Then, we have EQ[(Tt|f^||f^|)2]0E_{Q}\big[\big(T_{t}|\hat{f}|-|\hat{f}|\big)^{2}\big]\leq 0, and so QQ-a.s. Tt|f^|=|f^|T_{t}|\hat{f}|=|\hat{f}|. Therefore, max{0,f^}=(f^+|f^|)/2\max\{0,\hat{f}\}=(\hat{f}+|\hat{f}|)/2 is harmonic. Further, if f,gL2f,g\in L^{2} are harmonic, then max{f,g}=max{0,fg}+g\max\{f,g\}=\max\{0,f-g\}+g is harmonic. Correspondingly, min{f,g}=max{f,g}\min\{f,g\}=-\max\{-f,-g\} is harmonic. Of course, 11 is harmonic. All of this gives that (min{nmax(0,f^c),1})n1\big(\min\{n\max(0,\hat{f}-c),1\}\big)_{n\geq 1} is a sequence of uniformly bounded harmonic functions. The limit, as nn\rightarrow\infty, is I(A)I(A) which is therefore harmonic by dominated convergence. Hence, by (a), I(A)I(A) is constant, a contradiction.

‘c\Rightarrowa’ Let AA be such that TtI(A)=I(A)T_{t}I(A)=I(A) QQ-a.s. and Q(A)=ϵQ(A)=\epsilon for 0<ϵ<10<\epsilon<1. By this relation, the process begun on AA stays in AA and, if begun in AcA^{c} stays in AcA^{c}, with QQ-probability 11. Then, we have that Q1(B)=ϵ1Q(BA)Q_{1}(B)=\epsilon^{-1}Q(B\cap A) and Q2(B)=(1ϵ)1Q(BAc)Q_{2}(B)=(1-\epsilon)^{-1}Q(B\cap A^{c}) are distinct invariant probability measures such that Q=ϵQ1+(1ϵ)Q2Q=\epsilon Q_{1}+(1-\epsilon)Q_{2}. Therefore QQ is not extremal. ∎

8.4. Extremality of νρ\nu_{\rho}

We now address the ‘extremality’ of νρ\nu_{\rho} in the convex set of invariant measures \mathcal{I}. To do this rigorously, we will need to extend the process so that the extended semigroup TtρT_{t}^{\rho} and generator LρL^{\rho} act on L2(νρ)L^{2}(\nu_{\rho}) functions, not just Lipschitz functions \mathcal{L}. In this way, we can fit into Subsection 8.3, and in particular νρ\nu_{\rho} will be an invariant measure in this setting.

However, to present the main ideas we assume this extension has been done, and that adjoints can be taken. In the next subsection, we detail the extension to a L2(νρ)L^{2}(\nu_{\rho}) process. Recall s(x,y)=s(yx)=12(p(yx)+p(xy))s(x,y)=s(y-x)=\frac{1}{2}\big(p(y-x)+p(x-y)\big) is the symmetrized transition probability.

Theorem 8.4.1.

When s()s(\cdot) is irreducible on d\mathbb{Z}^{d}, the invariant measure νρ\nu_{\rho} is extremal.

Proof.

The idea is simple. We will need to understand the Dirichlet form of the process. In the next subsection, we show for fDom(ρ)f\in{\rm Dom}(\rho), the domain of the extended generator LρL^{\rho}, that the associated Dirichlet form satisfies

Dρ(f):=f,Lρfνρ=12x,yds(x,y)Eνρ[g(η(x))(f(ηx,y)f(η))2].D_{\rho}(f):=\langle f,-L^{\rho}f\rangle_{\nu_{\rho}}\ =\ \frac{1}{2}\sum_{x,y\in\mathbb{Z}^{d}}s(x,y)E_{\nu_{\rho}}\big[g(\eta(x))\big(f(\eta^{x,y})-f(\eta)\big)^{2}\big].

Now, let ff be a bounded harmonic function, that is when Ptρf=fP^{\rho}_{t}f=f, νρ\nu_{\rho} a.s. Hence, as the limit,

limt01t[Ptρff]= 0,\lim_{t\downarrow 0}\frac{1}{t}\big[P^{\rho}_{t}f-f\big]\ =\ 0,

(trivially) exists νρ\nu_{\rho} a.s., we conclude fDom(ρ)f\in{\rm Dom}(\rho) and Lρf=0L^{\rho}f=0, νρ\nu_{\rho} a.s.

Therefore, Dρ(f)=0D_{\rho}(f)=0, and so all summands vanish when s(x,y)>0s(x,y)>0. In particular, as g(k)>0g(k)>0 exactly when k1k\geq 1,

f(ηx,y)=f(η)a.s.νρforallx,ysuchthats(x,y)>0whenη(x)1.f(\eta^{x,y})=f(\eta){\rm\ a.s.-}\nu_{\rho}\ \ {\rm for\ all\ }x,y\ {\rm such\ that\ }s(x,y)>0{\rm\ when\ }\eta(x)\geq 1.

Consequently, ff is invariant to the motion of particles! So, by irreducibility of s()s(\cdot) and countability of d\mathbb{Z}^{d}, one has

f(ηx,y)=f(η)forallx,ya.s.νρf(\eta_{x,y})=f(\eta)\ \ {\rm for\ all\ }x,y\ {\rm a.s.-}\nu_{\rho}

where ηx,y\eta_{x,y} is the configuration which exchanges values η(x)\eta(x) and η(y)\eta(y).

Therefore, ff is finite permutation invariant. Since νρ\nu_{\rho} is a product measure with i.i.d. marginals, by Hewitt-Savage 010-1 law, ff is constant a.s.-νρ\nu_{\rho}. Inputting into Proposition 8.3.5 shows extremality. ∎

8.5. Extension to an L2(νρ)L^{2}(\nu_{\rho}) process

We first extend the semigroup defined on \mathcal{L} to L2(νρ)L^{2}(\nu_{\rho}). We define the concept of a Markov semigroup on 𝒳=L2(νρ){\mathcal{X}}=L^{2}(\nu_{\rho}).

Definition 8.5.1.

A family of linear operators PtP_{t} on 𝒳{\mathcal{X}} is a Markov semigroup if (a) P0=IP_{0}=I; (b) for f𝒳f\in{\mathcal{X}}, PtfP_{t}f is right-continuous in tt on 𝒳{\mathcal{X}}; (c) PtP_{t} satisfies the semigroup property Pt+s=PtPsP_{t+s}=P_{t}P_{s} for s,t0s,t\geq 0; (d) Pt1=1P_{t}1=1 for t0t\geq 0; (e) Ptf0P_{t}f\geq 0 for t0t\geq 0 and nonnegative f𝒳f\in{\mathcal{X}}.

Lemma 8.5.2.

PtP_{t} on \mathcal{L} extends by continuity to a Markov semigroup PtρP^{\rho}_{t} on L2(νρ)L^{2}(\nu_{\rho}).

Proof.

For ff\in\mathcal{L}, we have |f(η)|c(f)η|f(\eta)|\leq c(f)\|\eta\|, and hence L2(νρ){\mathcal{L}}\subset L^{2}(\nu_{\rho}) by Lemma 8.1.1. Also, for ff\in{\mathcal{L}}, we may write Ptf(η)=Eη[f(ηt)]P_{t}f(\eta)=E^{\eta}[f(\eta_{t})]. Therefore, by Jensen inequality, [Ptf(η)]2[Pt|f(η)|]2Ptf2(η)[P_{t}f(\eta)]^{2}\leq[P_{t}|f(\eta)|]^{2}\leq P_{t}f^{2}(\eta). Then,

PtfL2(νρ)2\displaystyle\|P_{t}f\|^{2}_{L^{2}(\nu_{\rho})} =\displaystyle= [Ptf]2dνρ\displaystyle\int[P_{t}f]^{2}d\nu_{\rho}
\displaystyle\leq Ptf2dνρ\displaystyle\int P_{t}f^{2}d\nu_{\rho}
=\displaystyle= f2dνρ=fL2(νρ)2.\displaystyle\int f^{2}d\nu_{\rho}=\|f\|^{2}_{L^{2}(\nu_{\rho})}.

Given that simple functions, those supported on finitely many variables {η(x):xd}\{\eta(x):x\in\mathbb{Z}^{d}\} and taking finitely many values, are contained in \mathcal{L}, we observe \mathcal{L} is dense in L2(νρ)L^{2}(\nu_{\rho}). Therefore, for fL2(νρ)f\in L^{2}(\nu_{\rho}), we may define PtρfP^{\rho}_{t}f as the Cauchy limit of {Ptfn}\{P_{t}f_{n}\} for a sequence of simple functions fnf_{n} which converge to ff in L2(νρ)L^{2}(\nu_{\rho}). Such an extension, given Theorems 7.2.3 and 7.2.4, fulfills the definition of a Markov semigroup on L2(νρ)L^{2}(\nu_{\rho}), details left to the reader. ∎

Exercise 8.5.3.

Verify that νρ\nu_{\rho} satisfies the definition of an invariant measure given at the beginning of Subsection 8.3 with respect to PtρP_{t}^{\rho}.

There is a one-to-one correspondence between Markov semigroups and associated generators by the Hille-Yosida theorem; see [66].

Proposition 8.5.4 (Hille-Yosida Theorem).

For a Markov semigroup TtT_{t} on L2(Q)L^{2}(Q), define

Dom\displaystyle{\rm Dom} =\displaystyle= {fL2(Q):limt0Ttfftexists}\displaystyle\big\{f\in L^{2}(Q):\lim_{t\downarrow 0}\frac{T_{t}f-f}{t}\ {\rm exists}\big\}
Lf\displaystyle Lf =\displaystyle= limt0TtfftforfDom\displaystyle\lim_{t\downarrow 0}\frac{T_{t}f-f}{t}\ {\rm for\ }f\in{\rm Dom}

Then, if fDomf\in{\rm Dom}, we have TtfDomT_{t}f\in{\rm Dom} and ddtTtf=LTtf=TtLf\frac{d}{dt}T_{t}f=LT_{t}f=T_{t}Lf.

Let LρL^{\rho} be the generator associated with semigroup PtρP_{t}^{\rho} with domain Dom(ρ){\rm Dom}(\rho).

Lemma 8.5.5.

We have Dom(ρ)\mathcal{L}\subset{\rm Dom}(\rho), LρL^{\rho} on Dom(ρ){\rm Dom}(\rho) extends LL on \mathcal{L}, and LρL^{\rho} is the closure of LL on \mathcal{L}, that is the graph of LρL^{\rho} is the closure in L2(νρ)×L2(νρ)L^{2}(\nu_{\rho})\times L^{2}(\nu_{\rho}) of the graph of LL.

Proof.

For ff\in\mathcal{L} and ηΩ\eta\in\Omega^{\prime}, by Lemma 7.2.2 and Theorem 7.2.3, we have

1t[Ptff]\displaystyle\frac{1}{t}\big[P_{t}f-f\big] =\displaystyle= 1t0tLPsf𝑑s\displaystyle\frac{1}{t}\int_{0}^{t}LP_{s}fds
\displaystyle\leq C(a0)c(f)ηt10te4a0s𝑑s.\displaystyle C(a_{0})c(f)\|\eta\|t^{-1}\int_{0}^{t}e^{4a_{0}s}ds.

Since Eνρ[η2]<E_{\nu_{\rho}}\big[\|\eta\|^{2}\big]<\infty by Lemma 8.1.1, and PtρP^{\rho}_{t} on L2(ρ)L^{2}(\rho) extends PtP_{t} on \mathcal{L}, we have by dominated convergence for ff\in\mathcal{L} that

1t[Ptρff]Lf\frac{1}{t}\big[P_{t}^{\rho}f-f\big]\ \rightarrow\ Lf

in L2(νρ)L^{2}(\nu_{\rho}) as t0t\downarrow 0. Hence, Dom(ρ)\mathcal{L}\subset{\rm Dom}(\rho), Lf=LρfLf=L^{\rho}f, and LρL^{\rho} is an extension of LL on \mathcal{L}.

Finally, as Pt:P_{t}:\mathcal{L}\rightarrow\mathcal{L} (cf. Lemma 7.2.2), and \mathcal{L} is dense in L2(νρ)L^{2}(\nu_{\rho}) and therefore in Dom(ρ){\rm Dom}(\rho), one may conclude that \mathcal{L} is a ‘core’ for LρL^{\rho}, that is the closure of LL on \mathcal{L} is equal to that of LρL^{\rho} on Dom(ρ){\rm Dom}(\rho); see [66, Lemma I.3.3]. We comment for later use that bounded functions in \mathcal{L} by the same token also form a ‘core’ for LρL^{\rho}. ∎

We now give the formula for the Dirichlet form. Recall the symmetrized transition probability s()s(\cdot).

Lemma 8.5.6.

For fDom(ρ)f\in{\rm Dom}(\rho), we have that

Dρ(f)=12x,ys(x,y)Eνρ[g(η(x))(f(ηx,y)f(η))2].D_{\rho}(f)\ =\ \frac{1}{2}\sum_{x,y}s(x,y)E_{\nu_{\rho}}\big[g(\eta(x))\big(f(\eta^{x,y})-f(\eta)\big)^{2}\big]. (8.5.1)
Proof.

We note, by the last line in the proof of Lemma 8.5.5, that bounded functions in \mathcal{L} form a ‘core’ for LρL^{\rho}. First, the formula (8.5.1) may be obtained for bounded ff\in{\mathcal{L}}, given that LfLf is explicitly defined and Dρ(f)=Eνρ[f(Lf)]D_{\rho}(f)=E_{\nu_{\rho}}\big[f(-Lf)\big], and is left as an exercise.

We now extend the representation to Dom(ρ){\rm Dom}(\rho). Let R(f)R(f) be the right-hand side of the display in the lemma. For fDom(ρ)f\in{\rm Dom}(\rho), take bounded fnf_{n}\in\mathcal{L} so that fnff_{n}\rightarrow f and LρfnLρfL^{\rho}f_{n}\rightarrow L^{\rho}f in L2(νρ)L^{2}(\nu_{\rho}). Then

limnDρ(fn)=Dρ(f),andlim infnR(fn)R(f)\lim_{n\rightarrow\infty}D_{\rho}(f_{n})=D_{\rho}(f),\ \ {\rm and}\ \ \liminf_{n\rightarrow\infty}R(f_{n})\geq R(f)

by Fatou’s lemma. Therefore, R(f)Dρ(f)R(f)\leq D_{\rho}(f) and in particular, R(f)<R(f)<\infty for fDom(ρ)f\in{\rm Dom}(\rho). However also,

0Dρ(ffn)ffnL2LρfLρfnL20\leq D_{\rho}(f-f_{n})\leq\|f-f_{n}\|_{L^{2}}\cdot\|L^{\rho}f-L^{\rho}f_{n}\|_{L^{2}}

which vanishes as nn\rightarrow\infty. Hence, limnR(ffn)=0\lim_{n\rightarrow\infty}R(f-f_{n})=0. With the inequality ab=infϵ>0{ϵa2/2+ϵ1b2/2}ab=\inf_{\epsilon>0}\big\{\epsilon a^{2}/2+\epsilon^{-1}b^{2}/2\big\}, one may bound

12x,ys(x,y)Eνρ[g(η(x))(h1(ηx,y)h1(η))(h2(ηx,y)h2(η))]R(h1)R(h2).\displaystyle\frac{1}{2}\sum_{x,y}s(x,y)E_{\nu_{\rho}}\big[g(\eta(x))\big(h_{1}(\eta^{x,y})-h_{1}(\eta)\big)\big(h_{2}(\eta^{x,y})-h_{2}(\eta)\big)\big]\leq\sqrt{R(h_{1})R(h_{2})}.

Hence, writing fn=(fnf)+ff_{n}=(f_{n}-f)+f, we may conclude limnR(fn)=R(f)\lim_{n\rightarrow\infty}R(f_{n})=R(f) to finish the proof. ∎

Exercise 8.5.7.

Show that Dρ(f)=f,LfνρD_{\rho}(f)=-\langle f,Lf\rangle_{\nu_{\rho}} satisfies (8.5.1) for bounded ff\in{\mathcal{L}}. Hint: Show f(η)Lf(η)f(\eta)Lf(\eta) is absolutely summable and integrable with respect to νρ\nu_{\rho}. Then, by Fubini’s theorem, one can interchange the expectation and sum. Noting Eνρ[g(η(x))f(ηx,y)f(η)]=Eνρ[g(η(y))f(η)f(ηy,x)]E_{\nu_{\rho}}\big[g(\eta(x))f(\eta^{x,y})f(\eta)\big]=E_{\nu_{\rho}}\big[g(\eta(y))f(\eta)f(\eta^{y,x})\big], one may reorganize the sum. See also Lemma 2.4 in [194].

8.6. Notes

In these notes, we have followed [5] for the invariance of νρ\nu_{\rho} and [194] for the extension to L2L^{2} (see also Section IV.4 in [147]) and extremality of νρ\nu_{\rho}; see these papers for extensions to non translation-invariant transition probabilities. See also [181][Section 2] for more on the connections between extremality, harmonicity, and ergodicity.

A natural question is what are all the extremals of the process. In [5], it is shown in d=1,2d=1,2 when gg is an increasing function that {ν¯Ψ:Ψ<lim infg(k)}\{\bar{\nu}_{\Psi}:\Psi<\liminf g(k)\} are all the extremals! When pp is not translation-invariant, also in d=1,2d=1,2 when gg is increasing, all the extremals are found–in this case, the invariant measures are not necessarily translation-invariant [5]. When pp is positive-recurrent, the extremals concentrate on configurations with a finite number of particles [215], [5].

For simple exclusion on d\mathbb{Z}^{d}, since local functions, those depending on a finite number of variables {η(x):xd}\{\eta(x):x\in\mathbb{Z}^{d}\}, form a core, one may verify that the Bernoulli product measures νρ=xdBern(ρ)\nu_{\rho}=\prod_{x\in\mathbb{Z}^{d}}{\rm Bern}(\rho) for ρ[0,1]\rho\in[0,1] are invariant for the infinite volume process (as compared to the finite-volume one in Proposition 2.2.1); see Chapter VIII in [147]. One may also use the arguments given here for the zero-range process. Extremality of νρ\nu_{\rho} can also be seen from the arguments for Theorem 8.4.1.

However, for zero-range and exclusion models, there remain many open problems! In particular, determining all the extremal invariant measures in all model settings is still not fully resolved. See [147], [194], as well as [3], [16], [48], [31], [32], [91], [126], [152] for more references, and discussion.

Section 9 Additive functionals and central limit theorems

The occupation time of a set, for instance, is an additive functional of a process. One would like to know the first order and second order behaviors, namely the LLN and CLT for these objects. This is an old subject, and in stochastic particle systems where the configuration space is difficult, with interesting scalings and limits.

We focus here mostly on symmetric exclusion processes on d\mathbb{Z}^{d}, when starting from an invariant measure. After a general introduction, we discuss ergodic and fluctuation behaviors, when starting under an invariant measure. The Kipnis-Varadhan CLT, which has wide application, not only to particle systems, is stated and proved. Comments on the behaviors in asymmetric simple exclusion are also made.

9.1. Basic problem and ergodic theory

Consider a Markov process η(t)\eta(t) on a state space Ω\Omega. Let μ\mu be an invariant measure for the process. Let f:Ωf:\Omega\rightarrow\mathbb{R} be an L2(μ)L^{2}(\mu) function. Recall that EμE_{\mu} stands for the expectation under μ\mu, and μ\mathbb{P}_{\mu} and 𝔼μ\mathbb{E}_{\mu} for the process measure and expectation when starting in μ\mu.

The basic problem is to determine the behavior as tt\rightarrow\infty of

Af(t)=0tf(ηs)𝑑s.A_{f}(t)\ =\ \int_{0}^{t}f(\eta_{s})ds.

In the following, we call Af(t)A_{f}(t) an ‘additive functional’ since Af(t+s)Af(s)A_{f}(t+s)-A_{f}(s) under μ\mu has the same distribution as Af(t)A_{f}(t) under μ\mu.

If μ\mu is extremal, then, as we have seen in Proposition 8.3.5, the process started from initial distribution μ\mu is ergodic with respect to time shifts, and hence (by Birkhoff’s theorem)

limt1t0tf(ηs)𝑑s=Eμ[f]μa.s.\lim_{t\uparrow\infty}\frac{1}{t}\int_{0}^{t}f(\eta_{s})ds\ =\ E_{\mu}[f]\ \ \mu-{\rm a.s.}

This covers the case when μ\mu is unique, for instance, in positive-recurrent Markov chains. When μ\mu is null-recurrent, different behaviors may emerge (see [168]).

The next order question is to ask about the fluctuations: Find the limits of

1t0t(f(ηs)Eμ[f])𝑑s.\frac{1}{\sqrt{t}}\int_{0}^{t}\big(f(\eta_{s})-E_{\mu}[f]\big)ds.

One expects a Gaussian limit, with sufficient mixing. In the following, we will assume μ\mu is extremal and that ff is already centered, that is Eμ[f]=0E_{\mu}[f]=0 to simplify expressions.

Consider the example of finite-state irreducible Markov chains. We may view μ=μ(x):xΩ\mu=\langle\mu(x):x\in\Omega\rangle and f=f(x):xΩf=\langle f(x):x\in\Omega\rangle as elements of |Ω|\mathbb{R}^{|\Omega|}. Note that (μL)(x)=0(\mu L)(x)=0 for all xΩx\in\Omega where LL is the generator of the process. Since μ\mu is the unique invariant measure, Null(LT)={cμ:c}{\rm Null}(L^{T})=\{c\mu:c\in\mathbb{R}\}. The orthogonal complement of this null space is Range(L){\rm Range}(L): For ϕRange(L)\phi\in{\rm Range}(L), we have ϕ=Lu\phi=Lu. Then, xμ(x)(Lu)(x)=0\sum_{x}\mu(x)(Lu)(x)=0 as μ\mu is invariant.

As a consequence, given Eμ[f]=xf(x)μ(x)=0E_{\mu}[f]=\sum_{x}f(x)\mu(x)=0, we have fμf\perp\mu and hence ff belongs to the range Range(L){\rm Range}(L), and f=Luf=-Lu for some function uu. That is, ff solves a ‘Poisson’ equation with respect to the generator.

We may now write

tt0tf(ηs)𝑑s=1tM(t)+1t(u(η(0))u(η(t)))\frac{t}{\sqrt{t}}\int_{0}^{t}f(\eta_{s})ds\ =\ \frac{1}{\sqrt{t}}M(t)+\frac{1}{\sqrt{t}}\big(u(\eta(0))-u(\eta(t))\big) (9.1.1)

where

M(t)=u(η(t))u(η(0))0tLu(ηs)𝑑sM(t)\ =\ u(\eta(t))-u(\eta(0))-\int_{0}^{t}Lu(\eta_{s})ds

is a martingale with respect to natural sigma-fields. The quadratic variation, as we have observed in Subsection 2.3, equals

M(t)=0t(Lu22uLu)(ηs)𝑑s\langle M\rangle(t)\ =\ \int_{0}^{t}(Lu^{2}-2uLu)(\eta_{s})ds

whose mean is

𝔼μ[M(t)]=t𝔼μ[M2(1)]= 2tEμ[u(Lu)]=: 2tD(u)\mathbb{E}_{\mu}\big[\langle M\rangle(t)\big]\ =\ t\mathbb{E}_{\mu}\big[M^{2}(1)\big]\ =\ 2tE_{\mu}[u(-Lu)]\ =:\ 2tD(u)

where D(u)D(u) is the Dirichlet form.

The second term in (9.1.1) is of order t1/2t^{-1/2} since uu is a function on finite state space, and hence bounded. The first term, however, can be treated with a martingale central limit theorem.

Proposition 9.1.1.

Let (t,t)(\mathcal{M}_{t},\mathcal{F}_{t}) be a mean-zero martingale with stationary, ergodic increments such that 𝔼[12]=σ2\mathbb{E}\big[\mathcal{M}^{2}_{1}\big]=\sigma^{2}. Then,

1ttN(0,σ2).\frac{1}{\sqrt{t}}\mathcal{M}_{t}\ \Rightarrow\ {\rm N}(0,\sigma^{2}).
Exercise 9.1.2.

This theorem can be found in discrete time in many places (cf. [108][Theorem 2.5 (b)], [192][Theorem 3]). From the discrete time version, prove the proposition above, by considering the discrete time martingale MtM_{\lfloor t\rfloor}.

To complete the argument, note the martingale M(t)M(t) has stationary and ergodic increments when the process is started from μ\mu. Hence, by Proposition 9.1.1, we conclude

1t0tf(ηs)𝑑sN(0,2D(u)).\frac{1}{\sqrt{t}}\int_{0}^{t}f(\eta_{s})ds\ \Rightarrow\ {\rm N}(0,2D(u)).

9.2. Occupation functionals in exclusion systems

Consider the dd-dimensional exclusion process ηt\eta_{t} with semigroup PtP_{t} and generator LL,

Lf(η)=x,ydη(x)(1η(y))p(x,y)[f(ηx,y)f(η)],Lf(\eta)=\sum_{x,y\in\mathbb{Z}^{d}}\eta(x)\big(1-\eta(y)\big)p(x,y)\big[f(\eta^{x,y})-f(\eta)\big],

lifting the finite-volume definition in Section 2. Such an infinite-volume system on Ω={0,1}d\Omega=\{0,1\}^{\mathbb{Z}^{d}} may be well constructed; see the Notes in Section 7. In the following, we will assume the jump probability pp is finite-range and translation-invariant.

Let νρ=xdBern(ρ)\nu_{\rho}=\prod_{x\in\mathbb{Z}^{d}}{\rm Bern}(\rho) be the Bernoulli product measure with marginal success probability ρ[0,1]\rho\in[0,1] on Ω\Omega. These measures can be shown invariant and extremal for the process, and when pp is symmetric they are also reversible; see the Notes in Section 8. Compare also with the finite-volume discussion in Section 2. In the following, we will work with the L2(νρ)L^{2}(\nu_{\rho})-exclusion processes.

Consider now the ‘additive functional’ question for occupation functions f(η)=η(0)ρf(\eta)=\eta(0)-\rho. Given νρ\nu_{\rho} is extremal and therefore ergodic with respect to time shifts (cf. Proposition 8.3.5), we see that the LLN behavior starting under νρ\nu_{\rho} is clear: For fL2(νρ)f\in L^{2}(\nu_{\rho}),

limt1t0tf(ηs)𝑑s=Eνρ[f]\lim_{t\uparrow\infty}\frac{1}{t}\int_{0}^{t}f(\eta_{s})ds\ =\ E_{\nu_{\rho}}[f]

both in L2(νρ)L^{2}(\nu_{\rho}) and νρ\nu_{\rho}-a.s. by Proposition 8.3.4 and Birkhoff’s ergodic theorem.

However, the fluctuation behavior of A(t)A(t), with respect to f(η)=η(0)ρf(\eta)=\eta(0)-\rho is different depending on the dimension dd, the symmetry/asymmetry of the jump probability pp, and the density ρ\rho. A more or less complete theory is known, except for some interesting asymmetric cases in d2d\leq 2 which connect with ‘KPZ’ class phenomenon, and ‘mean-zero asymmetric’ cases.

We first consider the types of variances that might be obtained. What is the variance of Af(t)A_{f}(t), what are its limits, and how does the limit depend on ff? For a general local function ff, that is one that depends only on a finite number of variables {η(x):xd}\{\eta(x):x\in\mathbb{Z}^{d}\}, let us try to get a formula for Var(Af(t)){\rm Var}(A_{f}(t)). Write, using stationarity, that

Var(Af(t))\displaystyle{\rm Var}(A_{f}(t)) =\displaystyle= 𝔼νρ[(0tf(ηs)𝑑s)2]\displaystyle\mathbb{E}_{\nu_{\rho}}\Big[\Big(\int_{0}^{t}f(\eta_{s})ds\Big)^{2}\Big]
=\displaystyle= 20t(ts)𝔼νρ[f(ηs)f(η0)]𝑑s.\displaystyle 2\int_{0}^{t}(t-s)\mathbb{E}_{\nu_{\rho}}[f(\eta_{s})f(\eta_{0})]ds.

By reversibility of νρ\nu_{\rho}, the semigroup PsP_{s} is self-adjoint, and we may express

𝔼νρ[f(ηs)f(η0)]\displaystyle\mathbb{E}_{\nu_{\rho}}[f(\eta_{s})f(\eta_{0})] =\displaystyle= Psf,fνρ\displaystyle\langle P_{s}f,f\rangle_{\nu_{\rho}}
=\displaystyle= Ps/2f,Ps/2fνρ=Ps/2fL2(νρCLOSE2 0.\displaystyle\langle P_{s/2}f,P_{s/2}f\rangle_{\nu_{\rho}}\ =\ \|P_{s/2}f\|_{L^{2}(\nu_{\rho}}^{2}\ \geq\ 0.

Recall, f,gμ:=Eμ[fg]\langle f,g\rangle_{\mu}:=E_{\mu}[fg].

Then, when the variance is scaled by tt, its limit exists, possibly infinite, and is in form

σ2(f)\displaystyle\sigma^{2}(f) =\displaystyle= limt1tVar(Af(t))\displaystyle\lim_{t\uparrow\infty}\frac{1}{t}{\rm Var}(A_{f}(t))
=\displaystyle= limt20t[1st]𝔼νρ[f(ηs)f(η0)]𝑑s\displaystyle\lim_{t\uparrow\infty}2\int_{0}^{t}\Big[1-\frac{s}{t}\Big]\mathbb{E}_{\nu_{\rho}}[f(\eta_{s})f(\eta_{0})]ds
=\displaystyle= 20𝔼νρ[f(ηs)f(η0)]𝑑s.\displaystyle 2\int_{0}^{\infty}\mathbb{E}_{\nu_{\rho}}[f(\eta_{s})f(\eta_{0})]ds.

The last equality follows from monotone convergence. This formula is the familiar ‘sum of correlations’ expression with respect to sums of correlated random variables.

9.2.1. Symmetric pp and duality relations

In symmetric exclusion, any mean-zero, local function can be written as

f(η)\displaystyle f(\eta) =\displaystyle= Bf^(B)xBη(x)ρρ(1ρ)\displaystyle\sum_{B}\hat{f}(B)\prod_{x\in B}\frac{\eta(x)-\rho}{\sqrt{\rho(1-\rho)}}
=\displaystyle= n1|B|=nf^(B)xBη(x)ρρ(1ρ).\displaystyle\sum_{n\geq 1}\sum_{|B|=n}\hat{f}(B)\prod_{x\in B}\frac{\eta(x)-\rho}{\sqrt{\rho(1-\rho)}}.

Here, the decomposition is over ‘degrees’, that is, functions which are the product of nn centered, normalized occupation variables.

This basis is quite central to symmetric exclusion because of the ‘duality’ relation. Namely, for a function

fB(η)=xBη(x)ρρ(1ρ)f_{B}(\eta)\ =\ \prod_{x\in B}\frac{\eta(x)-\rho}{\sqrt{\rho(1-\rho)}}

where |B|=n|B|=n, we have

(PtfB)(η)=|U|=npt(B,U)xUη(x)ρρ(1ρ)(P_{t}f_{B})(\eta)\ =\ \sum_{|U|=n}p_{t}(B,U)\prod_{x\in U}\frac{\eta(x)-\rho}{\sqrt{\rho(1-\rho)}}

where pt(B,U)p_{t}(B,U) is the transition probability of nn-particle simple exclusion from a configuration BB to configuration UU in time tt.

One way to prove this relation is to observe that

LfB(η)=|U|=nq(B,U)fU(η)Lf_{B}(\eta)\ =\ \sum_{|U|=n}q(B,U)f_{U}(\eta)

where q(B,U)q(B,U) is the transition rate of nn-particle symmetric exclusion; see Exercise 2.2.2.

At this point, we can use the duality relation, and independence of coordinates under νρ\nu_{\rho}, to evaluate the term

Eνρ[(Psf(η0)f(η0)]\displaystyle E_{\nu_{\rho}}[(P_{s}f(\eta_{0})f(\eta_{0})] =\displaystyle= Eνρ[Bf^(B)Upt(B,U)fU(η0)f(η0)]\displaystyle E_{\nu_{\rho}}\Big[\sum_{B}\hat{f}(B)\sum_{U}p_{t}(B,U)f_{U}(\eta_{0})\cdot f(\eta_{0})\Big]
=\displaystyle= BUf^(B)f^(U)pt(B,U)\displaystyle\sum_{B}\sum_{U}\hat{f}(B)\hat{f}(U)p_{t}(B,U)
=\displaystyle= n1|B|,|U|=nf^(B)f^(U)pt(B,U).\displaystyle\sum_{n\geq 1}\sum_{|B|,|U|=n}\hat{f}(B)\hat{f}(U)p_{t}(B,U).

Now, when f(η)=η(0)ρf(\eta)=\eta(0)-\rho is the centered occupation function, f^(B)=0\hat{f}(B)=0 for all B{0}B\neq\{0\}, and f^({0})=ρ(1ρ)\hat{f}(\{0\})=\sqrt{\rho(1-\rho)}. Then, the variance is calculated as

Var(Af(t))= 2ρ(1ρ)0t(ts)ps(0,0)𝑑s{\rm Var}(A_{f}(t))\ =\ 2\rho(1-\rho)\int_{0}^{t}(t-s)p_{s}(0,0)ds

where pt(0,0)p_{t}(0,0) is the return probability of a random walk according to jump probabilities pp!

From local limit theorems, when the transition probability is simple, p(ei)=p(ei)=1/(2d)p(e_{i})=p(-e_{i})=1/(2d) for the standard basis {ei}i=1d\{e_{i}\}_{i=1}^{d}, we have the following asymptotics.

Proposition 9.2.1.

For f(η)=η(0)ρf(\eta)=\eta(0)-\rho, under symmetric simple exclusion processes,

Var(Af(t))={8ρ(1ρ)32πt3/2+o(t3/2)ind=12ρ(1ρ)πtlogt+o(tlogt)ind=22ρ(1ρ)0pt(0,0)𝑑tind3.{\rm Var}(A_{f}(t))\ =\ \left\{\begin{array}[]{rl}\frac{8\rho(1-\rho)}{3\sqrt{2\pi}}t^{3/2}+o(t^{3/2})&\ {\rm in\ }d=1\\ \frac{2\rho(1-\rho)}{\pi}t\log t+o(t\log t)&\ {\rm in\ }d=2\\ 2\rho(1-\rho)\int_{0}^{\infty}p_{t}(0,0)dt&\ {\rm in\ }d\geq 3.\end{array}\right.

9.2.2. Asymmetric pp

By asymmetric, we mean that xxp(x)0\sum_{x}xp(x)\neq 0. The case that pp is not symmetric but xxp(x)=0\sum_{x}xp(x)=0, the ‘mean-zero’ asymmetric situation is not considered here; see the Notes for citations.

As in symmetric exclusion, one can understand the general asymptotics by calculating the term 𝔼νρ[f(ηs)f(η0)]\mathbb{E}_{\nu_{\rho}}[f(\eta_{s})f(\eta_{0})]. However, the ‘duality relation’ is no longer valid in the form given, since the generator does not preserve the ‘degree’ of a function, that is LL applied to a function of nn coordinates is no longer a linear combination of nn coordinate functions.

However, for f(η)=η(0)ρf(\eta)=\eta(0)-\rho, write

𝔼νρ[f(ηs)f(η0)]\displaystyle\mathbb{E}_{\nu_{\rho}}[f(\eta_{s})f(\eta_{0})] =\displaystyle= 𝔼νρ[ηs(0)η0(0)]ρ2\displaystyle\mathbb{E}_{\nu_{\rho}}[\eta_{s}(0)\eta_{0}(0)]-\rho^{2}
=\displaystyle= ρ{𝔼νρ[ηs(0)|η0(0)=1]𝔼νρ[ηs(0)]}\displaystyle\rho\big\{\mathbb{E}_{\nu_{\rho}}[\eta_{s}(0)|\eta_{0}(0)=1]-\mathbb{E}_{\nu_{\rho}}[\eta_{s}(0)]\big\}
=\displaystyle= ρ(1ρ){𝔼νρ[ηs(0)|η0(0)=1]𝔼νρ[ηs(0)|η0(0)=0]}.\displaystyle\rho(1-\rho)\big\{\mathbb{E}_{\nu_{\rho}}[\eta_{s}(0)|\eta_{0}(0)=1]-\mathbb{E}_{\nu_{\rho}}[\eta_{s}(0)|\eta_{0}(0)=0]\big\}.

The basic coupling, with respect to exclusion, couples two copies of the exclusion process starting from configurations ηη\eta^{\prime}\geq\eta^{\prime} where η(x)=η(x)\eta^{\prime}(x)=\eta^{\prime}(x) for x0x\neq 0 and η(0)=1\eta^{\prime}(0)=1, η(0)=0\eta^{\prime}(0)=0. Then, (ηt,ηt)(\eta^{\prime}_{t},\eta^{\prime}_{t}) has generator

L¯(η,η)\displaystyle\bar{L}(\eta^{\prime},\eta^{\prime}) =\displaystyle= x,yp(yx)1(η(x)=η(x)=1)[f((η)x,y,(η)x,y)f]\displaystyle\sum_{x,y}p(y-x)1(\eta^{\prime}(x)=\eta^{\prime}(x)=1)\big[f((\eta^{\prime})^{x,y},(\eta^{\prime})^{x,y})-f\big]
+x,yp(yx)1(η(x)=1,η(x)=0)[f((η)x,y,η)f].\displaystyle+\sum_{x,y}p(y-x)1(\eta^{\prime}(x)=1,\eta^{\prime}(x)=0)\big[f((\eta^{\prime})^{x,y},\eta^{\prime})-f\big].

The ηt\eta^{\prime}_{t} process always majorizes ηt\eta^{\prime}_{t}, with exactly one discrepancy, whose position we label RtR_{t}.

The dynamics of RtR_{t} is as follows: Infinitesimally, it displaces by zz with rate p(z)(1η(Rt+z))+p(z)η(Rt+z)p(z)(1-\eta(R_{t}+z))+p(-z)\eta(R_{t}+z). The term p(z)(1η(Rt+z))p(z)(1-\eta(R_{t}+z)) corresponds to the discrepancy, or ‘second-class’ particle as it is sometimes known, moving by its own intention, and the term p(z)η(Rt+z)p(-z)\eta(R_{t}+z) refers to when a particle at Rt+zR_{t}+z would move to location RtR_{t} in which case by the basic coupling, RtR_{t} accedes and takes the place Rt+zR_{t}+z.

Then, we have that

𝔼νρ[f(ηs)f(η0)]=ρ(1ρ)P¯(Rt=0) 0.\mathbb{E}_{\nu_{\rho}}[f(\eta_{s})f(\eta_{0})]\ =\ \rho(1-\rho)\bar{P}(R_{t}=0)\ \geq\ 0.

Hence, by monotone convergence the limit exists,

σf2= 2ρ(1ρ)0P¯(Rt=0)𝑑t.\sigma^{2}_{f}\ =\ 2\rho(1-\rho)\int_{0}^{\infty}\bar{P}(R_{t}=0)dt.

In mean value, substituting ρ\rho for η(Rt+z)\eta(R_{t}+z), we see that a ‘mean’ infinitesimal drift is

z[p(z)(1ρ)+p(z)ρ]=(12ρ)zp(z).\sum z[p(z)(1-\rho)+p(-z)\rho]\ =\ (1-2\rho)\sum zp(z).

This leads to the conjecture that

σf2<ρ1/2\sigma^{2}_{f}<\infty\ \Leftrightarrow\ \rho\neq 1/2

which has been proved; see the Notes.

Proposition 9.2.2.

For f(η)=η(0)ρf(\eta)=\eta(0)-\rho, with respect to asymmetric exclusion with drift zp(z)0\sum zp(z)\neq 0, we have

Var(Af(t))=σf2t+o(t){\rm Var}(A_{f}(t))\ =\ \sigma^{2}_{f}t+o(t)

when ρ1/2\rho\neq 1/2 or when d3d\geq 3.

However, when ρ=1/2\rho=1/2, we have Var(Af(t))C1t5/4{\rm Var}(A_{f}(t))\geq C_{1}t^{5/4}. In d=2d=2, we have Var(Af(t))C2tloglogt{\rm Var}(A_{f}(t))\geq C_{2}t\log\log t.

Remark 9.2.3.

We remark the orders expected when ρ1/2\rho\neq 1/2 in d=1,2d=1,2 are t4/3t^{4/3} and t(logt)2/3t(\log t)^{2/3} respectively. These orders connect with certain KPZ class phenomena, and are open to verify. See the Notes for more discussion.

9.3. Central limit theorems and H1H_{-1} norms

Our goal now is to prove asymptotic normality of t1/2Af(t)t^{-1/2}A_{f}(t) when σf2<\sigma^{2}_{f}<\infty. Except for the two open cases in Proposition 9.2.2, a central limit theorem also holds when Af(t)A_{f}(t) is normalized by the square root of its variance, although we do not discuss these results here; see the following Notes.

We focus on the symmetric case where the Kipnis-Varadhan CLT applies. The Kipnis-Varadhan theorem is a CLT for additive functionals of a Markov process, reversible and ergodic, on general state space Ω\Omega.

Theorem 9.3.1.

Consider an L2(μ)L^{2}(\mu) Markov process ηt\eta_{t} begun with ergodic, reversible invariant measure μ\mu. Let f:Ωf:\Omega\rightarrow\mathbb{R} be an L2(μ)L^{2}(\mu) function such that σf2<\sigma^{2}_{f}<\infty. Then,

1t0tf(ηs)𝑑sN(0,σf2).\frac{1}{\sqrt{t}}\int_{0}^{t}f(\eta_{s})ds\ \Rightarrow\ {\rm N}(0,\sigma^{2}_{f}).

A functional CLT/invariance principle can also be proved under the assumption of the theorem, but we do not discuss this extension here.

The main tool to prove Theorem 9.3.1 is to approximate t1/2Af(t)t^{-1/2}A_{f}(t) by a martingale, and then to use Proposition 9.1.1. The idea is to try to write f=Luf=-Lu. However, this is not possible in general. If it were possible, one could use the results in [26]. A resolvent type equation always holds however, that can be worked with. The following, which can be proved by this approach, is sufficient for the martingale approximation.

Proposition 9.3.2.

Under the assumptions of Theorem 9.3.1, there is a martingale M(t)M(t) with stationary and ergodic increments such that

1tAf(t)=1tM(t)+1tζ(t)\frac{1}{\sqrt{t}}A_{f}(t)\ =\ \frac{1}{\sqrt{t}}M(t)+\frac{1}{\sqrt{t}}\zeta(t)

where

limt1t𝔼μ[ζ2(t)]= 0and𝔼μ[M2(t)]=tσf2.\lim_{t\uparrow\infty}\frac{1}{t}\mathbb{E}_{\mu}[\zeta^{2}(t)]\ =\ 0\ \ \ {\rm and\ \ \ }\mathbb{E}_{\mu}\big[M^{2}(t)\big]=t\sigma^{2}_{f}.

9.3.1. 1{\mathcal{H}}_{1} and 1{\mathcal{H}}_{-1} norms

Before proving Proposition 9.3.2, some definitions will be useful. The generator LL of exclusion is well defined on the core of local functions. Define, for local functions ϕ\phi and λ0\lambda\geq 0, the semi-norm ϕ1,λ\|\phi\|_{1,\lambda} by

ϕ1,λ2=ϕ,(λL)ϕμ=D(ϕ)+λϕL2(μ)2.\|\phi\|_{1,\lambda}^{2}\ =\ \langle\phi,(\lambda-L)\phi\rangle_{\mu}\ =\ D(\phi)+\lambda\|\phi\|^{2}_{L^{2}(\mu)}.

Note that, since L-L is a nonnegative self-adjoint operator,

ϕ,(λL)ψμ=(λL)1/2ϕ,(λL)1/2ψμϕ1,λψ1,λ.\langle\phi,(\lambda-L)\psi\rangle_{\mu}\ =\langle(\lambda-L)^{1/2}\phi,(\lambda-L)^{1/2}\psi\rangle_{\mu}\ \leq\ \|\phi\|_{1,\lambda}\|\psi\|_{1,\lambda}.

After modding out by functions with ϕ1,λ=0\|\phi\|_{1,\lambda}=0, define the space 1,λ\mathcal{H}_{1,\lambda} as the completion with respect to 1,λ\|\cdot\|_{1,\lambda}.

Now, we define for a local function ϕ\phi that

ϕ1,λ=sup{ϕ,ψμψ1,λ:ψlocal}.\|\phi\|_{-1,\lambda}\ =\ \sup\left\{\frac{\langle\phi,\psi\rangle_{\mu}}{\|\psi\|_{1,\lambda}}:\psi\ {\rm local}\right\}.

Again, after modding out by functions ϕ1,λ=0\|\phi\|_{-1,\lambda}=0, define 1,λ\mathcal{H}_{-1,\lambda} as the completion with respect to 1,λ\|\cdot\|_{-1,\lambda}. When λ>0\lambda>0, (λL)1(\lambda-L)^{-1} is a bounded operator (bounded by λ1\lambda^{-1} from resolvent formulas–see the next subsection), and

ϕ1,λ2=ϕ,(λL)1ϕμ.\|\phi\|_{-1,\lambda}^{2}\ =\ \langle\phi,(\lambda-L)^{-1}\phi\rangle_{\mu}.

Both spaces 1,λ\mathcal{H}_{1,\lambda}, 1,λ\mathcal{H}_{-1,\lambda} are Hilbert spaces where innerproducts are given by polarization:

ϕ,ψ=14{ϕ+ψϕψ}.\langle\langle\phi,\psi\rangle\rangle\ =\ \frac{1}{4}\left\{\|\phi+\psi\|-\|\phi-\psi\|\right\}.

These two norms are dual to each other: For local functions,

ϕ,ψμϕ1,λψ1,λ.\langle\phi,\psi\rangle_{\mu}\ \leq\ \|\phi\|_{-1,\lambda}\|\psi\|_{1,\lambda}.

When λ=0\lambda=0, 1:=1,0\|\cdot\|_{1}:=\|\cdot\|_{1,0} and 1:=1,0\|\cdot\|_{-1}:=\|\cdot\|_{-1,0} are called the 1\mathcal{H}_{1} and 1\mathcal{H}_{-1} norms respectively. Note that ϕ12=D(ϕ)\|\phi\|_{1}^{2}=D(\phi).

We note there is another formula for ϕ1,λ\|\phi\|_{-1,\lambda} of note:

ϕ1,λ2\displaystyle\|\phi\|_{-1,\lambda}^{2} =sup{2ϕ,ψμψ1,λ2:ψlocal}.\displaystyle=\sup\left\{2\langle\phi,\psi\rangle_{\mu}-\|\psi\|^{2}_{1,\lambda}:\psi\ {\rm local}\right\}. (9.3.1)

We remark, when LL is not self-adjoint, there are useful notions of 1,λ{\mathcal{H}}_{1,\lambda} and 1,λ{\mathcal{H}}_{-1,\lambda} spaces; see [18][Lemma 2.1], [133] for instance.

Exercise 9.3.3.

Verify formula (9.3.1) from the definitions.

Also, show ϕ1,λϕ1\|\phi\|_{-1,\lambda}\uparrow\|\phi\|_{-1} and ϕ1,λϕ1\|\phi\|_{1,\lambda}\downarrow\|\phi\|_{1} as λ0\lambda\downarrow 0.

Sometimes the 1\mathcal{H}_{-1} norm is referred to as the ‘variance’ norm. Since ϕ1,λ\|\phi\|_{-1,\lambda} is increasing as λ0\lambda\downarrow 0, and limλ0ϕ1,λ=ϕ1\lim_{\lambda\downarrow 0}\|\phi\|_{-1,\lambda}=\|\phi\|_{-1}, we have

2ϕ12\displaystyle 2\|\phi\|_{-1}^{2} =\displaystyle= 2limλ0ϕ1,λ2\displaystyle 2\lim_{\lambda\downarrow 0}\|\phi\|_{-1,\lambda}^{2}
=\displaystyle= 2limλ0ϕ,(λL)1ϕμ\displaystyle 2\lim_{\lambda\downarrow 0}\langle\phi,(\lambda-L)^{-1}\phi\rangle_{\mu}
=\displaystyle= 2limλ00eλtEμ[ϕ(Ptϕ)]𝑑t\displaystyle 2\lim_{\lambda\downarrow 0}\int_{0}^{\infty}e^{-\lambda t}E_{\mu}[\phi(P_{t}\phi)]dt
=\displaystyle= 20𝔼μ[ϕ(ηt)ϕ(η0)]𝑑t=σϕ2.\displaystyle 2\int_{0}^{\infty}\mathbb{E}_{\mu}[\phi(\eta_{t})\phi(\eta_{0})]dt\ =\ \sigma^{2}_{\phi}.

The last evaluation of the limit follows as Eμ[ϕ(Ptϕ)]=𝔼μ[ϕ(ηt)ϕ(η0)]E_{\mu}[\phi(P_{t}\phi)]=\mathbb{E}_{\mu}[\phi(\eta_{t})\phi(\eta_{0})] is nonnegative since PtP_{t} is self-adjoint.

In particular, we observe the following.

Lemma 9.3.4.

We have σf2=2f12\sigma^{2}_{f}=2\|f\|^{2}_{-1} and so

theconditionσf2<f12<.{\rm the\ condition\ }\sigma^{2}_{f}<\infty\Leftrightarrow\|f\|^{2}_{-1}<\infty.

9.3.2. Step 1: Resolvent calculations

To facilitate the proof of Proposition 9.3.2, consider the resolvent equation

λuλLuλ=f\lambda u_{\lambda}-Lu_{\lambda}\ =\ f (9.3.2)

where

uλ(η)=(λL)1f=0eλtPtf(η)𝑑t.u_{\lambda}(\eta)\ =\ (\lambda-L)^{-1}f\ =\ \int_{0}^{\infty}e^{-\lambda t}P_{t}f(\eta)dt.
Exercise 9.3.5.

Show that Eνρ[uλ2]λ1Eνρ[f2]E_{\nu^{\prime}_{\rho}}[u^{2}_{\lambda}]\leq\lambda^{-1}E_{\nu^{\prime}_{\rho}}[f^{2}]. This bound is part of the standard theory of ‘resolvents’.

Let us multiply the resolvent equation by uλu_{\lambda} and take expectation:

λuλL2(μ)+D(uλ)=f,uλμ.\lambda\|u_{\lambda}\|_{L^{2}(\mu)}+D(u_{\lambda})\ =\ \langle f,u_{\lambda}\rangle_{\mu}.

Then,

λuλL2(μ)+uλ12f1uλ1\lambda\|u_{\lambda}\|_{L^{2}(\mu)}+\|u_{\lambda}\|_{1}^{2}\ \leq\ \|f\|_{-1}\|u_{\lambda}\|_{1}

which gives immediately that

uλ1f1andλuλL2(μ)2f12\|u_{\lambda}\|_{1}\ \leq\ \|f\|_{-1}\ \ {\rm and\ \ }\lambda\|u_{\lambda}\|^{2}_{L^{2}(\mu)}\ \leq\ \|f\|_{-1}^{2}

uniformly in λ>0\lambda>0.

Also, since |Lϕ,ψμ|ϕ1ψ1|\langle L\phi,\psi\rangle_{\mu}|\leq\|\phi\|_{1}\|\psi\|_{1}, we observe L:11L:\mathcal{H}_{1}\rightarrow\mathcal{H}_{-1} is a bounded operator, with bound 11. Hence, for all λ>0\lambda>0,

Luλ1uλ1f1.\|Lu_{\lambda}\|_{-1}\ \leq\ \|u_{\lambda}\|_{1}\ \leq\ \|f\|_{-1}.

Now, by the uniform boundedness principle, one can find a subsequence which converges weakly to an element w1w\in\mathcal{H}_{1}:

uλnw.u_{\lambda_{n}}\ \rightarrow\ w.

For ϕ\phi local, and as local functions are dense in H1H_{1}, we have

λuλ,ϕμλf1ϕL2,\lambda\langle u_{\lambda},\phi\rangle_{\mu}\ \leq\ \sqrt{\lambda}\|f\|_{-1}\|\phi\|_{L^{2}},

and since λuλ12f1\|\lambda u_{\lambda}\|_{-1}\leq 2\|f\|_{-1}, we conclude λuλ0\lambda u_{\lambda}\rightarrow 0 weakly in 1\mathcal{H}_{-1}. Therefore,

Luλnfweaklyin1.-Lu_{\lambda_{n}}\ \rightarrow\ f\ \ {\rm weakly\ in\ }\mathcal{H}_{-1}. (9.3.3)

9.3.3. Step 2: Strong approximations

At this point, we would like to claim that

f,uλf,w,uλ,Luλ=uλ12w12,andλuλL220\langle f,u_{\lambda}\rangle\rightarrow\langle f,w\rangle,\ \langle u_{\lambda},-Lu_{\lambda}\rangle=\|u_{\lambda}\|^{2}_{1}\rightarrow\|w\|^{2}_{1},\ {\rm and\ }\lambda\|u_{\lambda}\|^{2}_{L^{2}}\rightarrow 0

so that f,w=w11\langle f,w\rangle=\|w\|^{1}_{1} and ff satisfies a ‘weak’ Poisson equation. However, the weak convergence shown, as there are limits in λ\lambda in both components of uλ,Luλ\langle u_{\lambda},-Lu\lambda\rangle, is not strong enough to conclude this relation immediately.

Nevertheless, we will show that the convergences can be strengthened as follows.

Proposition 9.3.6.

We have

  • (i)

    limλ0λuλL2(μ)2= 0\lim_{\lambda\downarrow 0}\lambda\|u_{\lambda}\|^{2}_{L^{2}(\mu)}\ =\ 0.

  • (ii)

    There is a w1w\in\mathcal{H}_{1} such that uλwu_{\lambda}\rightarrow w strongly in 1\mathcal{H}_{1}.

    Also w12=w,fμ\|w\|_{1}^{2}=\langle w,f\rangle_{\mu}.

Proof of Proposition 9.3.2.

Given (i) and (ii) above, to be shown later, we now finish the proof of the Proposition 9.3.2. Write

Af(t)\displaystyle A_{f}(t) =\displaystyle= Mλ(t)+λ0tuλ(ηs)𝑑s+uλ(η0)uλ(ηs)\displaystyle M_{\lambda}(t)+\lambda\int_{0}^{t}u_{\lambda}(\eta_{s})ds+u_{\lambda}(\eta_{0})-u_{\lambda}(\eta_{s})
=:\displaystyle=: Mλ(t)+ζλ(t)\displaystyle M_{\lambda}(t)+\zeta_{\lambda}(t)

where

Mλ(t)=uλ(ηt)uλ(η0)0tLuλ(ηs)𝑑sM_{\lambda}(t)\ =\ u_{\lambda}(\eta_{t})-u_{\lambda}(\eta_{0})-\int_{0}^{t}Lu_{\lambda}(\eta_{s})ds

is a martingale and ζλ(t)\zeta_{\lambda}(t) is the remainder.

We claim now 𝔼μ[Mλ2(t)]=2tuλ12\mathbb{E}_{\mu}\big[M^{2}_{\lambda}(t)\big]=2t\|u_{\lambda}\|_{1}^{2}. Indeed, we need only evaluate

limt0t1𝔼μ[Mλ2(t)]=2uλ12.\displaystyle\lim_{t\downarrow 0}t^{-1}\mathbb{E}_{\mu}\big[M^{2}_{\lambda}(t)\big]=2\|u_{\lambda}\|_{1}^{2}. (9.3.4)

First, as Luλ=λuλfLu_{\lambda}=\lambda u_{\lambda}-f and uλ,fL2(μ)u_{\lambda},f\in L^{2}(\mu), we have Eμ[(Luλ)2]<E_{\mu}\big[(Lu_{\lambda})^{2}\big]<\infty and so

𝔼μ[(t10tLuλ(ηs)𝑑s)2]Ct(uλL2+fL2)0.\mathbb{E}_{\mu}\Big[\Big(t^{-1}\int_{0}^{t}Lu_{\lambda}(\eta_{s})ds\Big)^{2}\Big]\leq Ct\big(\|u_{\lambda}\|_{L^{2}}+\|f\|_{L^{2}}\big)\rightarrow 0.

Second, to finish,

t1𝔼μ[(uλ(ηt)uλ(η0))2]\displaystyle t^{-1}\mathbb{E}_{\mu}\Big[\Big(u_{\lambda}(\eta_{t})-u_{\lambda}(\eta_{0})\Big)^{2}\Big] =2t1Eμ[uλ2uλPtuλ]\displaystyle=2t^{-1}E_{\mu}\big[u^{2}_{\lambda}-u_{\lambda}P_{t}u_{\lambda}\big]
=2Eμ[uλ(Ptuλuλt)]\displaystyle=-2E_{\mu}\Big[u_{\lambda}\Big(\frac{P_{t}u_{\lambda}-u_{\lambda}}{t}\Big)\Big]
2Eμ[uλLuλ]=2uλ12.\displaystyle\rightarrow-2E_{\mu}\big[u_{\lambda}Lu_{\lambda}\big]=2\|u_{\lambda}\|_{1}^{2}.

As a consequence, we observe

𝔼μ[|Mλ(t)Mθ(t)|2]= 2tuλuθ12 0\mathbb{E}_{\mu}\big[|M_{\lambda}(t)-M_{\theta}(t)|^{2}\big]\ =\ 2t\|u_{\lambda}-u_{\theta}\|_{1}^{2}\ \rightarrow\ 0

as λ,θ0\lambda,\theta\downarrow 0 from (ii). Hence, being a Cauchy sequence, Mλ(t)M(t)M_{\lambda}(t)\rightarrow M(t) in L2(μ)L^{2}(\mu). Therefore, M(t)M(t) (with respect to the natural filtration of ηt\eta_{t}) is a martingale with ergodic and stationary increments such that

𝔼μ[M2(t)]=t𝔼μ[M2(1)]\mathbb{E}_{\mu}\big[M^{2}(t)\big]=t\mathbb{E}_{\mu}\big[M^{2}(1)\big]

and

𝔼μ[M2(1)]=limλ0𝔼μ[Mλ2(1)]= 2limλ0uλ12= 2w12.\mathbb{E}_{\mu}\big[M^{2}(1)\big]\ =\ \lim_{\lambda\downarrow 0}\mathbb{E}_{\mu}\big[M^{2}_{\lambda}(1)\big]\ =\ 2\lim_{\lambda\downarrow 0}\|u_{\lambda}\|^{2}_{1}\ =\ 2\|w\|^{2}_{1}.

Now, the error ζλ(t)\zeta_{\lambda}(t) is handled as follows: By the equation Af(t)=Mλ(t)+ζλ(t)A_{f}(t)=M_{\lambda}(t)+\zeta_{\lambda}(t), we see that a limit ζλ(t)ζ(t)\zeta_{\lambda}(t)\rightarrow\zeta(t) holds as λ0\lambda\downarrow 0 in L2(μ)L^{2}(\mu). Hence, Af(t)=M(t)+ζ(t)A_{f}(t)=M(t)+\zeta(t) and

ζ(t)=Mλ(t)M(t)+ζλ(t).\zeta(t)\ =\ M_{\lambda}(t)-M(t)+\zeta_{\lambda}(t).

By Schwarz inequality, using that μ\mu is invariant, we have by (i), choosing λ=t1\lambda=t^{-1}, that

t1ζλ(t)L2(μ)2\displaystyle t^{-1}\|\zeta_{\lambda}(t)\|_{L^{2}(\mu)}^{2} \displaystyle\leq 3[t1t2λ2uλL22+2t1uλL22]\displaystyle 3\big[t^{-1}t^{2}\lambda^{2}\|u_{\lambda}\|^{2}_{L^{2}}+2t^{-1}\|u_{\lambda}\|^{2}_{L^{2}}\big]
=\displaystyle= Ctut1L22 0\displaystyle\frac{C}{t}\|u_{t^{-1}}\|_{L^{2}}^{2}\ \rightarrow\ 0

as tt\uparrow\infty.

On the other hand,

t1Mt1(t)M(t)L22\displaystyle t^{-1}\|M_{t^{-1}}(t)-M(t)\|^{2}_{L^{2}} =\displaystyle= t1limθ0Mt1(t)Mθ(t)L22\displaystyle t^{-1}\lim_{\theta\downarrow 0}\|M_{t^{-1}}(t)-M_{\theta}(t)\|^{2}_{L^{2}}
=\displaystyle= t12tut1w12 0\displaystyle t^{-1}\cdot 2t\|u_{t^{-1}}-w\|_{1}^{2}\ \rightarrow\ 0

as tt\uparrow\infty.

Finally, we need to identify the variance: By (ii) and Lemma 9.3.4,

2w12= 2w,fμ=limλ02uλ,fμ= 2f12=σf2.2\|w\|_{1}^{2}\ =\ 2\langle w,f\rangle_{\mu}\ =\ \lim_{\lambda\downarrow 0}2\langle u_{\lambda},f\rangle_{\mu}\ =\ 2\|f\|_{-1}^{2}\ =\ \sigma^{2}_{f}.

This finishes the proof of Proposition 9.3.2, subject to Proposition 9.3.6. ∎

9.3.4. Step 3: Proof of Theorem 9.3.1

We now have a representation

1t0tf(ηs)𝑑s=1tM(t)+1tζ(t).\frac{1}{\sqrt{t}}\int_{0}^{t}f(\eta_{s})ds\ =\ \frac{1}{\sqrt{t}}M(t)+\frac{1}{\sqrt{t}}\zeta(t).

The error vanishes in L2(μ)L^{2}(\mu) and 𝔼μ[M2(1)]=σf2\mathbb{E}_{\mu}\big[M^{2}(1)\big]=\sigma^{2}_{f}.

The martingale central limit theorem, Proposition 9.1.1, finishes the proof. ∎

9.3.5. Step 4: Proof of Proposition 9.3.6

We now recall Mazur’s theorem (see [148][Lemma 4.38]). A proof is given at the end.

Lemma 9.3.7.

In a Hilbert space, if xnxx_{n}\rightarrow x weakly, there is a convex combination of the {x1,x2,,xn}\{x_{1},x_{2},\ldots,x_{n}\} which converges strongly to xx, that is xnx0\|x_{n}-x\|\rightarrow 0.

Now, let vnv_{n} be a a convex combination of {uλk}\{u_{\lambda_{k}}\} such that vnwv_{n}\rightarrow w strongly in 1\mathcal{H}_{1}. Then, as Luλnf-Lu_{\lambda_{n}}\rightarrow f weakly in 1\mathcal{H}_{1} and LL is linear, Lvnf-Lv_{n}\rightarrow f weakly in 1\mathcal{H}_{1}. In fact, since L(vnvm)1vnvm1\|L(v_{n}-v_{m})\|_{-1}\leq\|v_{n}-v_{m}\|_{1}, as LL is self-adjoint, we see that {Lvn}\{-Lv_{n}\} is a Cauchy in H1H_{-1}, and hence converges strongly to ff in H1H_{-1}.

Then,

w12=limvn12=limvn,Lvn=w,f.\|w\|^{2}_{1}\ =\ \lim\|v_{n}\|_{1}^{2}\ =\ \lim\langle v_{n},-Lv_{n}\rangle\ =\ \langle w,f\rangle.

Now, returning to the subsequence uλnu_{\lambda_{n}}, by lower semicontinuity and weak convergence of uλnwu_{\lambda_{n}}\rightarrow w in H1H_{1}, and (9.3.2), we have

w12\displaystyle\|w\|_{1}^{2} \displaystyle\leq lim infuλn12\displaystyle\liminf\|u_{\lambda_{n}}\|_{1}^{2}
\displaystyle\leq lim infλnuλnL22+uλn12\displaystyle\liminf\lambda_{n}\|u_{\lambda_{n}}\|^{2}_{L^{2}}+\|u_{\lambda_{n}}\|^{2}_{1}
=\displaystyle= lim inff,uλn\displaystyle\liminf\langle f,u_{\lambda_{n}}\rangle
=\displaystyle= f,w=w12.\displaystyle\langle f,w\rangle\ =\ \|w\|_{1}^{2}.

The same calculation can be repeated with ‘lim inf\liminf’ replaced by ‘lim sup\limsup’.

Therefore, we conclude uλn12w12\|u_{\lambda_{n}}\|_{1}^{2}\rightarrow\|w\|^{2}_{1}, which means uλnwu_{\lambda_{n}}\rightarrow w strongly in 1\mathcal{H}_{1}, and also that λnuλnL220\lambda_{n}\|u_{\lambda_{n}}\|^{2}_{L^{2}}\rightarrow 0.

By the same arguments, on any subsequence of {uλ}\{u_{\lambda}\}, a further subsequence uλnu_{\lambda^{\prime}_{n}} can be found so that λnuλnL220\lambda^{\prime}_{n}\|u_{\lambda^{\prime}_{n}}\|^{2}_{L^{2}}\rightarrow 0. Hence, limλ0λuλ12=0\lim_{\lambda\downarrow 0}\lambda\|u_{\lambda}\|^{2}_{1}=0, showing part (i).

To show part (ii), we need to show that the limit ww is obtained on any subsequential limit of uλu_{\lambda} strongly in 1\mathcal{H}_{1}. To this end, as before, suppose {uλn}\{u_{\lambda^{\prime}_{n}}\} is a subsequence converging strongly to ww^{\prime} in 1\mathcal{H}_{1}. We conclude as before that Luλnf-Lu_{\lambda^{\prime}_{n}}\rightarrow f strongly in 1\mathcal{H}_{-1}. We now show that ww12=0\|w-w^{\prime}\|_{1}^{2}=0 which will finish the claim.

Write,

ww12\displaystyle\|w-w^{\prime}\|_{1}^{2} =\displaystyle= limnuλnuλn12\displaystyle\lim_{n}\|u_{\lambda_{n}}-u_{\lambda^{\prime}_{n}}\|^{2}_{1}
=\displaystyle= limnuλnuλn,Luλn+Luλn\displaystyle\lim_{n}\langle u_{\lambda_{n}}-u_{\lambda^{\prime}_{n}},-Lu_{\lambda_{n}}+Lu_{\lambda^{\prime}_{n}}\rangle
=\displaystyle= limnuλnuλn,λnuλn+λnuλn\displaystyle\lim_{n}\langle u_{\lambda_{n}}-u_{\lambda^{\prime}_{n}},-\lambda_{n}u_{\lambda_{n}}+\lambda^{\prime}_{n}u_{\lambda^{\prime}_{n}}\rangle

since Luλn+Luλn=λnuλn+λnuλn-Lu_{\lambda_{n}}+Lu_{\lambda^{\prime}_{n}}=-\lambda_{n}u_{\lambda_{n}}+\lambda^{\prime}_{n}u_{\lambda^{\prime}_{n}} noting (9.3.2). Now, λnuλn,λnuλn0\lambda^{\prime}_{n}u_{\lambda^{\prime}_{n}},\lambda_{n}u_{\lambda_{n}}\rightarrow 0 weakly in H1H_{-1} (cf. before (9.3.3)). Hence, via the penultimate equation, and the relation Lu1u1\|Lu\|_{-1}\leq\|u\|_{1}, we may approximate uλnu_{\lambda_{n}} by ww and uλnu_{\lambda^{\prime}_{n}} by ww^{\prime}. Then, by the last equation, we see that the right-hand side vanishes. Therefore, w=ww=w^{\prime} in H1H_{1}. This finishes the proof of Proposition 9.3.6. ∎

Proof of Mazur’s Theorem. Let us assume the limit is w=0w=0 without loss of generality. From the weak convergence, one can find iteratively a subsequence {nk}\{n_{k}\} with n1=1n_{1}=1 such that

|unk,unj|k1,for 1j<k.|\langle\langle u_{n_{k}},u_{n_{j}}\rangle\rangle|\ \leq\ k^{-1},\ \ \ {\rm for\ }1\leq j<k.

Then,

1kj=1kunj21k2j=1kunj2+2k21i<jk1j\big\|\frac{1}{k}\sum_{j=1}^{k}u_{n_{j}}\big\|^{2}\ \leq\ \frac{1}{k^{2}}\sum_{j=1}^{k}\|u_{n_{j}}\|^{2}+\frac{2}{k^{2}}\sum_{1\leq i<j\leq k}\frac{1}{j}

which vanishes as kk\uparrow\infty. Hence, we can take vn=k1j=1kunjv_{n}=k^{-1}\sum_{j=1}^{k}u_{n_{j}} for nkn<nk+1n_{k}\leq n<n_{k+1}. ∎

9.4. Notes

Aside from the original paper [131], treatments of the Kipnis-Varadhan theorem, and applications to additive functionals and tagged particles, can be found in [133], [148]. There have been generalizations of the Kipnis-Varadhan theorem to nonreversible situations [202], [212], [159], some of which has been used here, albeit in the reversible setting. In the nonreversible case, as we have seen, it may be that σf2<\sigma^{2}_{f}<\infty but f1,S=\|f\|_{-1,S}=\infty where the 1\mathcal{H}_{-1} norm is with respect to the symmetrized operator S=(L+L)/2-S=-(L+L^{*})/2, e.g. f(η)=η(0)ρf(\eta)=\eta(0)-\rho for ρ1/2\rho\neq 1/2 in d=1d=1. However, a non-asymptotic bound Var(Af(t))f1,S2{\rm Var}\big(A_{f}(t)\big)\leq\|f\|^{2}_{-1,S} holds; see Lemma 12.2.1, Remark 12.2.2. An open problem of interest is to show in the general nonreversible case, with a condition such as f1,S<\|f\|_{-1,S}<\infty, that a CLT holds.

The asymptotic variances in Proposition 9.2.1 and associated CLT’s were first proved in [129]. For more general additive functionals, when ff is not necessarily the occupation function of a site, CLT’s and diffusive variance criteria are proved in [203] for reversible mass conservative systems.

For the asymmetric process with a non-zero drift, Proposition 9.2.2 is proved in a combination of papers [18], [191], [195], [196], and associated CLT’s are shown in [193]. In particular, the paper [195] shows that 1\mathcal{H}_{-1} norms are comparable across d1d\geq 1 finite-range exclusion processes with the same drift. For instance such comparisons would allow to lift variance calculations from d=1d=1 asymmetric simple exclusion processes, e.g. ‘ASEP’ or ‘TASEP’, as in [191], to more general finite-range processes.

The ‘second-class’ particle RtR_{t}, introduced in Subsection 9.2.2 in the context of ASEP is of interest by itself. When the process starts under νρ\nu_{\rho}, in d=1d=1, Var(Rt){\rm Var}\big(R_{t}\big) scales as t4/3t^{4/3} [13], [173], and in d=2d=2 scales as t(logt)2/3t(\log t)^{2/3} [222], both ‘super-diffusive’. In d3d\geq 3, the variance is diffusive of order O(t)O(t); see [143]. However, when the initial condition is a ‘step’ condition (to the left and right with different densities) in d=1d=1, the variance may have different orders [72], [75]; see also [1] and references therein. Moreover, among other properties, the second-class particle in d=1d=1 tracks the location of microscopic ‘shocks’ in the system [72], [73]. See also [2] and references therein for a ‘speed’ process coupling between second-class particles with different priorities.

The superdiffusive conjectures in Remark 9.2.3 regarding Var(Af(t)){\rm Var}\big(A_{f}(t)\big), for η(0)1/2\eta(0)-1/2 and ρ=1/2\rho=1/2, rely on a ‘Gaussian ansatz’, that the local limit terms P¯(Rt=0)t2/3\bar{P}(R_{t}=0)\sim t^{-2/3} in d=1d=1 and t1/2(logt)1/3t^{-1/2}(\log t)^{-1/3} in d=2d=2 scale like the power [Var(Rt)]1/2\big[{\rm Var}(R_{t})\big]^{-1/2}. Verification is an open problem; see however [12] for a weak form of the ansatz in d=1d=1.

In the mean-zero asymmetric setting, variance orders are the same as in the symmetrized process, and CLTs hold when the 1\mathcal{H}_{-1} norm is finite. This would include occupation functionals in d3d\geq 3. See [212] for a Kipnis-Varadhan-type CLT using a ‘sector inequality’ for the generators of mean-zero processes. In d=1d=1 mean-zero asymmetric processes, fractional Brownian motion limits for properly scaled, centered occupation variables have been shown [96]. For d=2d=2 mean-zero asymmetric systems, it is open to show a fluctuation limit for the properly scaled, centered occupation functionals. See [21], [22] for more discussion of these problems in simple exclusion and zero-range processes, when starting from an invariant measure.

Starting from a non-invariant initial condition, LLNs can be inferred for additive functionals in attractive systems such as exclusion processes via ‘local equilibrium’ results; see [130][Chapter 9]. However, less is known about associated fluctuations; see however [65], [217].

Finally, we comment that the study of ‘duality’ (cf. Subsection 9.2.1), and its applications in particle systems and other models has advanced in recent years (cf. [41], [94], [176], and references therein).

Section 10 A tagged particle in symmetric exclusion on ZdZ^{d}

Understanding the motion of a tracer particle, as it interacts with others, is a basic applied concern. We consider here the problem in the finite range symmetric exclusion processes when started under an invariant measure νρ\nu_{\rho}. Except for the case in dimension d=1d=1 when the jump law pp is nearest-neighbor, the tagged particle motion is diffusive and converges to a Brownian motion. In the exceptional case, it can be shown that the motion is subdiffusive and converges to a fractional Brownian motion of Hurst parameter 1/41/4.

First, we discuss LLNs. Then, the diffusive behavior is considered using the Kipnis-Varadhan theorem. Finally, we discuss an exceptional subdiffusive case.

10.1. Tagged problem setting

Consider the dd-dimensional exclusion process ηt\eta_{t} with finite-range translation-invariant jump probability p()p(\cdot), as discussed in Section 9. We will assume that the symmetrized jump probability s()=(p()+p())/2s(\cdot)=\big(p(\cdot)+p(-\cdot)\big)/2 is irreducible. The system consists typically of an infinite number particles. Let us identify one of them initially and let xtx_{t} be its position at time t0t\geq 0. To fix things, suppose it starts at the origin initially, x0=0x_{0}=0.

How to capture the evolution of xtx_{t}, say LLN and CLT statements? With respect to its own history, it is not Markovian because of influence of the other particles. However, if we consider xtx_{t} and ηt\eta_{t} together, then the joint process (xt,ηt)(x_{t},\eta_{t}) is Markovian with generator

L~f(x,η)\displaystyle\tilde{L}f(x,\eta) =\displaystyle= u,vxp(vu)η(u)(1η(v))[f(x,ηu,v)f(x,η)]\displaystyle\sum_{u,v\neq x}p(v-u)\eta(u)(1-\eta(v))\big[f(x,\eta^{u,v})-f(x,\eta)\big]
+vp(v)(1η(x+v))[f(x+v,ηx,x+v)f(x,η)].\displaystyle\ \ +\sum_{v}p(v)(1-\eta(x+v))\big[f(x+v,\eta^{x,x+v})-f(x,\eta)\big].

It will be convenient to consider ‘Lagrangian’ coordinates, or those in the reference frame of the tagged motion. Define ζt=τxtηt\zeta_{t}=\tau_{x_{t}}\eta_{t}, that is ζt(y)=ηt(y+xt)\zeta_{t}(y)=\eta_{t}(y+x_{t}) for all ydy\in\mathbb{Z}^{d} where τx\tau_{x} is shift by xx. Then, the joint process (xt,ζt)(x_{t},\zeta_{t}) is also Markovian and has generator

L^f(x,ζ)\displaystyle\hat{L}f(x,\zeta) =\displaystyle= u,v0p(vu)ζ(u)(1ζ(v))[f(x,ζu,v)f(x,ζ)]\displaystyle\sum_{u,v\neq 0}p(v-u)\zeta(u)(1-\zeta(v))\big[f(x,\zeta^{u,v})-f(x,\zeta)\big]
+vp(v)(1ζ(v))[f(x+v,θvζ)f(x,ζ)]\displaystyle\ \ +\sum_{v}p(v)(1-\zeta(v))\big[f(x+v,\theta_{v}\zeta)-f(x,\zeta)\big]

where θvζ\theta_{v}\zeta is the configuration which exchanges the values ζ(0)\zeta(0) and ζ(v)\zeta(v), displacing the particle at the origin, namely the tagged particle by vv, and then shifts the reference frame to this new origin.

In particular, an explicit description of θvζ\theta_{v}\zeta is given by

(θvζ)(y)={ζ(y+v)foryv,0ζ(v)fory=v1fory=0.(\theta_{v}\zeta)(y)\ =\ \left\{\begin{array}[]{rl}\zeta(y+v)&\ {\rm for\ }y\neq-v,0\\ \zeta(v)&\ {\rm for\ }y=-v\\ 1&\ {\rm for\ }y=0.\end{array}\right.

Both joint processes can be constructed with a core of local functions. Interestingly, the process ζt\zeta_{t} by itself is a Markov process. This can be seen as the generator LL acting on functions of ζ\zeta alone,

Lf(ζ)\displaystyle Lf(\zeta) =\displaystyle= u,v0p(vu)ζ(u)(1ζ(v))[f(ζu,v)f(ζ)]\displaystyle\sum_{u,v\neq 0}p(v-u)\zeta(u)(1-\zeta(v))\big[f(\zeta^{u,v})-f(\zeta)\big]
+vp(v)(1ζ(v))[f(θvζ)f(ζ)],\displaystyle\ \ +\sum_{v}p(v)(1-\zeta(v))\big[f(\theta_{v}\zeta)-f(\zeta)\big],

does not depend on xx, and hence the associated semigroup also does not depend on xx. The process ζt\zeta_{t} ‘drives’ the process xtx_{t} in that xtx_{t} can be recovered in terms of reference frame shifts.

Define Nv(t)N_{v}(t) as the count of shifts of ζ\zeta_{\cdot} of displacement vv up to time tt. Then,

xt=vvNv(t)x_{t}\ =\ \sum_{v}vN_{v}(t) (10.1.1)

where the sum may be restricted to vv in the support of p()p(\cdot). For instance, in one dimension, when pp is nearest-neighbor, xtx_{t} is the number of right shifts minus the number of left shifts.

Moreover, it is not difficult to find invariant measures for ζt\zeta_{t} generated by LL.

Lemma 10.1.1.

The Bernoulli product measure νρ=νρ(|η(0)=1)\nu^{\prime}_{\rho}=\nu_{\rho}(\cdot|\eta(0)=1), conditioned to have a particle at the origin, is invariant for ζt\zeta_{t}. When pp is symmetric, νρ\nu^{\prime}_{\rho} is reversible.

The Dirichlet form can be computed also on local functions:

D(f)\displaystyle D(f) =\displaystyle= Eνρ[f(Lf)]\displaystyle E_{\nu^{\prime}_{\rho}}[f(-Lf)] (10.1.2)
=\displaystyle= 12u,v0s(vu)Eνρ[(f(ζu,v)f(ζ))2]\displaystyle\frac{1}{2}\sum_{u,v\neq 0}s(v-u)E_{\nu^{\prime}_{\rho}}[(f(\zeta^{u,v})-f(\zeta))^{2}]
+12vs(v)Eνρ[(1ζ(v))f(θvζ)f(ζ))2]\displaystyle\ \ \ +\frac{1}{2}\sum_{v}s(v)E_{\nu^{\prime}_{\rho}}[(1-\zeta(v))f(\theta_{v}\zeta)-f(\zeta))^{2}]
=\displaystyle= De(f)+Dt(f)\displaystyle D_{e}(f)+D_{t}(f)

where s()s(\cdot) is the symmetrized probability, s(v)=(p(v)+p(v))/2s(v)=(p(v)+p(-v))/2, assumed to be irreducible on d\mathbb{Z}^{d}.

Lemma 10.1.2.

νρ\nu^{\prime}_{\rho} is extremal for the process ζt\zeta_{t}.

Exercise 10.1.3.

Since νρ\nu^{\prime}_{\rho} is invariant to exchanges of coordinates and also the operator θv\theta_{v}, the proof of Lemma 10.1.1 is similar to the proof of Proposition 2.2.1 which shows νρN\nu^{N}_{\rho} is invariant in the finite-volume setting. Verify these calculations.

Exercise 10.1.4.

Perform the computations to derive the Dirichlet form, and deduce Lemma 10.1.2 following the proof of Theorem 8.4.1.

Now, as before, with zero-range processes, we can extend the process ζt\zeta_{t} to an L2(νρ(|η(0)=1))L^{2}(\nu_{\rho}(\cdot|\eta(0)=1)) process. The problem now is to understand the LLN and fluctuations for xtx_{t} in terms of the formula (10.1.1).

10.1.1. Martingales for xtx_{t}

Each count Nv(t)N_{v}(t), as with a Poisson process, can be compensated by its intensity, 0tp(v)(1ζs(v))𝑑s\int_{0}^{t}p(v)(1-\zeta_{s}(v))ds, to form a martingle

Mv(t)=Nv(t)0tp(v)(1ζs(v))𝑑sM_{v}(t)\ =\ N_{v}(t)-\int_{0}^{t}p(v)(1-\zeta_{s}(v))ds

with quadratic variation

Mv(t)=0tp(v)(1ζs(v))𝑑s.\langle M_{v}\rangle(t)\ =\ \int_{0}^{t}p(v)(1-\zeta_{s}(v))ds.

Then,

v:=Mv2(t)0tp(v)(1ζs(v))𝑑s\mathcal{M}_{v}:=M^{2}_{v}(t)-\int_{0}^{t}p(v)(1-\zeta_{s}(v))ds

is a martingale.

How to verify the above statements? Technically, we should have formed the generator L\vec{L} for the process ({Nv(t)},ζt)(\{N_{v}(t)\},\zeta_{t}). Then, with f({Nv},ζ)=Nvf(\{N_{v}\},\zeta)=N_{v}, we may compute Lf\vec{L}f and Lf22fLf\vec{L}f^{2}-2f\vec{L}f to see that

Mv(t)=f({Nv(t)},ζt)f({Nv(0)},ζ0)0tLf𝑑sM_{v}(t)\ =\ f(\{N_{v}(t)\},\zeta_{t})-f(\{N_{v}(0)\},\zeta_{0})-\int_{0}^{t}\vec{L}fds

and

Mv(t)=0t{Lf22fLf}𝑑s.\langle M_{v}\rangle(t)\ =\ \int_{0}^{t}\big\{\vec{L}f^{2}-2f\vec{L}f\big\}ds.

Although ff is not a bounded function, one may apply truncations to bring it in to the domain of the generator L\vec{L}, while noting Nv(t)N(t):=wNw(t)N_{v}(t)\leq N(t):=\sum_{w}N_{w}(t), a Poisson(1)(1) distributed r.v., to help remove the truncations.

Now, we may write

xt=vvMv(t)+0tvvp(v)(1ζs(v))𝑑s.x_{t}\ =\ \sum_{v}vM_{v}(t)+\int_{0}^{t}\sum_{v}vp(v)(1-\zeta_{s}(v))ds. (10.1.3)

The first term, M^(t)=vMv(t)\hat{M}(t)=\sum vM_{v}(t) is another (vector valued) martingale with quadratic variation, for d\ell\in\mathbb{Z}^{d}, given by

M^(t)=0tv(v)2p(v)(1ζs(v))𝑑s.\langle\hat{M}\cdot\ell\rangle(t)\ =\ \int_{0}^{t}\sum_{v}(v\cdot\ell)^{2}p(v)(1-\zeta_{s}(v))ds. (10.1.4)
Remark 10.1.5.

At this point, we comment, we will need only formulas (10.1.3) and (10.1.4) in the following. These could have been derived from the generator action of L^\hat{L}. The purpose above was to explain more physically their interpretation in terms of counts {Nv}\{N_{v}\}.

We also note, since νρ\nu^{\prime}_{\rho} is extremal, by Proposition 8.3.5, M^(t)\hat{M}(t) has stationary and ergodic increments and, by (10.1.4),

𝔼νρ[(M^(t))2]=t(1ρ)v(v)2p(v).\displaystyle\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big(\hat{M}(t)\cdot\ell\big)^{2}\big]=t(1-\rho)\sum_{v}(v\cdot\ell)^{2}p(v). (10.1.5)

The fourth moment of M^(t)\hat{M}(t)\cdot\ell may also be bounded via a generalization of the Burkholder-Gundy-Davis inequalities:

𝔼νρ[(M^(t))4]\displaystyle\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big(\hat{M}(t)\cdot\ell\big)^{4}\big] C𝔼νρ[max{M^(t)2(t),At(2)}]\displaystyle\leq C\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\max\big\{\langle\hat{M}(t)\cdot\ell\rangle^{2}(t),A_{t}^{(2)}\big\}\big]
C𝔼νρ[M^(t)2(t)]+C𝔼νρ[At(2)]\displaystyle\leq C\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\langle\hat{M}(t)\cdot\ell\rangle^{2}(t)\big]+C\mathbb{E}_{\nu^{\prime}_{\rho}}\big[A_{t}^{(2)}\big]

where At(2)A_{t}^{(2)} is the compensator of the jumps process Dt:=0st(Δ(M^(s)))2=0st(Δ(xs))2D_{t}:=\sum_{0\leq s\leq t}\big(\Delta(\hat{M}(s)\cdot\ell)\big)^{2}=\sum_{0\leq s\leq t}\big(\Delta(x_{s}\cdot\ell)\big)^{2} and Δy(t)=|y(t)y(t)|\Delta y(t)=|y(t)-y(t-)| measures the size of a jump; see [116][Theorem I.3.17] and [110][Corollary 2.4]. It is also known that 𝔼νρ[At(2)]4𝔼νρ[Dt2]\mathbb{E}_{\nu^{\prime}_{\rho}}\big[A_{t}^{(2)}\big]\leq 4\mathbb{E}_{\nu^{\prime}_{\rho}}\big[D^{2}_{t}\big]; see [110][page 4] and [144][Lemma 4.1].

As the range of jumps R<R<\infty, we have |Δ(xs)|R|\Delta(x_{s}\cdot\ell)|\leq R\|\ell\|. Also, the integrand of M^(t)\langle\hat{M}\cdot\ell\rangle(t) is bounded. Then, we may bound

𝔼νρ[(M^(t))4]Ct2.\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big(\hat{M}(t)\cdot\ell\big)^{4}\big]\leq Ct^{2}.

10.2. LLN for xtx_{t}

The law of large numbers for xtx_{t} is already interesting. In some sense xtx_{t} should be a random walk, but it is impeded by the other particles. How much is the question.

Theorem 10.2.1.

Starting under νρ\nu^{\prime}_{\rho}, we have a.s. and in L1L^{1} that

1txt(1ρ)vvp(v).\frac{1}{t}{x_{t}}\ \rightarrow\ (1-\rho)\sum_{v}vp(v).
Proof.

Write

1txt=1tM^(t)+1t0tvvp(v)(1ζs(v))𝑑s.\frac{1}{t}{x_{t}}\ =\ \frac{1}{t}\hat{M}(t)+\frac{1}{t}\int_{0}^{t}\sum_{v}vp(v)(1-\zeta_{s}(v))ds.

Since the fourth moment of |M^(t)||\hat{M}(t)| is bounded by t2t^{2} and νρ\nu^{\prime}_{\rho} is extremal and therefore ergodic to time shifts (Proposition 8.3.5), we have by the ergodic theorem (Birkhoff) that the right side converges to its mean, equal to (1ρ)vvp(v)(1-\rho)\sum_{v}vp(v), both a.s. and in L1L^{1}. ∎

We comment the more simple estimate 𝔼νρ[|M^(t)|2]Ct\mathbb{E}_{\nu^{\prime}_{\rho}}\big[|\hat{M}(t)|^{2}\big]\leq Ct (cf. (10.1.5)) does not lead immediately to a.s. convergence, although L1L^{1} convergence would hold.

10.3. General CLT for xtx_{t}

We now discuss a central limit theorem for xtx_{t} when the jump probability pp is symmetric, first proved in [131]. It can be extended to a functional CLT with respect to a Brownian motion limit, but that is not done here. We mostly follow the scheme in [131].

Theorem 10.3.1.

Let pp be symmetric. Starting under νρ\nu^{\prime}_{\rho}, we have

1txtN(0,𝒞)\frac{1}{\sqrt{t}}x_{t}\ \Rightarrow\ {\rm N}(0,\mathcal{C})

where 𝒞=𝒞(ρ,p)\mathcal{C}=\mathcal{C}(\rho,p) is a covariance matrix.

The limiting covariance 𝒞\mathcal{C} is not explicit, although there are physics conjectures, and some rigorous results for its behavior as a function of ρ\rho [139]. However, it is nondegenerate, except for a particular case.

Proposition 10.3.2.

Except in the case, d=1d=1 and pp is nearest-neighbor (p(1)=p(1)=1/2p(1)=p(-1)=1/2), the covariance 𝒞\mathcal{C} is nondegenerate.

We first prove Theorem 10.3.1 and then later Proposition 10.3.2. Let h(ζ)=(v)p(v)(1ζ(v))h(\zeta)=\sum(v\cdot\ell)p(v)(1-\zeta(v)) be the local, bounded drift function. For d\ell\in\mathbb{Z}^{d}, it will be useful to bound the H1H_{-1} norm, with respect to LL, of h(ζ)h(\zeta)\cdot\ell.

Lemma 10.3.3.

We have h(ζ)=(v)p(v)(1ζ(v))h(\zeta)\cdot\ell=\sum(v\cdot\ell)p(v)(1-\zeta(v)) belongs to H1H_{-1}.

Proof.

Since pp is symmetric, hh is a linear combination of (1ζ(w))(1ζ(w))(1-\zeta(w))-(1-\zeta(-w)) for ww in the support of pp. Consider, as νρ\nu^{\prime}_{\rho} is invariant with respect to the operator θw\theta_{w}, for local functions ϕ\phi that

(1ζ(w))(1ζ(w)),ϕνρ\displaystyle\langle(1-\zeta(w))-(1-\zeta(-w)),\phi\rangle_{\nu^{\prime}_{\rho}}
=Eνρ[(1ζ(w))ϕ(ζ)]Eνρ[(1θw(ζ)(w))ϕ(θw(ζ))]\displaystyle\quad\quad=E_{\nu^{\prime}_{\rho}}[(1-\zeta(w))\phi(\zeta)]-E_{\nu^{\prime}_{\rho}}[(1-\theta_{w}(\zeta)(-w))\phi(\theta_{w}(\zeta))]
=Eνρ[(1ζ(w))(ϕ(ζ)ϕ(θw(ζ))]\displaystyle\quad\quad=E_{\nu^{\prime}_{\rho}}[(1-\zeta(w))(\phi(\zeta)-\phi(\theta_{w}(\zeta))]
Eνρ[(1ζ(w))2(ϕ(ζ)ϕ(θw(ζ))2]1/2\displaystyle\quad\quad\leq E_{\nu^{\prime}_{\rho}}[(1-\zeta(w))^{2}(\phi(\zeta)-\phi(\theta_{w}(\zeta))^{2}]^{1/2}
=Eνρ[(1ζ(w))(ϕ(ζ)ϕ(θw(ζ))2]1/2.\displaystyle\quad\quad=E_{\nu^{\prime}_{\rho}}[(1-\zeta(w))(\phi(\zeta)-\phi(\theta_{w}(\zeta))^{2}]^{1/2}.

Now, the last quantity is less than 2/pminD(ϕ)1/2\sqrt{2/p_{min}}D(\phi)^{1/2} where pmin=min{p(v):vSupp(p)}p_{min}=\min\{p(v):v\in{\rm Supp}(p)\}. Hence, hh\cdot\ell belongs to H1H_{-1}. ∎

Proof of Theorem 10.3.1.

From the martingale decomposition (10.1.3), we have

1txt=1tM^(t)+1t0tvp(v)(1ζs(v))𝑑s.\frac{1}{\sqrt{t}}{x_{t}}\ =\ \frac{1}{\sqrt{t}}\hat{M}(t)+\frac{1}{\sqrt{t}}\int_{0}^{t}\sum vp(v)(1-\zeta_{s}(v))ds.

Since pp is symmetric, the process ζt\zeta_{t} is reversible with respect to νρ\nu^{\prime}_{\rho}. We want to apply the Kipnis-Varadhan apparatus to the second term.

By Lemma 10.3.3, we have hH1h\cdot\ell\in H_{-1}. Then, by Proposition 9.3.2, there is a square integrable martingale M(t)M(t)\cdot\ell and error χ(t)\chi(t) such that |χ(t)|/t|\chi(t)|/\sqrt{t} vanishes in L2L^{2},

0th(ζs)𝑑s=M(t)+χ(t),\int_{0}^{t}h(\zeta_{s})\cdot\ell\ ds\ =\ M(t)\cdot\ell+\chi(t),

and

𝔼νρ[(M(t))2]=t𝔼νρ[(M(1))2]<.\displaystyle\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big(M(t)\cdot\ell\big)^{2}\big]=t\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big(M(1)\cdot\ell\big)^{2}\big]<\infty. (10.3.1)

Hence,

1txt=M^(t)+M(t)t+1tχ(t).\frac{1}{\sqrt{t}}{x_{t}}\ =\ \frac{\hat{M}(t)\cdot\ell+M(t)\cdot\ell}{\sqrt{t}}+\frac{1}{\sqrt{t}}\chi(t).

At this point, one completes the argument by the martingale central limit Theorem 9.1.1, since M^(t)+M(t)\hat{M}(t)+M(t) has stationary and ergodic increments and, noting (10.3.1), (10.1.5),

𝔼νρ[(M^(t)+M(t))2]=t𝔼νρ[((M^+M)(1))2]<.\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big(\hat{M}(t)\cdot\ell+M(t)\cdot\ell\big)^{2}\big]=t\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big((\hat{M}+M)(1)\cdot\ell\big)^{2}\big]<\infty.

Finally, we comment that the covariance 𝒞\mathcal{C} satisfies

2𝒞i,j\displaystyle 2\mathcal{C}_{i,j} =𝔼νρ[((M^+M)(1)(ei+ej))2]\displaystyle=\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big((\hat{M}+M)(1)\cdot(e_{i}+e_{j})\big)^{2}\big]
𝔼νρ[((M^+M)(1)ei)2]𝔼νρ[((M^+M)(1)ej)2].\displaystyle\quad\quad-\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big((\hat{M}+M)(1)\cdot e_{i}\big)^{2}\big]-\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big((\hat{M}+M)(1)\cdot e_{j}\big)^{2}\big].\qed

10.3.1. Proof of Proposition 10.3.2

In the exceptional case, the two martingales M^\hat{M} and MM cancel each other, leading to subdiffusive fluctuations for xtx_{t} discussed in the next subsection. However, in all other situations, full cancellation does not occur.

The argument relies on the following bound. Recall the Dirichlet form DeD_{e} from (10.1.2).

Lemma 10.3.4.

We have for d\ell\in\mathbb{Z}^{d} and ϕL2(νρ)H1\phi\in L^{2}(\nu^{\prime}_{\rho})\cap H_{1} that

|h,ϕνρ|CDe(ϕ)1/2.|\langle h\cdot\ell,\phi\rangle_{\nu^{\prime}_{\rho}}|\ \leq\ CD_{e}(\phi)^{1/2}.
Proof.

From the form of hh, we need only show the result for ζ(w)ζ(w)\zeta(w)-\zeta(-w) where ww is in the support of pp. The key point is that, aside from the exceptional case, one can either go around, in terms of exchanges of coordinates, the origin in d2d\geq 2 or hop over it in d=1d=1, without disturbing the tagged particle sitting at the origin.

One can rewrite, by irreducibility of pp, that

ζ(w)ζ(w)=k=0mζ(qk)ζ(qk+1)\zeta(w)-\zeta(-w)\ =\ \sum_{k=0}^{m}\zeta(q_{k})-\zeta(q_{k+1})

in terms of a sequence from w=q0w=q_{0} to w=qm-w=q_{m} so that p(qk+1qk)>0p(q_{k+1}-q_{k})>0 for 0km0\leq k\leq m. Then,

|ζ(qk)ζ(qk+1),ϕνρ|\displaystyle|\langle\zeta(q_{k})-\zeta(q_{k+1}),\phi\rangle_{\nu^{\prime}_{\rho}}| =Eνρ[ζ(qk)[ϕ(ζ)ϕ(ζqk,qk+1)]\displaystyle=E_{\nu^{\prime}_{\rho}}[\zeta(q_{k})[\phi(\zeta)-\phi(\zeta^{q_{k},q_{k+1}})]
ρ1/2Eνρ[(ϕ(ζ)ϕ(ζqk,qk+1))2]1/2\displaystyle\leq\rho^{1/2}E_{\nu^{\prime}_{\rho}}[(\phi(\zeta)-\phi(\zeta^{q_{k},q_{k+1}}))^{2}]^{1/2}
2ρpminDe(ϕ)1/2.\displaystyle\leq\sqrt{\frac{2\rho}{p_{min}}}D_{e}(\phi)^{1/2}.\qed
Proof of Proposition 10.3.2.

From the formula for the limiting variance, we need to show there is an d\ell\in\mathbb{Z}^{d} such that

limλ0𝔼νρ[(M^(1)+Mλ(1))2]> 0.\lim_{\lambda\downarrow 0}\mathbb{E}_{\nu^{\prime}_{\rho}}\big[(\hat{M}(1)\cdot\ell+M_{\lambda}(1)\cdot\ell)^{2}\big]\ >\ 0.

In the argument below, \ell in the support of pp will suffice.

Step 1. Note that hh is bounded, and consider the resolvent equation

λuλLuλ=h.\lambda u_{\lambda}-Lu_{\lambda}=h\cdot\ell.

Multiply by uλu_{\lambda} and take expectation to obtain λEνρ[uλ2]+uλ12=h,uλνρ\lambda E_{\nu^{\prime}_{\rho}}[u^{2}_{\lambda}]+\|u_{\lambda}\|^{2}_{1}=\langle h\cdot\ell,u_{\lambda}\rangle_{\nu^{\prime}_{\rho}}. Since hH1h\cdot\ell\in H_{-1} by Lemma 10.3.3, we obtain that uλL2(νρ)H1u_{\lambda}\in L^{2}(\nu^{\prime}_{\rho})\cap H_{1}. Hence, we obtain the inequality

uλ12h,uλνρCDe(uλ)\|u_{\lambda}\|_{1}^{2}\ \leq\ \langle h\cdot\ell,u_{\lambda}\rangle_{\nu^{\prime}_{\rho}}\ \leq\ CD_{e}(u_{\lambda}) (10.3.2)

by Lemma 10.3.4.

Let 𝔤(x,ζ)=x+uλ(ζ){{\mathfrak{g}}}(x,\zeta)=x\cdot\ell+u_{\lambda}(\zeta). Then,

M^(t)+Mλ(t)=𝔤(xt,ζt)𝔤(x0,ζ0)0tL^𝔤(xs,ζs)𝑑s.\hat{M}(t)\cdot\ell+M_{\lambda}(t)\cdot\ell\ =\ {{\mathfrak{g}}}(x_{t},\zeta_{t})-{{\mathfrak{g}}}(x_{0},\zeta_{0})-\int_{0}^{t}\hat{L}{{\mathfrak{g}}}(x_{s},\zeta_{s})ds.

By a similar argument as for (9.3.4) (in the proof of the Kipnis-Varadhan Proposition 9.3.2), we have

𝔼νρ[(M^(1)+Mλ(1))2]=1t𝔼νρ[(𝔤(xt,ζt)𝔤(x0,ζ0))2]=2Eνρ[𝔤L^𝔤].\mathbb{E}_{\nu^{\prime}_{\rho}}\big[(\hat{M}(1)\cdot\ell+M_{\lambda}(1)\cdot\ell)^{2}\big]\ =\ \frac{1}{t}\mathbb{E}_{\nu^{\prime}_{\rho}}\big[({{\mathfrak{g}}}(x_{t},\zeta_{t})-{{\mathfrak{g}}}(x_{0},\zeta_{0}))^{2}\big]\ =\ -2E_{\nu^{\prime}_{\rho}}\big[{{\mathfrak{g}}}\hat{L}{{\mathfrak{g}}}\big].

An explicit computation gives that the right hand side equals

Eνρ[u,v0p(vu)[𝔤(x,ζu,v)𝔤(x,ζ)]2]\displaystyle E_{\nu^{\prime}_{\rho}}\Big[\sum_{u,v\neq 0}p(v-u)\big[{{\mathfrak{g}}}(x,\zeta^{u,v})-{{\mathfrak{g}}}(x,\zeta)\big]^{2}\Big]
+Eνρ[vp(v)(1ζ(v))[𝔤(x+v,θvζ)𝔤(x,ζ)]2].\displaystyle\ \ +E_{\nu^{\prime}_{\rho}}\Big[\sum_{v}p(v)(1-\zeta(v))\big[{{\mathfrak{g}}}(x+v,\theta_{v}\zeta)-{{\mathfrak{g}}}(x,\zeta)\big]^{2}\Big].

The first term is 2De(uλ)2D_{e}(u_{\lambda}). Then, by dropping the second term, we have the lower bound

𝔼νρ[(M^(1)+Mλ(1))2] 2De(uλ).\mathbb{E}_{\nu^{\prime}_{\rho}}\big[(\hat{M}(1)\cdot\ell+M_{\lambda}(1)\cdot\ell)^{2}\big]\ \geq\ 2D_{e}(u_{\lambda}).

Step 2. Now, if uλ1\|u_{\lambda}\|_{1} vanishes as λ0\lambda\downarrow 0, we have

𝔼νρ[(Mλ(1))2]= 2uλ12 0\mathbb{E}_{\nu^{\prime}_{\rho}}\big[\big(M_{\lambda}(1)\cdot\ell\big)^{2}\big]\ =\ 2\|u_{\lambda}\|_{1}^{2}\ \rightarrow\ 0

and so the limiting variance would be 𝔼νρ[(M^(1))2]=2v(v)2p(v)(1ρ)\mathbb{E}_{\nu^{\prime}_{\rho}}\big[(\hat{M}(1)\cdot\ell)^{2}\big]=2\sum_{v}(v\cdot\ell)^{2}p(v)(1-\rho) which is positive for \ell in the support of pp.

On the other hand, if uλ1↛0\|u_{\lambda}\|_{1}\not\rightarrow 0, then De(uλ)D_{e}(u_{\lambda}) also does not vanish by (10.3.2). Hence, still the limiting variance is positive. ∎

10.4. Subdiffusive CLT in the exceptional case

Since particles are ordered in d=1d=1 when the transition probability pp is nearest-neighbor, one may suspect that the expected displacement of a particle n time tt may be less than diffusive when pp is additionally symmetric. This is indeed the case, when starting under νρ\nu^{\prime}_{\rho}.

Theorem 10.4.1.

Starting under νρ\nu^{\prime}_{\rho}, we have

1t1/4xtN(0,σ2)\frac{1}{t^{1/4}}x_{t}\ \Rightarrow\ {\rm N}(0,\sigma^{2})

where σ2=2/π[(1ρ)/ρ]\sigma^{2}=\sqrt{2/\pi}[(1-\rho)/\rho].

A functional CLT is also known, but here instead of Brownian motion the limit will be a fractional BM with Hurst parameter 1/41/4 [165].

There are a couple of ways to prove this subdiffusive CLT, first proved in [9]. Another proof was given in [183]. We present a method which makes a connection with the current through the bond (1,0)(-1,0) based on [57].

Define

J1,0(t)=N+(t)N(t)J_{-1,0}(t)\ =\ N_{+}(t)-N_{-}(t)

where N+(t)N_{+}(t) is the number of particles which start on the left of x=1/2x=1/2 and move across the bond (1,0)(-1,0) up to time tt, and N(t)N_{-}(t) is the number of particles to the right of x=1/2x=1/2 crossing to the left.

Then, we have the following relations between xtx_{t} and J1,0(t)J_{-1,0}(t):

{xtA}\displaystyle\{x_{t}\geq A\} =\displaystyle= {J1,0(t)x=1A1ηt(x)}whenA1\displaystyle\{J_{-1,0}(t)\geq\sum_{x=1}^{A-1}\eta_{t}(x)\}\ \ {\rm when\ }A\geq 1
{xt=0}\displaystyle\{x_{t}=0\} =\displaystyle= {J1,0(t)=0}\displaystyle\{J_{-1,0}(t)=0\}
{xtA}\displaystyle\{x_{t}\leq A\} =\displaystyle= {J1,0(t)x=A+10ηt(x)}whenA1.\displaystyle\{J_{-1,0}(t)\leq\sum_{x=A+1}^{0}\eta_{t}(x)\}\ \ {\rm when\ }A\leq-1. (10.4.1)

We will show the following result which will imply Theorem 10.4.1. The proof of Theorem 10.4.2 is deferred to Subsection 10.4.3.

Theorem 10.4.2.

Starting under νρ\nu^{\prime}_{\rho}, we have

1t1/4J1,0(t)N(0,ρ2σ2).\frac{1}{t^{1/4}}J_{-1,0}(t)\ \Rightarrow\ {\rm N}(0,\rho^{2}\sigma^{2}).

We now give the proof of Theorem 10.4.1.

Proof of Theorem 10.4.1.

Write, for A>0A>0, that

νρ(xtAt1/4)\displaystyle\mathbb{P}_{\nu^{\prime}_{\rho}}\big(x_{t}\geq At^{1/4}\big) =\displaystyle= νρ(J1,0(t)x=1At1/41ηt(x))\displaystyle\mathbb{P}_{\nu^{\prime}_{\rho}}\Big(J_{-1,0}(t)\geq\sum_{x=1}^{\lceil At^{1/4}\rceil-1}\eta_{t}(x)\Big)
=\displaystyle= νρ(t1/4J1,0(t)t1/4x=1At1/41ηt(x)).\displaystyle\mathbb{P}_{\nu^{\prime}_{\rho}}\Big(t^{-1/4}J_{-1,0}(t)\geq t^{-1/4}\sum_{x=1}^{\lceil At^{1/4}\rceil-1}\eta_{t}(x)\Big).

Since, under νρ\nu^{\prime}_{\rho}, {ηt(x)}x1\{\eta_{t}(x)\}_{x\geq 1} are i.i.d. Bernoulli random variables,

t1/4x=1At1/41ηt(x)Aρa.s.t^{-1/4}\sum_{x=1}^{\lceil At^{1/4}\rceil-1}\eta_{t}(x)\ \rightarrow\ A\rho\ \ \ {\rm a.s.}

Then, from Theorem 10.4.2, we have

limtνρ(xtAt1/4)\displaystyle\lim_{t\rightarrow\infty}\mathbb{P}_{\nu^{\prime}_{\rho}}(x_{t}\geq At^{1/4}) =limtνρ(t1/4J1,0(t)Aρ)\displaystyle=\lim_{t\rightarrow\infty}\mathbb{P}_{\nu^{\prime}_{\rho}}\big(t^{-1/4}J_{-1,0}(t)\geq A\rho\big)
=P(N(0,σ2ρ2)Aρ).\displaystyle=P\big({\rm N}(0,\sigma^{2}\rho^{2})\geq A\rho\big).

The right-hand side is the same as P(N(0,σ2)A)P({\rm N}(0,\sigma^{2})\geq A).

A similar argument works for A<0A<0. ∎

10.4.1. Stirring representation

One way to prove Theorem 10.4.2 is to use a ‘graphical’ representation of symmetric exclusion process (cf. [147][Chapter 8). We present the representation in the nearest-neighbor setting in d=1d=1.

Recall that the generator for symmetric simple exclusion has form (cf. (2.2.2))

Lϕ(η)=x[ϕ(ηx,x+1)ϕ(η)].L\phi(\eta)\ =\ \sum_{x\in\mathbb{Z}}\big[\phi(\eta^{x,x+1})-\phi(\eta)\big].

In other words, the process evolves by ‘exchanging’ values with neighboring coordinate variables.

Now, consider a collection of Poisson processes with intensity 1/21/2 indexed by the bonds {(x,x+1):x}\{(x,x+1):x\in\mathbb{Z}\}. Place a particle at each vertex in \mathbb{Z}. At the event times of the Poisson process with index (x,x+1)(x,x+1), the particles at xx and x+1x+1 exchange positions. Let ξtx\xi^{x}_{t} be the location of the particle intially at xx at time t0t\geq 0. Marginally, each ξtx\xi^{x}_{t} has the statistics of a nearest-neighbor symmetric random walk, although jointly they are dependent.

We claim that

ηt(x)= 1{x{ξti:η0(i)=1}},\eta_{t}(x)\ =\ 1\big\{x\in\{\xi^{i}_{t}:\eta_{0}(i)=1\}\big\},

that is ηt(x)=1\eta_{t}(x)=1 exactly when there is an ii\in\mathbb{Z} such that ξti=x\xi^{i}_{t}=x and η0(i)=1\eta_{0}(i)=1. Infinitesimally, the possible transitions are exchanges of nearest-neighbor values which is the same as given in the generator LL. Then,

J1,0(t)=i<01(ξti0)η0(i)i01(ξti<0)η0(i).J_{-1,0}(t)\ =\ \sum_{i<0}1(\xi^{i}_{t}\geq 0)\eta_{0}(i)-\sum_{i\geq 0}1(\xi^{i}_{t}<0)\eta_{0}(i).

Define now

K+(t)=i<01{ξti0},andK(t)=i01{ξti<0}K_{+}(t)=\sum_{i<0}1\{\xi^{i}_{t}\geq 0\},\ \ {\rm and\ \ }K_{-}(t)=\sum_{i\geq 0}1\{\xi^{i}_{t}<0\}

which represent the number of stirring particles starting from the left of the origin which end up on the right at time tt, and vice versa.

Since, in the stirring process, a crossing of the bond (1,0)(-1,0) in one direction corresponds to a crossing in the other direction, as all sites are occupied by stirring particles, we have K+(t)K(t)K_{+}(t)-K_{-}(t) is constant in time. But, K+(0)=K(0)=0K_{+}(0)=K_{-}(0)=0, and hence K(t):=K+(t)=K(t)K(t):=K_{+}(t)=K_{-}(t) for all t0t\geq 0. When K(t)1K(t)\geq 1, let i1<i2<<iK(t)<0i_{1}<i_{2}<\cdots<i_{K(t)}<0 be the random locations where ξtik0\xi_{t}^{i_{k}}\geq 0, and 0j1<<jK(t)0\leq j_{1}<\cdots<j_{K(t)} be the random locations where ξtjk<0\xi_{t}^{j_{k}}<0. Then, we can write the current as

J1,0(t)=k=1K(t)ak\displaystyle J_{-1,0}(t)\ =\ \sum_{k=1}^{K(t)}a_{k} (10.4.2)

where ak(t)=η0(ik)η0(jk)a_{k}(t)=\eta_{0}(i_{k})-\eta_{0}(j_{k}); Note the time dependence on tt comes from the random locations ik,jki_{k},j_{k} which depend on tt. Conditionally on K(t)K(t), and the random locations, the variables {ak}k=1K(t)\{a_{k}\}_{k=1}^{K(t)} are independent with respect to νρ\nu^{\prime}_{\rho}. Moreover, conditionally, only the variable α1\alpha_{1}, if j1=0j_{1}=0, is different from {αk}k=2K(t)\{\alpha_{k}\}_{k=2}^{K(t)} which are i.i.d., taking values 1,0,1-1,0,1 with mean 00 and variance 2ρ(1ρ)2\rho(1-\rho).

10.4.2. Estimates on KK

In the following, PP and EE refer to the stirring process probability and expectation when η0\eta_{0} is distributed according to νρ\nu^{\prime}_{\rho}. We have the following properties of KK.

Lemma 10.4.3.

We have

t1/2E[K(t)](2π)1/2.t^{-1/2}E[K(t)]\ \rightarrow\ (2\pi)^{-1/2}.
Proof.

Write, by symmetry,

E[K(t)]\displaystyle E[K(t)] =\displaystyle= i<0P(ξti0)=i<0P(ξt0i)\displaystyle\sum_{i<0}P(\xi^{i}_{t}\geq 0)\ =\ \sum_{i<0}P(\xi^{0}_{t}\geq-i)
=\displaystyle= i>0P(ξt0i)=E[(z(t))+]\displaystyle\sum_{i>0}P(\xi^{0}_{t}\geq i)\ =\ E[(z(t))_{+}]

where z(t)z(t) is a simple random walk starting at the origin and (z(t))+(z(t))_{+} is the positive part.

Now, {t1/2z(t)}\{t^{-1/2}z(t)\} is a uniformly integrable sequence of random variables which converges in distribution to N(0,1){\rm N}(0,1). Hence,

t1/2E[K(t)]0(2π)1/2xex2/2dx= 1.t^{-1/2}E[K(t)]\ \rightarrow\ \int_{0}^{\infty}(2\pi)^{-1/2}xe^{-x^{2}/2}dx\ =\ 1.\qed

We also have that the variables 1(ξtx0)1(\xi^{x}_{t}\geq 0) and 1(ξty0)1(\xi^{y}_{t}\geq 0) are negatively correlated, which makes intuitive sense since the exchange mechanism is repulsive to an extent.

Lemma 10.4.4.

For x,y<0x,y<0, we have that

P(ξtx,ξty0)P(ξtx0)P(ξty0).P(\xi^{x}_{t},\xi^{y}_{t}\geq 0)\ \leq\ P(\xi^{x}_{t}\geq 0)P(\xi^{y}_{t}\geq 0).

We refer the reader to Lemma 4.12 [147] or page 365 [9] for proofs of the lemma (in a more general context). See also the discussion in [150], which shows a very general form of negative association, a ‘strong Rayleigh’ condition for symmetric exclusion processes started from product measures.

A consequence of the Lemma 10.4.4 is that Var(K(t))E[K(t)]{\rm Var}(K(t))\leq E[K(t)].

10.4.3. Proof of Theorem 10.4.2

Consider the following steps.

Step 1. To prove the theorem, noting (10.4.2), we show that the following difference converges in probability, as tt\rightarrow\infty,

W(t)=t1/4[k=1K(t)akk=1(2π)1/2t1/2ak] 0.W(t)\ =\ t^{-1/4}\Big[\sum_{k=1}^{K(t)}a_{k}-\sum_{k=1}^{\lfloor(2\pi)^{-1/2}t^{1/2}\rfloor}a_{k}\Big]\ \rightarrow\ 0.

We make explicit the contribution of the term α1\alpha_{1} which might reflect the tagged particle initially at the origin: Write, noting empty sums vanish,

W(t)\displaystyle W(t) =W(t)1(K(t)=0)+W(t)1(K(t)1)\displaystyle=W(t)1(K(t)=0)+W(t)1(K(t)\geq 1)
=t1/4[k=2K(t)akk=2(2π)1/2t1/2ak]1(K(t)1),\displaystyle=t^{-1/4}\Big[\sum_{k=2}^{K(t)}a_{k}-\sum_{k=2}^{\lfloor(2\pi)^{-1/2}t^{1/2}\rfloor}a_{k}\Big]1(K(t)\geq 1),

with respect to variables {αk}k=2K(t)\{\alpha_{k}\}_{k=2}^{K(t)} which are i.i.d. mean 00 and variance 2ρ(1ρ)2\rho(1-\rho), conditionally on K(t),{ik,jk}K(t),\{i_{k},j_{k}\}.

Then, the variance, noting the conditional mean vanishes,

Var(W(t))\displaystyle{\rm Var}(W(t)) =\displaystyle= E[E[W(t)2|K(t),{ik,jk}]]\displaystyle E\Big[E[W(t)^{2}|K(t),\{i_{k},j_{k}\}]\Big]
\displaystyle\leq 2ρ(1ρ)t1/2E[|K(t)(2π)1/2t1/2|]\displaystyle 2\rho(1-\rho)t^{-1/2}E\Big[\big|K(t)-\lfloor(2\pi)^{-1/2}t^{1/2}\rfloor\big|\Big]
\displaystyle\leq 2ρ(1ρ)t1/2E[|K(t)E[K(t)]|]\displaystyle 2\rho(1-\rho)t^{-1/2}E\Big[\big|K(t)-E[K(t)]\big|\Big]
+2ρ(1ρ)t1/2|E[K(t)](2π)1/2t1/2|.\displaystyle\ \ \ \ +2\rho(1-\rho)t^{-1/2}\big|E[K(t)]-\lfloor(2\pi)^{-1/2}t^{1/2}\rfloor\big|.

Since K(t)K(t) is the sum of negatively correlated random variables, we have Var(K(t))E[K(t)]=O(t1/2){\rm Var}(K(t))\leq E[K(t)]=O(t^{1/2}) and also t1/2|E[K(t)](2π)1/2|=o(1)t^{-1/2}\big|E[K(t)]-(2\pi)^{-1/2}\big|=o(1) by Lemma 10.4.3. Hence, for b>0b>0, we can apply Chebychev’s inequality to get

P(W(t)>b)b2Var(W(t))b2[O(t1/4)+o(1)] 0.P(W(t)>b)\ \leq\ b^{-2}{\rm Var}(W(t))\ \leq\ b^{-2}\big[O(t^{-1/4})+o(1)\big]\ \rightarrow\ 0.

Step 2. Now, since α11(K(t)1)\alpha_{1}1(K(t)\geq 1) is bounded, t1/4α11(K(t)1)0t^{-1/4}\alpha_{1}1(K(t)\geq 1)\rightarrow 0 a.s. Hence, to finish the argument, we will take the limit of

E[exp{iθ1t1/4k=2(2π)1/2t1/2ak}]\displaystyle E\Big[\exp\Big\{i\theta\frac{1}{t^{1/4}}\sum_{k=2}^{\lfloor(2\pi)^{-1/2}t^{1/2}\rfloor}a_{k}\Big\}\Big]
=E[E[exp{iθ1t1/4k=2(2π)1/2t1/2ak}|K(t),{ik,jk}]].\displaystyle\ \ \ =\ E\Big[E\Big[\exp\Big\{i\theta\frac{1}{t^{1/4}}\sum_{k=2}^{\lfloor(2\pi)^{-1/2}t^{1/2}\rfloor}a_{k}\Big\}\Big|K(t),\{i_{k},j_{k}\}\Big]\Big].

Note, by Lemma 10.4.3, that ((2π)1/2b)t1/2K(t)((2π)1/2+b)t1/2((2\pi)^{-1/2}-b)t^{1/2}\leq K(t)\leq((2\pi)^{-1/2}+b)t^{1/2} with high probability for each b>0b>0. Then, there are roughly ((2π)1/2±b)t1/2\lfloor((2\pi)^{-1/2}\pm b)t^{1/2}\rfloor summands in the sum above, with high probability.

Hence, the last display may be approximated by

E[ψ(θt1/4)(2π)1/2t1/2+o(t1/2)],\displaystyle E\Big[\psi\big(\theta t^{-1/4}\big)^{\lfloor(2\pi)^{-1/2}t^{1/2}\rfloor+o(t^{1/2})\rfloor}\Big],

where ψ\psi is the characteristic function of aka_{k} conditioned on K(t)K(t) and the random locations, which has an explicit distribution on values 0,1,10,-1,1 with mean 00 and variance 2ρ(1ρ)2\rho(1-\rho). One now follows the strategy for the usual CLT to obtain the last term converges to the characteristic function of a Normal r.v. with variance 2ρ(1ρ)(2π)1/2=2/πρ(1ρ)2\rho(1-\rho)\cdot(2\pi)^{-1/2}=\sqrt{2/\pi}\rho(1-\rho) as desired. ∎

10.5. Notes

The tagged particle problem, starting from νρ\nu_{\rho}, is somewhat complete at the level of LLN and CLT for symmetric exclusion processes with finite range on d\mathbb{Z}^{d}. See [147], [148] and references therein for treatments. See also [117] for longer range symmetric exclusion processes. Large and moderate deviations have also been studied [155], [200], [201], [218]. See also [209] and references therein for related work on random walk in random environment.

For asymmetric simple exclusion, a CLT has been shown in diffusive scale when d3d\geq 3 [202], or when d=1d=1 and the jumps are nearest-neighbor [128]. Also, when the jumps are mean-zero, finite-range, but asymmetric in d1d\geq 1, the CLT also holds [212].

When the jumps are asymmetric with a nonzero drift, the variance of the tagged particle at time tt is shown to be diffusive, in the sense of Laplace transforms for all d=1,2d=1,2 [197]. However, the associated CLT, when d=2d=2 and when d=1d=1 and the jumps are not nearest-neighbor, is open.

When starting out of the invariant measure, the LLN behavior has been studied in [180], but less is known for the fluctuations or other limits; see however [118], [47], [49], [50], [65], [211].

See also [114], [120], [121], [198] for discussions and some results for a tagged particle in zero-range models. On other spaces, such as trees, see [45], [93] for recent developments.

We comment that the tagged particle problem is an old one going back at least to Einstein’s 1905 opus. Recently, derivation of Brownian motion rigorously from deterministic hard sphere dynamics with elastic collisions, where initially positions of particles are in thermal equilibrium, has been addressed in [29]. See [90], [7], [206], [210] for reviews and discussions.

Section 11 Equilibrium fluctuations of symmetric exclusion

We motivate the study of ‘equilibrium’ fluctuations of dd-dimensional symmetric exclusion via another proof of the t1/4t^{1/4}-scaling limit of the current, Theorem 10.4.2, in the one dimensional nearest-neighbor process. ‘Equilibrium’ fluctuations capture the CLT behavior of the empirical mass density around the constant solution of the hydrodynamic equation, when started from an invariant measure νρ\nu_{\rho}. The limiting equation is a type of linear stochastic heat equation, an SPDE whose solution is an infinite dimensional ‘Ornstein-Uhlenbeck’ process.

We will focus our discussion in the symmetric simple exclusion context when p(±ei)=(2d)1p(\pm e_{i})=(2d)^{-1} with respect to the standard basis {ei}i=1d\{e_{i}\}_{i=1}^{d}.

11.1. Another derivation of the current fluctuations limit

Consider the d=1d=1 nearest-neighbor, symmetric exclusion setting discussed in Subsection 10.4. Recall the current Jx,x+1(t)J_{x,x+1}(t) through the bond (x,x+1)(x,x+1) in \mathbb{Z} is the number of particles crossing the bond from left to right minus the number crossing from right to left up to time tt.

A moment’s thought gives, reflecting the boundary values at xx, that

Jx1,x(t)Jx,x+1(t)=ηt(x)η0(x),J_{x-1,x}(t)-J_{x,x+1}(t)\ =\ \eta_{t}(x)-\eta_{0}(x),

the difference being equal to 00, 11 or 1-1. Then, formally,

J1,0(t)=x0Jx1,x(t)Jx,x+1(t)=x0ηt(x)η0(x).J_{-1,0}(t)\ =\ \sum_{x\geq 0}J_{x-1,x}(t)-J_{x,x+1}(t)\ =\ \sum_{x\geq 0}\eta_{t}(x)-\eta_{0}(x).

However, the display does not make sense as typically there are an infinite number of particles in the system.

We may truncate however in the following way: Let

Gn(x)=(1xn)1(0xn).G_{n}(x)\ =\ \Big(1-\frac{x}{n}\Big)1(0\leq x\leq n).

Write, in terms of a scaling parameter NN, that

x0Gn(x/N)[Jx1,x(t)Jx,x+1(t)]\displaystyle\sum_{x\geq 0}G_{n}(x/N)\big[J_{x-1,x}(t)-J_{x,x+1}(t)\big]
=J1,0(t)+x1[Gn(x/N)Gn(x1/N)]Jx1,x(t)\displaystyle\ \ \ \ =J_{-1,0}(t)+\sum_{x\geq 1}\big[G_{n}(x/N)-G_{n}(x-1/N)\big]J_{x-1,x}(t)
=J1,0(t)+1nNx=1N+1Jx1,x(t).\displaystyle\ \ \ \ =J_{-1,0}(t)+\frac{1}{nN}\sum_{x=1}^{N+1}J_{x-1,x}(t).

At the same time, we have

x0Gn(x/N)[Jx1,x(t)Jx,x+1(t)]\displaystyle\sum_{x\geq 0}G_{n}(x/N)\big[J_{x-1,x}(t)-J_{x,x+1}(t)\big] =\displaystyle= x0Gn(x/N)[ηt(x)η0(x)].\displaystyle\sum_{x\geq 0}G_{n}(x/N)\big[\eta_{t}(x)-\eta_{0}(x)\big].

Following our custom, since space is scaled by NN, we will speed up time by N2N^{2}, and define the mass ‘fluctuation field’ WtNW^{N}_{t} with respect to d\mathbb{Z}^{d} by its action on GG:

WtN(G)=1Nd/2xdG(x/N)(ηN2t(x)ρ),W^{N}_{t}(G)\ =\ \frac{1}{N^{d/2}}\sum_{x\in\mathbb{Z}^{d}}G(x/N)\big(\eta_{N^{2}t}(x)-\rho\big), (11.1.1)

here written for d1d\geq 1.

In d=1d=1, scaling the current by the fourth root of the time scaling, we have for all n1n\geq 1 that

1NJ1,0(N2t)=WtN(Gn)W0N(Gn)1nN3/2x=1N+1Jx1,x(N2t).\displaystyle\frac{1}{\sqrt{N}}J_{-1,0}(N^{2}t)=W^{N}_{t}(G_{n})-W^{N}_{0}(G_{n})-\frac{1}{nN^{3/2}}\sum_{x=1}^{N+1}J_{x-1,x}(N^{2}t). (11.1.2)

The idea now is that the first two terms on the right should be given in terms of a limit fluctuation field WtW_{t}, which we must define, while the last term on the right hand side should vanish as NN\uparrow\infty and nn\uparrow\infty.

One can adjust the construction of the process (cf. Remark 10.1.5), to include counts Nx,x+1+(t)N^{+}_{x,x+1}(t) and Nx,x+1(t)N^{-}_{x,x+1}(t), keeping track of the numbers of particles crossing (x,x+1)(x,x+1) from left to right and vice versa. Then, Jx,x+1(t)=Nx,x+1+(t)Nx,x+1(t)J_{x,x+1}(t)=N^{+}_{x,x+1}(t)-N^{-}_{x,x+1}(t) and

Mx,x+1(t)\displaystyle M_{x,x+1}(t) =Jx,x+1(t)120t[ηs(x)(1ηs(x+1))ηs(x+1)(1ηs(x))]𝑑s\displaystyle=J_{x,x+1}(t)-\frac{1}{2}\int_{0}^{t}\big[\eta_{s}(x)(1-\eta_{s}(x+1))-\eta_{s}(x+1)(1-\eta_{s}(x))\big]ds
=Jx,x+1(t)120t[ηs(x)ηs(x+1)]dsand\displaystyle=J_{x,x+1}(t)-\frac{1}{2}\int_{0}^{t}\big[\eta_{s}(x)-\eta_{s}(x+1)\big]ds\ \ {\rm and}
Mx,x+1(t)2120t[ηs(x)(1ηs(x+1))+ηs(x+1)(1ηs(x))]𝑑sM_{x,x+1}(t)^{2}-\frac{1}{2}\int_{0}^{t}\big[\eta_{s}(x)(1-\eta_{s}(x+1))+\eta_{s}(x+1)(1-\eta_{s}(x))\big]ds

are martingales. Since jumps are not simultaneous in the process, {Mx,x+1(t)}x\{M_{x,x+1}(t)\}_{x\in\mathbb{Z}} are orthogonal martingales.

Exercise 11.1.1.

Show E[Mx,x+1(t)My,y+1(t)]=0E[M_{x,x+1}(t)M_{y,y+1}(t)]=0 by decomposing on the possible crossing times of bonds (x,x+1)(x,x+1) and (y,y+1)(y,y+1), which are stopping times occurring a.s. at distinct times, and the martingale property. That is, write Mx,x+1(t)=(Mx,x+1(τk+1)Mx,x+1(τk))M_{x,x+1}(t)=\sum(M_{x,x+1}(\tau_{k+1})-M_{x,x+1}(\tau_{k})) and a similar formula for My,y+1(t)M_{y,y+1}(t) where 0=τ0<<τN(t)<τN(t)+1=t0=\tau_{0}<\cdots<\tau_{N(t)}<\tau_{N(t)+1}=t are the N(t)N(t) jumps on these bonds up to time tt. Then, we have

E[(Mx,x+1(τk+1)Mx,x+1(τk))(My,y+1(τj+1)My,y+1(τj))]E\big[(M_{x,x+1}(\tau_{k+1})-M_{x,x+1}(\tau_{k}))(M_{y,y+1}(\tau_{j+1})-M_{y,y+1}(\tau_{j}))\big]

equals zero if k=jk=j since jumps are not simultaneous. But, if k<jk<j, then since My,y+1(τj+1t)M_{y,y+1}(\tau_{j+1}\wedge t) is a martingale, the display also vanishes.

In the following, recall as before that EμE_{\mu} stands for the probability and expectation under μ\mu, and μ\mathbb{P}_{\mu} and 𝔼μ\mathbb{E}_{\mu} for the process measure and expectation when starting in μ\mu.

Lemma 11.1.2.

Starting in an invariant measure, νρ\nu_{\rho}, we have

limnsupN1𝔼νρ[(1nN3/2x=1N+1Jx1,x(N2t))2]= 0.\lim_{n\uparrow\infty}\sup_{N\geq 1}\mathbb{E}_{\nu_{\rho}}\Big[\Big(\frac{1}{nN^{3/2}}\sum_{x=1}^{N+1}J_{x-1,x}(N^{2}t)\Big)^{2}\Big]\ =\ 0.
Proof.

Write

1nN3/2x=1N+1Jx1,x(N2t)\displaystyle\frac{1}{nN^{3/2}}\sum_{x=1}^{N+1}J_{x-1,x}(N^{2}t)
=1nN3/2x=1N+1120N2t[η(x1)(1η(x))η(x)(1η(x1))]𝑑s\displaystyle\quad\quad=\frac{1}{nN^{3/2}}\sum_{x=1}^{N+1}\frac{1}{2}\int_{0}^{N^{2}t}\big[\eta(x-1)(1-\eta(x))-\eta(x)(1-\eta(x-1))\big]ds
+1nN3/2x=1N+1Mx1,x(N2t)\displaystyle\quad\quad\ \ \ \ \ +\ \frac{1}{nN^{3/2}}\sum_{x=1}^{N+1}M_{x-1,x}(N^{2}t) (11.1.3)
=1nN3/2120N2t[ηs(0)ηs(N)]𝑑s+1nN3/2x=1N+1Mx1,x(N2t).\displaystyle\quad\quad=\frac{1}{nN^{3/2}}\frac{1}{2}\int_{0}^{N^{2}t}\big[\eta_{s}(0)-\eta_{s}(N)\big]ds+\frac{1}{nN^{3/2}}\sum_{x=1}^{N+1}M_{x-1,x}(N^{2}t).

Here, we used that η(x1)(1η(x))η(x)(1η(x1))=η(x1)η(x)\eta(x-1)(1-\eta(x))-\eta(x)(1-\eta(x-1))=\eta(x-1)-\eta(x).

Now, from an H1H_{-1}-norm/variance estimate Proposition 9.2.1, we have for all yy that

𝔼νρ[(0N2t(ηs(y)ρ)𝑑s)2]C(ρ)N3/2t3/2.\mathbb{E}_{\nu_{\rho}}\Big[\Big(\int_{0}^{N^{2}t}\big(\eta_{s}(y)-\rho\big)ds\Big)^{2}\Big]\ \leq\ C(\rho)N^{3/2}t^{3/2}.

Hence, the integral term in (11.1) is bounded by Cn2N3N3t3/2=Cn2Cn^{-2}N^{-3}N^{3}t^{3/2}=Cn^{-2} which vanishes as nn\uparrow\infty.

For the martingale term in (11.1), using orthogonality of martingales and η(x)1\eta(x)\leq 1, we obtain

𝔼νρ[(1nN3/2x=1N+1Mx1,x(N2t))2]\displaystyle\mathbb{E}_{\nu_{\rho}}\Big[\Big(\frac{1}{nN^{3/2}}\sum_{x=1}^{N+1}M_{x-1,x}(N^{2}t)\Big)^{2}\Big]
1n2N3x=1N+1𝔼νρ[Mx1,x2(N2t)]\displaystyle\ \ \ \leq\ \frac{1}{n^{2}N^{3}}\sum_{x=1}^{N+1}\mathbb{E}_{\nu_{\rho}}\big[M^{2}_{x-1,x}(N^{2}t)\big]
12n2N3x=1N+1𝔼νρ0N2t[η(x)(1η(x+1))+η(x+1)(1η(x))]𝑑s\displaystyle\ \ \ \leq\ \frac{1}{2n^{2}N^{3}}\sum_{x=1}^{N+1}\mathbb{E}_{\nu_{\rho}}\int_{0}^{N^{2}t}\big[\eta(x)(1-\eta(x+1))+\eta(x+1)(1-\eta(x))\big]ds
=O(n2)\displaystyle\ \ \ =\ O(n^{-2})

To conclude the proof. ∎

To complete the argument, we need to understand the limit fluctuation fields. This is the subject of the next subsection. In Subsection 11.2.2, we will complete the proof of Theorem 10.4.2.

11.2. Infinite dimensional Ornstein-Uhlenbeck process limit

We consider now the general d1d\geq 1 setting. Consider the space 𝔇=Cc(d){\mathfrak{D}}=C^{\infty}_{c}(\mathbb{R}^{d}), consisting of compactly supported, CC^{\infty} real functions on d\mathbb{R}^{d}. Its dual 𝔇{\mathfrak{D}}^{\prime} is the space of distributions, that is the continuous linear functionals acting on 𝔇{\mathfrak{D}}.

Recall the definition of WtN(G)W^{N}_{t}(G) in (11.1.1). To capture the evolution of WtN(G)W^{N}_{t}(G) for a fixed G𝔇G\in{\mathfrak{D}}, write, with respect to the finite-range symmetric exclusion generator LL (cf. (2.2.2)),

WtN(G)\displaystyle W^{N}_{t}(G) =\displaystyle= W0N(G)+N20tLWsN(G)𝑑s+tN(G)\displaystyle W^{N}_{0}(G)+N^{2}\int_{0}^{t}LW^{N}_{s}(G)ds+\mathcal{M}^{N}_{t}(G)

where, after the usual twice summation-by-parts under symmetry,

N2LWtN(G)=12Nd/2x,ydp(y)x,yNG(x/N)ηN2s(x)N^{2}LW^{N}_{t}(G)\ =\ \frac{1}{2N^{d/2}}\sum_{x,y\in\mathbb{Z}^{d}}p(y)\triangle^{N}_{x,y}G(x/N)\eta_{N^{2}s}(x)

and tN(G)\mathcal{M}^{N}_{t}(G) is a martingale such that

𝒩tN(G)=(tN(G))2N20t[L(WsN(G))22YsN(G)LWsN(G)]𝑑s{{\mathcal{N}}}^{N}_{t}(G)\ =\ (\mathcal{M}^{N}_{t}(G))^{2}-N^{2}\int_{0}^{t}\big[L(W^{N}_{s}(G))^{2}-2Y^{N}_{s}(G)LW^{N}_{s}(G)\big]ds

is a martingale. The last integral in the display, the quadratic variation of tN(G)\mathcal{M}^{N}_{t}(G), can be evaluated as

N(G)t=N20t[L(WsN(G))22YsN(G)LWsN(G)]𝑑s\displaystyle\big\langle\mathcal{M}^{N}(G)\big\rangle_{t}\ =\ N^{2}\int_{0}^{t}\big[L(W^{N}_{s}(G))^{2}-2Y^{N}_{s}(G)LW^{N}_{s}(G)\big]ds
=1Nd0txdp(y)[x,yNG(x/N)]2ηN2s(x)(1ηN2s(x+y))𝑑s.\displaystyle\ \ \ =\ \frac{1}{N^{d}}\int_{0}^{t}\sum_{x\in\mathbb{Z}^{d}}p(y)[\nabla^{N}_{x,y}G(x/N)]^{2}\eta_{N^{2}s}(x)(1-\eta_{N^{2}s}(x+y))ds.

Here, similar to the hydrodynamics calculations (cf. Subsection 2.4), x,yN=N[G((x+y)/N)G(x/N)]\nabla^{N}_{x,y}=N\big[G((x+y)/N)-G(x/N)\big] and x,yNG=N2[G((x+y)/N)2G(x/N)+G((xy)/N)]\triangle^{N}_{x,y}G=N^{2}\big[G((x+y)/N)-2G(x/N)+G((x-y)/N)\big] are the scaled discrete gradient and Laplacian.

Since xp(y)x,yNG(x/N)=0\sum_{x}p(y)\triangle^{N}_{x,y}G(x/N)=0, we may subtract ρ\rho and write

WtN(G)=W0N(G)+120tWsN(yp(y),yNG(/N))ds+tN(G)and\displaystyle W^{N}_{t}(G)=W^{N}_{0}(G)+\frac{1}{2}\int_{0}^{t}W^{N}_{s}\Big(\sum_{y}p(y)\triangle^{N}_{\cdot,y}G(\cdot/N)\Big)ds+\mathcal{M}^{N}_{t}(G)\ \ \ \ \ {\rm and} (11.2.1)
𝒩tN(G)\displaystyle{{\mathcal{N}}}^{N}_{t}(G)
=(tN(G))21Nd0tx,ydp(y)[x,yNG(x/N)]2ηN2s(x)(1ηN2s(x+y))𝑑s.\displaystyle\ =\big(\mathcal{M}^{N}_{t}(G)\big)^{2}-\frac{1}{N^{d}}\int_{0}^{t}\sum_{x,y\in\mathbb{Z}^{d}}p(y)\big[\nabla^{N}_{x,y}G(x/N)\big]^{2}\eta_{N^{2}s}(x)\big(1-\eta_{N^{2}s}(x+y)\big)ds.

Now, as before with respect to the hydrodynamics, we have two steps:

Step 1: Show tightness of {WtN:t[0,T]}N1\{W^{N}_{t}:t\in[0,T]\}_{N\geq 1} in an appropriate space, and continuity of limit trajectories under limit points.

Step 2: Identify the limit points in terms of a unique ‘infinite dimensional Ornstein-Uhlenbeck’ process.

Putting it together, we will arrive at the following informal description: WtNW^{N}_{t} converges to WtW_{t} which solves, in the nearest-neighbor symmetric setting,

dYt=12dWtdt+d1ρ(1ρ)dt,dY_{t}\ =\ \frac{1}{2d}\triangle W_{t}dt+\sqrt{d^{-1}\rho(1-\rho)}\nabla d\mathcal{B}_{t}, (11.2.2)

more explained in the following subsections.

Spaces

A natural space will be D([0,T],𝔇)D([0,T],{{\mathfrak{D}}}^{\prime}), the distribution valued right-continuous with left limits trajectories on 𝔇{{\mathfrak{D}}}, with the strong dual topology.

We remark there are other natural spaces one could consider. For instance, WtNW^{N}_{t} could act on the Schwartz space of rapidly decreasing functions 𝒮{\mathcal{S}}, in which case WtNW^{N}_{t} would be a member of 𝒮{\mathcal{S}}^{\prime}, the space of ‘tempered distributions.’ One could work also with the Hermite basis based k{\mathcal{H}}_{k} spaces containing 𝒮{\mathcal{S}}. Then, WtNW^{N}_{t} would be a member of k𝒮{\mathcal{H}}_{-k}\subset{\mathcal{S}}^{\prime}. In another direction, we could have also specified the lattice as 𝕋Nd{\mathbb{T}}_{N}^{d}, instead of d\mathbb{Z}^{d}. See Chapter 11 [130] for instance where spaces k{\mathcal{H}}_{-k} with respect to 𝕋Nd{\mathbb{T}}_{N}^{d} are used; on d\mathbb{R}^{d}, the Hermite spaces would use definitions in [177][p. 142].

Both 𝒮{\mathcal{S}}^{\prime} and k{\mathcal{H}}_{-k} are nuclear, Frechét spaces, whereas the space of distributions 𝔇{\mathfrak{D}}^{\prime} is a ‘strict inductive limit’ of nuclear Frechét spaces. Importantly, in each of these spaces, tightness of {WtN:t[0,T]}\{W^{N}_{t}:t\in[0,T]\} is implied by tightness of {WtN(G):t[0,T]}\{W^{N}_{t}(G):t\in[0,T]\} for each GG in 𝒮{\mathcal{S}}^{\prime}, k{\mathcal{H}}_{-k}, or 𝒟{\mathcal{D}}^{\prime}; see [77], [78], [160] for more discussion.

11.2.1. A precise statement of (11.2.2)

Let QNQ_{N} be the probability measure on D([0,T],𝔇)D([0,T],{\mathfrak{D}}^{\prime}) governing {WtN:t[0,T]}\{W^{N}_{t}:t\in[0,T]\}, when the underlying nearest-neighbor, symmetric exclusion process starts from invariant measure νρ\nu_{\rho}.

Theorem 11.2.1.

We have QNQ_{N} converges to QQ, concentrated on C([0,T],𝔇)C([0,T],{\mathfrak{D}}^{\prime}), governing a Gaussian Markov random field with mean 00 and covariance,

EQ[Ws(G)Wt(H)]\displaystyle E_{Q}[W_{s}(G)W_{t}(H)]
=ρ(1ρ)(2πd1(ts))d/2ddG(v)H(u)exp{d|uv|22(ts)}𝑑u𝑑v\displaystyle\ =\ \frac{\rho(1-\rho)}{(2\pi d^{-1}(t-s))^{d/2}}\int_{\mathbb{R}^{d}}\int_{\mathbb{R}^{d}}G(v)H(u)\exp\Big\{-\frac{d|u-v|^{2}}{2(t-s)}\Big\}dudv

for all 0st0\leq s\leq t, G,H𝔇G,H\in{\mathfrak{D}}.

The process WtW_{t} governed by QQ is sometimes called a ‘generalized Ornstein-Uhlenbeck process’, as discussed in Holley-Stroock [112]. The scalings and the limit in Theorem 11.2.1, where space is scaled by 1/N1/N, time by v(N)=N2v(N)=N^{2} and the empirical measure by 1/N1/\sqrt{N}, are sometimes referred to as a ‘Edwards-Wilkinson’ fluctuation limit.

Holley-Stroock martingale problem

The existence/uniqueness of QQ in Theorem 11.2.1 follows from a ‘martingale problem’ characterization.

Let U=(2d)1U=(2d)^{-1}\triangle be the nonnegative self-adjoint operator defined on domain L2(d)L^{2}(\mathbb{R}^{d}) and let TtT_{t} be the associated heat semigroup. Define B=d1ρ(1ρ)B=\sqrt{d^{-1}\rho(1-\rho)}\nabla to be the linear gradient operator. Let also t\mathcal{F}_{t} be the sigma-field in D([0,T],𝔇)D([0,T],{\mathfrak{D}}) generated by a process Ws(H)W_{s}(H) for sts\leq t and H𝔇H\in{\mathfrak{D}}.

Theorem 11.2.2.

Suppose QQ is a probability measure governing WtW_{t}, concentrating on C([0,T],𝔇)C([0,T],{\mathfrak{D}}^{\prime}), and for each H𝔇H\in{\mathfrak{D}},

MtU,H=Wt(H)W0(H)0tWs(UH)𝑑sM_{t}^{U,H}\ =\ W_{t}(H)-W_{0}(H)-\int_{0}^{t}W_{s}(UH)ds

and

NtU,H=(MtU,H)2BHL22tN^{U,H}_{t}\ =\ (M_{t}^{U,H})^{2}-\|BH\|^{2}_{L^{2}}t

are L1(Q)L^{1}(Q), t\mathcal{F}_{t}-martingales. Then, for all 0s<t0\leq s<t, and subsets AdA\subset\mathbb{R}^{d}, QQ a.s.,

Q[Wt(H)A|s]\displaystyle Q\Big[W_{t}(H)\in A|\mathcal{F}_{s}\big] (11.2.3)
=A12π0tsBTrHL22𝑑rexp{|yWs(TtsH)|220tsBTrHL22𝑑r}𝑑y.\displaystyle\ \ =\ \int_{A}\frac{1}{\sqrt{2\pi\int_{0}^{t-s}\|BT_{r}H\|^{2}_{L^{2}}dr}}\exp\Big\{\frac{-|y-W_{s}(T_{t-s}H)|^{2}}{2\int_{0}^{t-s}\|BT_{r}H\|^{2}_{L^{2}}dr}\Big\}dy.

Therefore, the finite-dimensional distributions of QQ, and hence the measure QQ on C([0,T],𝔇)C([0,T],{\mathfrak{D}}), are determined by its restriction to 0\mathcal{F}_{0}.

We refer to the work of Holley-Stroock [112] for more details; see also Chapter 11 [130].

Sketch of proof of Theorem 11.2.1

Assuming Steps 1,2, we outline the proof of Theorem 11.2.1. In our context, the restriction to 0\mathcal{F}_{0} is already known: Under the invariant measure νρ\nu_{\rho}, we have W0NW^{N}_{0} converges to a Gaussian field with mean zero and covariance

EQ[W0(G)W0(H)]=ρ(1ρ)G,HL2.E_{Q}[W_{0}(G)W_{0}(H)]\ =\ \rho(1-\rho)\langle G,H\rangle_{L^{2}}. (11.2.4)
Exercise 11.2.3.

Show that the joint distribution of W0N(H1),,W0N(H)W^{N}_{0}(H_{1}),\ldots,W^{N}_{0}(H_{\ell}) is Gaussian with covariance given via (11.2.4). One can use the Cramér-Wold device.

Also, from the martingale property in Theorem 11.2.2, the formula (11.2.3), and that ddtTt=TtU\frac{d}{dt}T_{t}=T_{t}U, we can argue

EQ[Ws(G)Wt(H)]\displaystyle E_{Q}[W_{s}(G)W_{t}(H)] =\displaystyle= EQ[Ws(G)(MtU,HMsU,H)]\displaystyle E_{Q}\big[W_{s}(G)(M_{t}^{U,H}-M_{s}^{U,H})\big] (11.2.5)
+stEQ[Ws(G)Wu(UH)]du+EQ[Ws(G)Ws(H)]\displaystyle\ \ \ \ +\int_{s}^{t}E_{Q}\big[W_{s}(G)W_{u}(UH)\big]du+E_{Q}\big[W_{s}(G)W_{s}(H)\big]
=\displaystyle= EQ[Ws(G)Ws(TtsH)]=EQ[W0(G)W0(TtsH)].\displaystyle E_{Q}\big[W_{s}(G)W_{s}(T_{t-s}H)\big]\ =\ E_{Q}\big[W_{0}(G)W_{0}(T_{t-s}H)\big].

This covariance is exactly what is given in Theorem 11.2.1.

Now, since t(H)=BHL21MtU,H\mathcal{B}_{t}(H)=\|BH\|^{-1}_{L^{2}}M_{t}^{U,H} is a continuous martingale with quadratic variation tt, by Levy’s characterization, we have that t(H)\mathcal{B}_{t}(H) is distributed as a Brownian motion. Hence, we have

Wt(H)=W0(H)+0tWs(UH)𝑑s+BHL2t(H)W_{t}(H)\ =\ W_{0}(H)+\int_{0}^{t}W_{s}(UH)ds+\|BH\|_{L^{2}}\mathcal{B}_{t}(H) (11.2.6)

where t\mathcal{B}_{t} is the infinite dimensional Brownian motion (Gaussian Markov random field) with covariance

EQ[s(G)t(H)]=(min{s,t})dG(u)GL2H(u)HL2𝑑u.E_{Q}[\mathcal{B}_{s}(G)\mathcal{B}_{t}(H)]\ =\ (\min\{s,t\})\int_{\mathbb{R}^{d}}\frac{\nabla G(u)}{\|\nabla G\|_{L^{2}}}\frac{\nabla H(u)}{\|\nabla H\|_{L^{2}}}du.

In this way, (11.2.6) gives a meaning to the integral form of (11.2.2).

Exercise 11.2.4.

Use polarization with the martingales MsU,GM^{U,G}_{s} and MtU,HM^{U,H}_{t} to show the formula in the last display.

What remains in the proof of Theorem 11.2.1 is to show Steps 1,2 from which one may conclude that QNQ_{N} converges to a QQ, supported on continuous trajectories, satisfying the ‘martingale problem’ conditions in Theorem 11.2.2. This is done in Subsection 11.3.

11.2.2. Application: Proof of Theorem 10.4.2

We return to our motivating example with respect to current fluctuations. By (11.1.2) and Lemma 11.1.2, since N1/2J1,0(N2t)N^{-1/2}J_{-1,0}(N^{2}t) does not depend on nn, we have uniformly in N1N\geq 1 that

{WtN(Gn)+W0N(Gn):n1}\{W^{N}_{t}(G_{n})+W^{N}_{0}(G_{n}):n\geq 1\}

is a Cauchy sequence in L2(νρ)L^{2}(\nu_{\rho}). Note, by stationarity, that

supN1𝔼νρ[(WtN(H))2]2HL2(d)2.\sup_{N\geq 1}\mathbb{E}_{\nu_{\rho}}\big[\big(W^{N}_{t}(H)\big)^{2}\big]\leq 2\|H\|^{2}_{L^{2}(\mathbb{R}^{d})}.

Then, by Theorem 11.2.1, approximating GnG_{n} by smooth compactly supported functions, we have for fixed nn as NN\uparrow\infty that

WtN(Gn)W0N(Gn)Wt(Gn)W0(Gn).W^{N}_{t}(G_{n})-W_{0}^{N}(G_{n})\ \Rightarrow\ W_{t}(G_{n})-W_{0}(G_{n}).

Since {Wt(Gn)W0(Gn):n1}\{W_{t}(G_{n})-W_{0}(G_{n}):n\geq 1\} is Cauchy in L2(νρ)L^{2}(\nu_{\rho}), we denote its limit by Wt(H0)W0(H0)W_{t}(H_{0})-W_{0}(H_{0}), whose distribution is a mean-zero Gaussian.

In particular,

1NJ1,0(N2t)Wt(H0)W0(H0).\frac{1}{\sqrt{N}}J_{-1,0}(N^{2}t)\ \Rightarrow\ W_{t}(H_{0})-W_{0}(H_{0}).

By Lemma 11.1.2, one may identify the limiting variance by computing

limnlimNVar(N1/2J1,0(N2t))=limnlimN𝔼νρ[(WtN(Gn)W0N(Gn))2].\displaystyle\lim_{n\uparrow\infty}\lim_{N\uparrow\infty}{\rm Var}\big(N^{-1/2}J_{-1,0}(N^{2}t)\big)=\lim_{n\uparrow\infty}\lim_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho}}\Big[\big(W^{N}_{t}(G_{n})-W^{N}_{0}(G_{n})\big)^{2}\Big]. (11.2.7)
Exercise 11.2.5.

Use duality, that is 𝔼νρ[(ηN2t(x)ρ)(η0(y)ρ)]=ρ(1ρ)PN2t(0,yx)=ρ(1ρ)P(ZN2t=yx)\mathbb{E}_{\nu_{\rho}}[(\eta_{N^{2}t}(x)-\rho)(\eta_{0}(y)-\rho)]=\rho(1-\rho)P_{N^{2}t}(0,y-x)=\rho(1-\rho)P\big(Z_{N^{2}t}=y-x\big), where ZZ_{\cdot} is a continuous-time simple symmetric random walk starting at 00 (cf. Subsection 9.2.1), to verify that the variance (11.2.7) with t=1t=1 equals 2/πρ(1ρ)\sqrt{2/\pi}\rho(1-\rho). Hint: To analyze the cross term, weak convergence ZN2/NN(0,1)Z_{N^{2}}/N\Rightarrow{\rm N}(0,1) may be useful.

11.3. Proof of Steps 1,2: Tightness and identification

We first restate Steps 1, 2 given informally before (11.2.2) in the setting of nearest-neighbor symmetric exclusion.

Step 1: Show tightness of {QN}N1\{Q_{N}\}_{N\geq 1} governing {WtN:t[0,T]}N1\{W^{N}_{t}:t\in[0,T]\}_{N\geq 1}, members in D([0,T],𝔇)D([0,T],{\mathfrak{D}}^{\prime}), in the uniform topology of C([0,T],𝔇)C([0,T],{\mathfrak{D}}^{\prime}). Hence, trajectories under limit points QQ will be continuous.

Step 2: Identify the limit points QQ in terms of the unique ‘infinite dimensional Ornstein-Uhlenbeck’ process given in Theorem 11.2.1.

In the following, recall that pp is nearest-neighbor, symmetric and translation-invariant.

11.3.1. Moments of tN(H)\mathcal{M}^{N}_{t}(H)

Recall the martingales tN(H)\mathcal{M}^{N}_{t}(H) and 𝒩tN(H){\mathcal{N}}^{N}_{t}(H) specified in (11.2.1). Before going to the proofs of Steps 1,2, we record some moment estimates of tN(H)\mathcal{M}^{N}_{t}(H) for H𝔇H\in{\mathfrak{D}}.

By taking expectation of the quadratic variation, we obtain

𝔼νρ[(tN(H))2]=ρ(1ρ)TNdx,ydp(y)[x,yNH(x/N)]2C(ρ,T)HL2(d)2.\displaystyle\mathbb{E}_{\nu_{\rho}}\big[(\mathcal{M}^{N}_{t}(H))^{2}\big]=\frac{\rho(1-\rho)T}{N^{d}}\sum_{x,y\in\mathbb{Z}^{d}}p(y)\big[\nabla^{N}_{x,y}H(x/N)\big]^{2}\leq C(\rho,T)\|\nabla H\|^{2}_{L^{2}(\mathbb{R}^{d})}. (11.3.1)

To bound the fourth moment, we will take the following approach. Other arguments, via Burkholder-Gundy-Davis inequalities may also be used.

Lemma 11.3.1.

For all local functions FF, s,t[0,T]s,t\in[0,T], and λ\lambda\in\mathbb{R}, we have

Zs,tλ=exp{λF(ηt)λF(ηs)steλF(ηu)LeλF(ηu)𝑑u}Z^{\lambda}_{s,t}\ =\ \exp\Big\{\lambda F(\eta_{t})-\lambda F(\eta_{s})-\int_{s}^{t}e^{-\lambda F(\eta_{u})}Le^{\lambda F(\eta_{u})}du\Big\}

is a martingale.

Proof.

The lemma is a type of ‘Girsanov’ formula. See [66][around p. 175] which shows Zs,tZ_{s,t} is a local martingale. Since we are dealing with the exclusion process, where occupation numbers are bounded, it is integrable and so a martingale. ∎

Lemma 11.3.2.

For H𝔇H\in{\mathfrak{D}}, and t[0,T]t\in[0,T], we have

𝔼νρ[(tN(H))4]C(H)(t2+Nd2t).\mathbb{E}_{\nu_{\rho}}\big[\big(\mathcal{M}^{N}_{t}(H)\big)^{4}\big]\ \leq\ C(H)\big(t^{2}+N^{-d-2}t\big).
Proof.

Let ZN2s,N2tλZ^{\lambda}_{N^{2}s,N^{2}t} be the martingale with

F(η)=Nd/2xH(x/N)(η(x)ρ).F(\eta)=N^{-d/2}\sum_{x}H(x/N)\big(\eta(x)-\rho\big).

By explicit calculation,

eλF(ηN2u)(N2L)eλF(ηN2u)\displaystyle e^{-\lambda F(\eta_{N^{2}u})}(N^{2}L)e^{\lambda F(\eta_{N^{2}u})}
=N2x,yp(yx)[eλNd/2[H(y/N)H(x/N)]1]ηN2u(x)(1ηN2u).\displaystyle\quad\quad=\ N^{2}\sum_{x,y}p(y-x)\big[e^{\lambda N^{-d/2}[H(y/N)-H(x/N)]}-1\big]\eta_{N^{2}u}(x)\big(1-\eta_{N^{2}u}\big).

Morevoer,

𝔼νρ[ZN2s,N2tλ]= 1.\mathbb{E}_{\nu_{\rho}}\big[Z^{\lambda}_{N^{2}s,N^{2}t}\big]\ =\ 1. (11.3.2)

Now, we may expand the left-hand side and equate in powers of λ\lambda. By symmetry of pp, we evaluate (11.3.2) as

𝔼νρ[exp{λMtN(H))\displaystyle\mathbb{E}_{\nu_{\rho}}\Big[\exp\Big\{\lambda M^{N}_{t}(H)\big)
λ2N22Nd0tx,yp(yx)(H(y/N)H(x/N))2ηN2u(x)(1ηN2u(y))du\displaystyle\ \ \ -\frac{\lambda^{2}N^{2}}{2N^{d}}\int_{0}^{t}\sum_{x,y}p(y-x)\big(H(y/N)-H(x/N)\big)^{2}\eta_{N^{2}u}(x)\big(1-\eta_{N^{2}u}(y)\big)du
+λ30t1ds+λ40t2ds+λ50t4ds}]= 1.\displaystyle\ \ \ \ \ \ +\lambda^{3}\int_{0}^{t}{\mathcal{R}}^{1}ds+\lambda^{4}\int_{0}^{t}{\mathcal{R}}^{2}ds+\lambda^{5}\int_{0}^{t}{\mathcal{R}}^{4}ds\Big\}\Big]\ =\ 1.

It is not difficult now, although a long calculation, to estimate {i}i=13\{{\mathcal{R}}^{i}\}_{i=1}^{3} and obtain the desired statement. Note that by matching λ2\lambda^{2} terms, one recovers (11.3.1) for instance. ∎

Exercise 11.3.3.

Make the computation in the proof of the above lemma to match fourth powers of λ\lambda to obtain the lemma statement.

11.3.2. Proof of Step 2, given Step 1

We will apply results in the limit theory of martingales in the context of symmetric simple exclusion. References in this vein include [66], [116], [216], among others.

Suppose QQ is a limit point found with respect to the uniform topology of {QN}N1\{Q_{N}\}_{N\geq 1}, necessarily supported on continuous 𝔇{\mathfrak{D}}^{\prime}-valued trajectories. We will identify the subsequence by {N:N1}\{N:N\geq 1\} itself to streamline notation.

We now show that MtU,HM_{t}^{U,H} and NtU,HN^{U,H}_{t} are L1(Q)L^{1}(Q) martingales, and thereby identify QQ via Theorem 11.2.2.

Consider the formula for tN(G)\mathcal{M}^{N}_{t}(G) in (11.2.1). Given Step 1 and that the function w(H)wt(H)w0(H)(1/2)0tws(yp(y),yNH(/N))dsw_{\cdot}(H)\mapsto w_{t}(H)-w_{0}(H)-(1/2)\int_{0}^{t}w_{s}\big(\sum_{y}p(y)\triangle^{N}_{\cdot,y}H(\cdot/N)\big)ds is continuous in the uniform topology, the term tN(G)\mathcal{M}^{N}_{t}(G) would converge in distribution to a limit

MtU,H:=Wt(H)W0(H)12d0tWs(H)𝑑s.M^{U,H}_{t}:=W_{t}(H)-W_{0}(H)-\frac{1}{2d}\int_{0}^{t}W_{s}(\triangle H)ds.

Observe, by (11.3.1), that supN1𝔼νρ[(tN(H))2]<\sup_{N\geq 1}\mathbb{E}_{\nu_{\rho}}\big[\big(\mathcal{M}^{N}_{t}(H)\big)^{2}\big]<\infty. Therefore, we conclude {tN(H)}N1\{\mathcal{M}^{N}_{t}(H)\}_{N\geq 1} is uniformly integrable for each t[0,T]t\in[0,T]. Since the martingales tN(H)MtU,H\mathcal{M}^{N}_{t}(H)\Rightarrow M^{U,H}_{t}, we conclude the limit MtU,HM^{U,H}_{t} is an L2(Q)L^{2}(Q) martingale by Theorem IX.1.12 in [116].

Also, as

𝔼νρ[{1Nd0tx,ydp(y)(x,yNH(x/N))2\displaystyle\mathbb{E}_{\nu_{\rho}}\Big[\Big\{\frac{1}{N^{d}}\int_{0}^{t}\sum_{x,y\in\mathbb{Z}^{d}}p(y)\big(\nabla^{N}_{x,y}H(x/N)\big)^{2} (11.3.3)
(ηN2s(x)(1ηN2s(x+y))ρ(1ρ))ds}2]C(ρ)tNdHL2(d)2,\displaystyle\quad\quad\cdot\Big(\eta_{N^{2}s}(x)\big(1-\eta_{N^{2}s}(x+y)\big)-\rho(1-\rho)\Big)ds\Big\}^{2}\Big]\ \leq\ \frac{C(\rho)t}{N^{d}}\|\nabla H\|^{2}_{L^{2}(\mathbb{R}^{d})},

we have N(H)t\langle\mathcal{M}^{N}(H)\rangle_{t} converges to ρ(1ρ)tHL2(d)2\rho(1-\rho)t\|\nabla H\|^{2}_{L^{2}(\mathbb{R}^{d})} in probability.

By the continuous mapping theorem, (tN(H))2(MtU,H)2\big(\mathcal{M}^{N}_{t}(H)\big)^{2}\Rightarrow\big(M^{U,H}_{t}\big)^{2}. Moreover, by the convergence in probability implied by (11.3.3), we observe (tN(H))2N(H)t(MtU,H)2ρ(1ρ)tHL2(d)2=:NtU,H\big(\mathcal{M}^{N}_{t}(H)\big)^{2}-\langle\mathcal{M}^{N}(H)\rangle_{t}\Rightarrow\big(M^{U,H}_{t}\big)^{2}-\rho(1-\rho)t\|\nabla H\|^{2}_{L^{2}(\mathbb{R}^{d})}=:N^{U,H}_{t}. To see that the limit NtU,HN^{U,H}_{t} is an L1(Q)L^{1}(Q) martingale, we observe {(tN(H))2N(H)t:N1}\big\{\big(\mathcal{M}^{N}_{t}(H)\big)^{2}-\langle\mathcal{M}^{N}(H)\rangle_{t}:N\geq 1\big\} is uniformly integrable by the fourth moment estimate Lemma 11.3.2. Hence, as desired NtU,HN^{U,H}_{t} is a martingale, again by Theorem IX.1.12 in [116].

11.3.3. Proof of Step 1

To show tightness of {QN}\{Q_{N}\} with respect to the uniform topology, as 𝔇{\mathfrak{D}} is the ‘inductive limit’ of nuclear Frechét spaces, it is sufficient to verify tightness of {WtN(H):N1}\{W^{N}_{t}(H):N\geq 1\} for each H𝔇H\in{\mathfrak{D}}; see [78].

We remark, as in the study of hydrodynamics, tightness with respect to uniform topology implies that in the Skorohod topology. We have therefore the following tightness criterion. Denote the uniform modulus of continuity by

wW(δ)=sups,t[0,T]|ts|δ|WtWs|.w_{W}(\delta)\ =\ \sup_{\stackrel{{\scriptstyle|t-s|\leq\delta}}{{s,t\in[0,T]}}}|W_{t}-W_{s}|.
Lemma 11.3.4.

A family of probability measures {QN}\{Q_{N}\} on D([0,T],𝔇)D([0,T],{\mathfrak{D}}^{\prime}) is tight if for each H𝔇H\in{\mathfrak{D}},

  • (a)

    limAlimNQN[|W0N(H)|>A]= 0\lim_{A\uparrow\infty}\lim_{N\uparrow\infty}Q_{N}\big[|W^{N}_{0}(H)|>A\big]\ =\ 0 and,

  • (b)

    for all ϵ>0\epsilon>0, limδ0limNQN[wWN(H)(δ)ϵ]= 0\lim_{\delta\downarrow 0}\lim_{N\uparrow\infty}Q_{N}\big[w_{W^{N}(H)}(\delta)\geq\epsilon\big]\ =\ 0.

Proof.

Prelimit, we have

WtN(H)\displaystyle W^{N}_{t}(H) =tN(H)+W0N(H)\displaystyle=\mathcal{M}^{N}_{t}(H)+W^{N}_{0}(H) (11.3.4)
+12Nd/20tx,yp(y)(x,yNH)(x/N)(ηN2s(x)ρ)ds.\displaystyle\quad+\frac{1}{2N^{d/2}}\int_{0}^{t}\sum_{x,y}p(y)(\triangle^{N}_{x,y}H)(x/N)(\eta_{N^{2}s}(x)-\rho)ds.

We need to show each of these terms satisfies the criteria.

The term W0N(H)W^{N}_{0}(H). The mean square, starting from the invariant measure νρ\nu_{\rho}, is bounded in the limit by 2ρ(1ρ)HL2(d)22\rho(1-\rho)\|H\|^{2}_{L^{2}(\mathbb{R}^{d})}, and hence item (a) holds. Part (b) holds trivially.

The integral term. Part (a) holds trivially. For item (b), by Chebychev and Schwarz inequalities, we may bound

QN[sups,t[0,T]|ts|δ|st12Nd/2x,yp(y)(x,yNG)(x/N)(ηN2u(x)ρ)du|>ϵ]\displaystyle Q_{N}\Big[\sup_{\stackrel{{\scriptstyle|t-s|\leq\delta}}{{s,t\in[0,T]}}}\Big|\int_{s}^{t}\frac{1}{2N^{d/2}}\sum_{x,y}p(y)\big(\triangle^{N}_{x,y}G\big)(x/N)(\eta_{N^{2}u}(x)-\rho)du\Big|>\epsilon\Big]
δϵ20TEQN[(12Nd/2x,yp(y)(x,yNG)(x/N)(ηN2u(x)ρ))2]𝑑u.\displaystyle\quad\leq\frac{\delta}{\epsilon^{2}}\int_{0}^{T}E_{Q_{N}}\Big[\Big(\frac{1}{2N^{d/2}}\sum_{x,y}p(y)\big(\triangle^{N}_{x,y}G\big)(x/N)(\eta_{N^{2}u}(x)-\rho)\Big)^{2}\Big]du.

Starting from νρ\nu_{\rho}, the last quantity is bounded by 2d1ρ(1ρ)Tδϵ2GL2(d)22d^{-1}\rho(1-\rho)T\delta\epsilon^{-2}\|\triangle G\|_{L^{2}(\mathbb{R}^{d})}^{2}, which vanishes as δ0\delta\downarrow 0.

The term tN(H)\mathcal{M}^{N}_{t}(H). Part (a) holds trivially. For item (b), We employ the standard ‘three ϵ\epsilon argument, dividing the interval [0,T][0,T] into O(T/δ)O(T/\delta) subintervals (a similar scheme was used in Subsection 3.3). Noting when s,ts,t belong to a single subinterval or are in adjacent ones, we may bound

sup|ts|δ|tN(hz)sN(hz)|maxsuptIii 3|tN(hz)tiN(hz)|\sup_{|t-s|\leq\delta}|\mathcal{M}^{N}_{t}(h_{z})-\mathcal{M}^{N}_{s}(h_{z})|\leq\max_{i}\sup_{t\in I_{i}}\ 3|\mathcal{M}^{N}_{t}(h_{z})-\mathcal{M}^{N}_{t_{i}}(h_{z})|

where the max is over the subintervals {Ii}\{I_{i}\} and tit_{i} is the left endpoint of the iith one. Then, by stationarity, Chebychev and Doob’s inequality and Lemma 11.3.2,

QN[supt,s[0,T]|ts|δ|tN(H)sN(H)|>ϵ]\displaystyle Q_{N}\Big[\sup_{\stackrel{{\scriptstyle|t-s|\leq\delta}}{{t,s\in[0,T]}}}|\mathcal{M}^{N}_{t}(H)-\mathcal{M}^{N}_{s}(H)|>\epsilon\Big]
iQN[suptIi|tN(H)tiN(H)|>ϵ/3]\displaystyle\quad\leq\sum_{i}Q_{N}\Big[\sup_{t\in I_{i}}|\mathcal{M}^{N}_{t}(H)-\mathcal{M}^{N}_{t_{i}}(H)|>\epsilon/3\Big]
iC(ϵ/3)4EQN[(δN(H))4]C(H)|Tδ[δ2+δ/Nd+1].\displaystyle\quad\leq\sum_{i}\frac{C}{(\epsilon/3)^{4}}E_{Q_{N}}\Big[\big(\mathcal{M}^{N}_{\delta}(H)\big)^{4}\Big]\ \leq\ \frac{C(H)|T}{\delta}\cdot\big[\delta^{2}+{\delta}/{N^{d+1}}\big].

The right-hand side of the display vanishes as NN\uparrow\infty and δ0\delta\downarrow 0. ∎

11.4. Notes

The proof given here for the current fluctuations Theorem 10.4.2 follows [118], and the idea of truncation goes back to [183].

We comment, with respect to equilibrium fluctuations, in the context of symmetric exclusion models, as for the hydrodynamic limit, there is no ‘replacement’ estimate needed; see also the treatment in [130]. The theory of generalized Ornstein Uhlenbeck processes originates in [112].

Recently, a proof of fluctuations starting from ‘flat’ states via ‘discrete regularity structures’ has been given in symmetric exclusion [113].

‘Nonequilibrium’ fluctuations have also been shown in symmetric exclusion [175]. In asymmetric models, fluctuations starting from an invariant measure are also known in d3d\geq 3 [42].

11.4.1. KPZ etc.

In d=1d=1, for the nearest-neighbor asymmetric process, including TASEP, there are many works describing the behaviors of currents, ‘height’ functions, and fluctuation fields starting from an invariant measure and other initial conditions. Instead of a generalized OU process, under time scaling v(N)=N3/2v(N)=N^{3/2}, space scaling 1/N1/N, and say scaling 1/N1/\sqrt{N} of the ‘height’ functions, the limits are different, those with respect to a ‘KPZ’ (Kardar-Parisi-Zhang) fixed point (cf. [158]).

On the other hand, if the asymmetry is weak in the sense the drift of the transition probability is O(1/N)O(1/\sqrt{N}), under diffusive time/space scaling, the limit of certain translated fluctuation fields solves a ‘stochastic Burgers’ or sometimes called ‘KPZ-Burgers’ equation.

These limits connect with integrable probability, last passage percolation and the ‘Directed Landscape’, polymers, singular KPZ SPDE, and random matrices. See [4], [11], [25], [51], [55], [56], [97], [98], [103], [99], [104], [105], [107], [115], [125], [153], [171], [207], [219], [220] for reviews and discussion, among other references.

In d2d\geq 2, the work [39] on scaled continuum stochastic Burgers equation shows Gaussian fluctuations. In d=2d=2, Gaussian behaviors have been shown with respect to scaled ‘subcritical’ continuum KPZ equations [44], [40], [102]. In d3d\geq 3, Gaussian behaviors have been seen starting from asymmetric exclusion [141]. As mentioned in [39], in d=2d=2, it is open to see such behavior starting from asymmetric exclusion, or other particle systems.

In d=1d=1, the fluctuation fields of many-component systems of particles, and coupled SPDE’s including coupled stochastic Burgers equations have been considered, although many open problems remain; see [38], [19], [82], [170], [184], [185], [188], [208] and references therein.

Section 12 Boltzmann-Gibbs principle for symmetric zero-range processes

We discuss the equilibrium fluctuations of dd-dimensional symmetric finite-range zero-range processes, that is the scaling limit of the empirical mass fluctuation field, starting from an invariant measure νρ\nu_{\rho}. Unlike for symmetric exclusion models, a ‘replacement’ at the fluctuation level must be made in order to identify the limit field as a generalized OU process. This replacement, sometimes called the ‘Boltzmann-Gibbs’ principle, is of its own interest. The proof we give makes use of a ‘spectral gap’ estimate.

12.1. Statement of equilibrium fluctuations

Recall, from Sections 4 and 7, that the rate function g:0+g:\mathbb{N}_{0}\rightarrow\mathbb{R}_{+} and the jump probability p()p(\cdot) define the zero-range process with generator

Lf(η)=x,ydp(y)g(η(x))[f(ηx,x+y)f(η)].Lf(\eta)=\sum_{x,y\in\mathbb{Z}^{d}}p(y)g(\eta(x))\big[f(\eta^{x,x+y})-f(\eta)\big].

To reduce notation, we will assume that pp is symmetric, translation-invariant, and nearest-neighbor: p(±ei)=1/(2d)p(\pm e_{i})=1/(2d) for the standard basis {ei}i=1d\{e_{i}\}_{i=1}^{d}. Also, we remind that gg satisfies g(0)=0g(0)=0, g(k)>0g(k)>0 for k1k\geq 1. We will also impose the following.

  • (Lip)

    |g(k+1)g(k)|a0|g(k+1)-g(k)|\leq a_{0} for all k0k\geq 0.

  • (M)

    There exists k0k_{0} and ϵ0>0\epsilon_{0}>0 such that g(k+k+0)g(k)ϵ0g(k+k+0)-g(k)\geq\epsilon_{0} for all k0k\geq 0.

The first assumption is something we have already seen in the construction of the process on d\mathbb{Z}^{d} in Section 7, which includes the independent particle process when g(k)kg(k)\equiv k. The second assures a uniform ‘spectral gap’ that will be discussed later in Subsection 12.4.

We will also fix an invariant measure νρ=xdκΨ(ρ)\nu_{\rho}=\prod_{x\in\mathbb{Z}^{d}}\kappa_{\Psi(\rho)}, a product of ‘Poisson’ like marginals, and the process will be assumed to begin under this extremal invariant measure. We will assume the process is an L2(νρ)L^{2}(\nu_{\rho}) process on d\mathbb{Z}^{d}. Recall Section 8 for specifications and details. There is no difficulty in assuming if preferred that the process is on the torus 𝕋Nd{\mathbb{T}}^{d}_{N} where there are no construction issues. As before, EμE_{\mu} denotes the probability and expectation under μ\mu, and μ\mathbb{P}_{\mu} and 𝔼μ\mathbb{E}_{\mu} the process measure and expectation when starting in μ\mu.

Recall, as in Section 11, that WtN(G)W^{N}_{t}(G) for fixed GG smooth with compact support stands for the fluctuation field,

WtN(G)=1Nd/2xG(x/N)(ηN2t(x)ρ).W^{N}_{t}(G)\ =\ \frac{1}{N^{d/2}}\sum_{x}G(x/N)\big(\eta_{N^{2}t}(x)-\rho\big).

To derive the limit field, write as before

WtN(G)\displaystyle W^{N}_{t}(G) =\displaystyle= W0N(G)+N20tLWsN(G)𝑑s+tN(G)\displaystyle W^{N}_{0}(G)+N^{2}\int_{0}^{t}LW^{N}_{s}(G)ds+\mathcal{M}^{N}_{t}(G)

where, after the usual summation-by-parts,

LWtN(G)=12Nd/2x,ydp(y)x,yNG(x/N)(g(ηN2s(x))Ψ(ρ)).LW^{N}_{t}(G)\ =\ \frac{1}{2N^{d/2}}\sum_{x,y\in\mathbb{Z}^{d}}p(y)\triangle^{N}_{x,y}G(x/N)\big(g\big(\eta_{N^{2}s}(x)\big)-\Psi(\rho)\big).

Here, Ψ(a)=Eνa[g(η(0))]\Psi(a)=E_{\nu_{a}}[g(\eta(0))], and tN(G)\mathcal{M}^{N}_{t}(G) is a martingale such that

𝒩tN(G)=(tN(G))2N20tL(YsN(G))22YsN(G)LYsN(G)𝑑s{{\mathcal{N}}}^{N}_{t}(G)\ =\ (\mathcal{M}^{N}_{t}(G))^{2}-N^{2}\int_{0}^{t}L(Y^{N}_{s}(G))^{2}-2Y^{N}_{s}(G)LY^{N}_{s}(G)ds

is a martingale. The last integral in the display, equal to N(G)t\langle\mathcal{M}^{N}(G)\rangle_{t}, can be evaluated as

N20t[L(YsN(G))22YsN(G)LYsN(G)]𝑑s\displaystyle N^{2}\int_{0}^{t}\Big[L(Y^{N}_{s}(G))^{2}-2Y^{N}_{s}(G)LY^{N}_{s}(G)\Big]ds
=1Nd0tx,ydp(y)[x,yNG(x/N)]2g(ηN2s(x))𝑑s.\displaystyle\ \ \ =\ \frac{1}{N^{d}}\int_{0}^{t}\sum_{x,y\in\mathbb{Z}^{d}}p(y)[\nabla^{N}_{x,y}G(x/N)]^{2}g\big(\eta_{N^{2}s}(x)\big)ds.

These calculations are analogous to those for hydrodynamics in Sections 4, 5.

Following the method described for exclusion processes in Section 11, we have two steps:

Step 1: Show tightness of {WtN:t[0,T]}\{W^{N}_{t}:t\in[0,T]\} in an appropriate space, and continuity of limit trajectories under limit points.

Step 2: Identify the limit points in terms of a unique ‘infinite dimensional Ornstein-Uhlenbeck’ process

As before, the space of trajectories is D([0,T],𝒟)D([0,T],{\mathcal{D}}^{\prime}), where 𝒟{\mathcal{D}}^{\prime} is the dual space of distributions with respect to 𝒟=Cc(d){\mathcal{D}}=C^{\infty}_{c}(\mathbb{R}^{d}). Step 1, tightness, is accomplished as before, and it is left to the reader to verify the proof in the zero-range setting.

The more interesting part, for zero-range processes, is Step 2 where instead of the occupation variable η(x)\eta(x) we have a function of it, namely g(η(x))g(\eta(x)) in both martingales above. If the normalization were NdN^{-d} instead of Nd/2N^{-d/2}, replacing the nonlinear function with a function of the mass empirical density is the ‘standard’ hydrodynamic replacement. Here, we have to work a little harder. However, starting in equilibrium νρ\nu_{\rho} helps.

The following ‘Boltzmann-Gibbs’ estimate allows the replacement in tN(G)\mathcal{M}^{N}_{t}(G).

Theorem 12.1.1.

For smooth, compactly supported GG, we have

limN𝔼νρ[|0t1Nd/2x,ydp(y)x,yNG(x/N)\displaystyle\lim_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho}}\Big[\Big|\int_{0}^{t}\frac{1}{N^{d/2}}\sum_{x,y\in\mathbb{Z}^{d}}p(y)\triangle^{N}_{x,y}G(x/N)
(g(ηN2s(x))Ψ(ρ)Ψ(ρ)(ηN2s(x)ρ))]ds|2]= 0.\displaystyle\quad\quad\quad\cdot\Big(g\big(\eta_{N^{2}s}(x)\big)-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta_{N^{2}s}(x)-\rho\big)\Big)]ds\Big|^{2}\Big]\ =\ 0.

The replacement, however, in the square martingale 𝒩tN(G){{\mathcal{N}}}^{N}_{t}(G) will be a consequence of the following limit.

limN𝔼νρ[|0t1Ndx,yp(y)[x,yNG(x/N)]2[g(ηN2s(x))Ψ(ρ)]𝑑s|2]= 0.\lim_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho}}\Big[\Big|\int_{0}^{t}\frac{1}{N^{d}}\sum_{x,y}p(y)[\nabla^{N}_{x,y}G(x/N)]^{2}\Big[g\big(\eta_{N^{2}s}(x)\big)-\Psi(\rho)\Big]ds\Big|^{2}\Big]\ =\ 0. (12.1.1)

Hence, we arrive at the following result, specializing to the nearest-neighbor setting, when p(±ei)=1/(2d)p(\pm e_{i})=1/(2d) with respect to the standard basis {ei}i=1d\{e_{i}\}_{i=1}^{d}.

Theorem 12.1.2.

We have that WtNW^{N}_{t} converges to WtW_{t} where

dWt=Ψ(ρ)2dWtdt+d1Ψ(ρ)dt.dW_{t}\ =\ \frac{\Psi^{\prime}(\rho)}{2d}\triangle W_{t}dt+\sqrt{d^{-1}\Psi(\rho)}\nabla d\mathcal{B}_{t}. (12.1.2)

The characterization of WtW_{t} in terms of the generalized OU martingale problem of Holley and Stroock is as before with symmetric exclusion in Section 11. Though, the operators U=(Ψ(ρ)/(2d))U=(\Psi^{\prime}(\rho)/(2d))\triangle and B=IΨ(ρ)/d)B=I\Psi(\rho)/d)\nabla differ in prefactor constants.

Analogous to before with symmetric exclusion,

Eνρ[W0(G)W0(H)]=σ2G,HE_{\nu_{\rho}}[W_{0}(G)W_{0}(H)]\ =\ \sigma^{2}\langle G,H\rangle

where σ2(ρ)=Eνρ[(η(0)ρ)2]\sigma^{2}(\rho)=E_{\nu_{\rho}}[(\eta(0)-\rho)^{2}]. Also, the covariance of Wt(G)W_{t}(G) and Ws(H)W_{s}(H) satisfies the formula (11.2.5) where TtT_{t} is the semigroup associated to (Ψ(ρ)/(2d))(\Psi^{\prime}(\rho)/(2d))\triangle.

One way to look at (12.1.2) is to relate it to the hydrodynamic equation:

tρ=12dΨ(ρ)\partial_{t}\rho\ =\ \frac{1}{2d}\triangle\Psi(\rho)

with initial condition ρ(0,x)=ρ0(x)\rho(0,x)=\rho_{0}(x). The quantity WtNW^{N}_{t} can be seen as an ‘error’ via a ‘linearization’ of the hydrodynamic equation about the equilibrium density ρ\rho (the constant solution when starting from νρ\nu_{\rho}), where Ψ(ρ(t,x))Ψ(ρ)+Ψ(ρ)ρ(t,x)\Psi(\rho(t,x))\sim\Psi(\rho)+\Psi^{\prime}(\rho)\rho(t,x). See [206] for more physical intuition behind this intepretation.

We remark in passing, in the case g(k)kg(k)\equiv k, the setting of independent particles, the replacement Theorem 12.1.1 is not needed as, analogous to symmetric exclusion, the martingale tN(G){\mathcal{M}}^{N}_{t}(G) is already ‘closed’ with respect to WtNW^{N}_{t}, that is fully expressed in terms of WtN(G)W^{N}_{t}(G) and WtN(x,yNG)W^{N}_{t}(\triangle^{N}_{x,y}G).

12.2. Kipnis-Varadhan estimate

We begin with the following ‘Kipnis-Varadhan’ [131] non-asymptotic bound of independent interest, helpful to establish the Boltzmann-Gibbs principle. Recall the notions of H1H_{1} and H1H_{-1} norms from Section 9. These extend to the zero-range context, where the local functions used to define spaces H1H_{1} and H1H_{-1} are local L2(νρ)L^{2}(\nu_{\rho}) functions.

Lemma 12.2.1.

For all local L2(νρ)L^{2}(\nu_{\rho}) functions, we have for the symmetric zero-range process

𝔼νρ[(0tf(ηs)𝑑s)2] 12tf12.\mathbb{E}_{\nu_{\rho}}\Big[\Big(\int_{0}^{t}f(\eta_{s})ds\Big)^{2}\Big]\ \leq\ 12t\|f\|_{-1}^{2}.

Note that it may be that f1\|f\|_{-1} diverges for a given fL1(νρ)f\in L^{1}(\nu_{\rho}).

Proof.

Write the resolvent equation, for λ>0\lambda>0,

λuλLuλ=f.\lambda u_{\lambda}-Lu_{\lambda}\ =\ f.

Multiplying by uλu_{\lambda} and integrating, we have

λuλ02+uλ12=f,uλνρ,\lambda\|u_{\lambda}\|^{2}_{0}+\|u_{\lambda}\|^{2}_{1}\ =\ \langle f,u_{\lambda}\rangle_{\nu_{\rho}},

where f,hνρ=Eνρ[fg]\langle f,h\rangle_{\nu_{\rho}}=E_{\nu_{\rho}}[fg]. Note that f,uλνρf1uλ1\langle f,u_{\lambda}\rangle_{\nu_{\rho}}\leq\|f\|_{-1}\|u_{\lambda}\|_{1}, and so uλ1f1\|u_{\lambda}\|_{1}\leq\|f\|_{-1}. Now, consider the martingale

Mλ(t)=uλ(ηt)uλ(η0)0tLuλ(ηs)𝑑s,M_{\lambda}(t)\ =\ u_{\lambda}(\eta_{t})-u_{\lambda}(\eta_{0})-\int_{0}^{t}Lu_{\lambda}(\eta_{s})ds,

with quadratic variation Mλ=0t[Luλ22uλLuλ]𝑑s\langle M_{\lambda}\rangle=\int_{0}^{t}\big[Lu_{\lambda}^{2}-2u_{\lambda}Lu_{\lambda}\big]ds.

Write

0tf(ηs)𝑑s=Mλ(t)λ0tuλ(ηs)𝑑s+uλ(η0)uλ(ηt).\int_{0}^{t}f(\eta_{s})ds\ =\ M_{\lambda}(t)-\lambda\int_{0}^{t}u_{\lambda}(\eta_{s})ds+u_{\lambda}(\eta_{0})-u_{\lambda}(\eta_{t}).

Since 𝔼νρ[Mλ2(t)]=2tuλ12\mathbb{E}_{\nu_{\rho}}\big[M_{\lambda}^{2}(t)\big]=2t\|u_{\lambda}\|_{1}^{2}, from squaring the left hand side of the above display, using (a+b+c+d)24(a2+b2+c2+d2)(a+b+c+d)^{2}\leq 4(a^{2}+b^{2}+c^{2}+d^{2}), by stationarity, we have

𝔼νρ[(0tf(ηs)𝑑s)2] 4{2tuλ12+λ2t2uλ02+2uλ02}.\mathbb{E}_{\nu_{\rho}}\Big[\Big(\int_{0}^{t}f(\eta_{s})ds\Big)^{2}\Big]\ \leq\ 4\Big\{2t\|u_{\lambda}\|_{1}^{2}+\lambda^{2}t^{2}\|u_{\lambda}\|^{2}_{0}+2\|u_{\lambda}\|^{2}_{0}\Big\}.

Choosing λ=t1\lambda=t^{-1}, we see that the left hand side is bounded by

12tf,uλνρ 12tf12.12t\langle f,u_{\lambda}\rangle_{\nu_{\rho}}\ \leq\ 12t\|f\|^{2}_{-1}.\qed
Remark 12.2.2.

We comment Lemma 12.2.1 also holds for asymmetric zero-range processes, among others, where the H1H_{1} and H1H_{-1} norms are with respect to the symmetrized generator S=(L+L)/2S=(L+L^{*})/2. One can also put a ‘sup0tT\sup_{0\leq t\leq T}’ inside the 𝔼νρ\mathbb{E}_{\nu_{\rho}}-expectation, via a martingale argument. See [133], [195] for these generalizations.

12.3. Derivation of Boltzmann-Gibbs estimate

We need to show the variance of

0t1Nd/2x,ydp(y)x,yNG(x/N)(g(ηN2s(x))Ψ(ρ)Ψ(ρ)(ηN2s(x)ρ))𝑑s\int_{0}^{t}\frac{1}{N^{d/2}}\sum_{x,y\in\mathbb{Z}^{d}}p(y)\triangle^{N}_{x,y}G(x/N)\Big(g\big(\eta_{N^{2}s}(x)\big)-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta_{N^{2}s}(x)-\rho\big)\Big)ds

vanishes in the NN\uparrow\infty limit. It will be enough to bound the variance of

0t1Nd/2xdH(x/N)(g(ηN2s(x))Ψ(ρ)Ψ(ρ)(ηN2s(x)ρ))𝑑s\displaystyle\int_{0}^{t}\frac{1}{N^{d/2}}\sum_{x\in\mathbb{Z}^{d}}H(x/N)\Big(g\big(\eta_{N^{2}s}(x)\big)-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta_{N^{2}s}(x)-\rho\big)\Big)ds (12.3.1)

for H𝒟H\in{\mathcal{D}}, from which Theorem 12.1.1 can be deduced.

Write (12.3.1) as

0txNd/2H(x/N){g(ηN2s(x))𝔼νρ[g(ηN2s(x))|yB,xηN2s(y)]}ds\displaystyle\int_{0}^{t}\sum_{x}N^{-d/2}H(x/N)\Big\{g(\eta_{N^{2}s}(x))-\mathbb{E}_{\nu_{\rho}}\big[g(\eta_{N^{2}s}(x))\big|\sum_{y\in B_{\ell,x}}\eta_{N^{2}s}(y)\big]\Big\}ds
+0txNd/2H(x/N){𝔼νρ[g(ηN2s(x))|yB,xηN2s(y)]\displaystyle\ \ \ \ +\ \int_{0}^{t}\sum_{x}N^{-d/2}H(x/N)\Big\{\mathbb{E}_{\nu_{\rho}}\big[g(\eta_{N^{2}s}(x))\big|\sum_{y\in B_{\ell,x}}\eta_{N^{2}s}(y)\big] (12.3.2)
Ψ(ρ)Ψ(ρ)(ηN2s(x)ρ)}ds=A1+A2.\displaystyle\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ -\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta_{N^{2}s}(x)-\rho\big)\Big\}ds\ =\ A_{1}+A_{2}.

Here, B,xB_{\ell,x} is a block of width 2\ell\geq 2 centered at xx, and N\ell\ll N is another scaling parameter. Related to the study of the hydrodynamic limit, the idea is that A1A_{1} considers the approximation of g(ηN2s(x)CLOSEg(\eta_{N^{2}s}(x) by its conditional expectation average with respect to a local density. The term A1A_{1} gives the error with respect to the leading order terms in this conditional expectation.

The strategy will be to bound the H1H_{-1} norm of A1A_{1}, and to use Schwarz inequality and Taylor expansions with A2A_{2}, a sort of ‘equivalence of ensembles’ estimate. These are done in the next two subsections. In Subsection 12.3.3, we assemble these bounds to prove Theorem 12.1.1.

12.3.1. Bound on A1A_{1}

To bound the variance of A1A_{1}, we will bound the H1H_{-1} norm of its integrand, denoted 𝔄1{\mathfrak{A}}_{1}. Since time has been sped up by v(N)=N2v(N)=N^{2}, the generator of ηN2s\eta_{N^{2}s} is N2LN^{2}L. For local L2(νρ)L^{2}(\nu_{\rho}) functions ϕ\phi, we would like to demonstrate

𝔄1,ϕνρ𝔜1(N)(N2D(ϕ))1/2,\big\langle{\mathfrak{A}}_{1},\phi\big\rangle_{\nu_{\rho}}\leq{{\mathfrak{Y}}_{1}(N)}\big(N^{2}D(\phi)\big)^{1/2},

where the Dirichlet form N2D(ϕ)=ϕ,(N2L)ϕνρN^{2}D(\phi)=\big\langle\phi,(-N^{2}L)\phi\big\rangle_{\nu_{\rho}} and 𝔜1(N){\mathfrak{Y}}_{1}(N) is a bound of the maximum ratio 𝔄1,ϕνρ/(N2D(ϕ))1/2\big\langle{\mathfrak{A}}_{1},\phi\rangle_{\nu_{\rho}}/\big(N^{2}D(\phi)\big)^{1/2}. Then, the H1H_{-1} norm of 𝔄1{\mathfrak{A}}_{1} is bounded by 𝔜1(N){\mathfrak{Y}}_{1}(N), which we show vanishes as NN\uparrow\infty.

To this end, write

Nd/2H(x/N)τxV(η),ϕνρ=Nd/2H(x/N)τxV(η),ϕνρ,\big\langle N^{-d/2}H(x/N)\tau_{x}V(\eta),\phi\big\rangle_{\nu_{\rho}}\ =\ \big\langle N^{-d/2}H(x/N)\tau_{x}V(\eta),\phi_{\ell}\big\rangle_{\nu^{\ell}_{\rho}},

given V(η)=g(η(0))Eνρ[g(η(0))|yB,0η(y)]V(\eta)=g(\eta(0))-E_{\nu_{\rho}}[g(\eta(0))|\sum_{y\in B_{\ell,0}}\eta(y)] depends only on variables indexed by B,0B_{\ell,0}, where τx\tau_{x} is the shift operator, νρ=yB,xκΨ(ρ)\nu^{\ell}_{\rho}=\prod_{y\in B_{\ell,x}}\kappa_{\Psi(\rho)} is the restriction, and ϕ=Eνρ[ϕ|{η(y):yB,x}]\phi_{\ell}=E_{\nu_{\rho}}\big[\phi|\{\eta(y):y\in B_{\ell,x}\}\big]. We comment, as νρ\nu_{\rho} is a product measure, that V(η)=g(η(0))Eνρ[g(η(0))|yB,0η(y)]V(\eta)=g(\eta(0))-E_{\nu^{\ell}_{\rho}}[g(\eta(0))|\sum_{y\in B_{\ell,0}}\eta(y)].

We may further evaluate the right-hand side as

k0P(k,)Nd/2H(x/N)τxV(η),ϕνk,\sum_{k\geq 0}P(k,\ell)\big\langle N^{-d/2}H(x/N)\tau_{x}V(\eta),\phi_{\ell}\big\rangle_{\nu_{k,\ell}}

where νk,\nu_{k,\ell} is the ‘canonical’ measure, that is νρ\nu^{\ell}_{\rho} conditioned on there being kk particles in B,xB_{\ell,x}, and P(k,)=Pνρ(yB,xη(y)=k)P(k,\ell)=P_{\nu_{\rho}}\big(\sum_{y\in B_{\ell,x}}\eta(y)=k\big).

Recall η(x)=(2+1)dyB,xη(y)\eta^{\ell}(x)=(2\ell+1)^{-d}\sum_{y\in B_{\ell,x}}\eta(y) (cf. (4.5.1) from Section 4). Underlying the above localization, that is for adding and subtracting the conditional expectation Eνρ[g(η(x))|η(x)]E_{\nu_{\rho}}[g(\eta(x))|\eta^{\ell}(x)], is that we can now solve a certain ‘Poisson’ equation, no matter the particle number kk, since Eνk,[τxV]=0E_{\nu_{k,\ell}}[\tau_{x}V]=0 for all kk.

Indeed, note that νk,\nu_{k,\ell} is the unique invariant measure for the irreducible zero-range dynamics localized to B,xB_{\ell,x} with generator

Lx,f(η)=z,z+yB,xp(y)g(η(z))[f(ηz,z+y)f(η)],L_{x,\ell}f(\eta)=\sum_{z,z+y\in B_{\ell,x}}p(y)g(\eta(z))\big[f(\eta^{z,z+y})-f(\eta)\big],

and τxV\tau_{x}V is mean-zero with respect to νk,\nu_{k,\ell}, which assigns probabilities to configurations in {0,1,,k}B,x\{0,1,\ldots,k\}^{B_{\ell,x}}. Moreover, one may verify that νk,\nu_{k,\ell} is reversible with respect to Lx,L_{x,\ell}. Also, the Dirichlet form with respect to Lx,-L_{x,\ell} may be computed,

Dx,(f,νk,)\displaystyle D_{x,\ell}(f;\nu_{k,\ell}) =f,(Lx,)fνk,\displaystyle=\big\langle f,(-L_{x,\ell})f\big\rangle_{\nu_{k,\ell}}
=z,z+yB,xp(y)Eνk,[g(η(z))(f(ηz,z+y)f(η))2].\displaystyle=\sum_{z,z+y\in B_{\ell,x}}p(y)E_{\nu_{k,\ell}}\Big[g(\eta(z))\big(f(\eta^{z,z+y})-f(\eta)\big)^{2}\Big].

So, in particular, Lx,-L_{x,\ell} is a nonnegative, reversible operator.

Exercise 12.3.1.

Verify the reversibility of νk,\nu_{k,\ell} and the form of the Dirichlet form Dx,D_{x,\ell}.

Now, thinking of νk,\nu_{k,\ell} as a vector in |B,x|(k+1)\mathbb{R}^{|B_{\ell,x}|(k+1)}, since it is in null space of the transpose N2Lx,TN^{2}L^{T}_{x,\ell} as it is a stationary measure, and Eνk,[τxV]=0E_{\nu_{k,\ell}}[\tau_{x}V]=0 so that τxV\tau_{x}V is orthogonal to νk,\nu_{k,\ell}, we conclude that τxV\tau_{x}V belongs to the range of N2Lx,N^{2}L_{x,\ell}. See Subsection 9.1 for related decompositions.

Hence, we may solve τxV=N2Lx,u\tau_{x}V\ =\ -N^{2}L_{x,\ell}u for some function uu. In particular, as Lx,-L_{x,\ell} is nonnegative, and reversible with respect to νk,\nu_{k,\ell},

Nd/2H(x/N)τxV(η),ϕνk,=Nd/2H(x/N)(N2Lx,)u,ϕνk,\displaystyle\big\langle N^{-d/2}H(x/N)\tau_{x}V(\eta),\phi_{\ell}\big\rangle_{\nu_{k,\ell}}=\big\langle N^{-d/2}H(x/N)\big(-N^{2}L_{x,\ell}\big)u,\phi_{\ell}\big\rangle_{\nu_{k,\ell}}
=Nd/2H(x/N)(N2Lx,)1/2u,(N2Lx,)1/2ϕνk,\displaystyle\quad\quad=\big\langle N^{-d/2}H(x/N)\big(-N^{2}L_{x,\ell}\big)^{1/2}u,\big(-N^{2}L_{x,\ell}\big)^{1/2}\phi_{\ell}\big\rangle_{\nu_{k,\ell}}
=Nd/2H(x/N)(N2L,k)1/2τxV,(N2L,k)1/2ϕνk,.\displaystyle\quad\quad=\big\langle N^{-d/2}H(x/N)\big(-N^{2}L_{\ell,k}\big)^{-1/2}\tau_{x}V,\big(-N^{2}L_{\ell,k}\big)^{1/2}\phi_{\ell}\big\rangle_{\nu_{k,\ell}}.

At this point, we state a spectral gap inequality to be discussed later. Namely, for mean-zero functions, we have that

(Lx,)1/2τxVL2(νk,)2𝔐(,k)τxVL2(ν,k)2\big\|\big(-L_{x,\ell}\big)^{-1/2}\tau_{x}V\big\|^{2}_{L^{2}(\nu_{k,\ell})}\ \leq\ {{\mathfrak{M}}}(\ell,k)\big\|\tau_{x}V\big\|^{2}_{L^{2}(\nu_{\ell,k})}

where a bound of the inverse of the ‘spectral gap’ 𝔐(,k)C02{{\mathfrak{M}}}(\ell,k)\leq C_{0}\ell^{2} is independent of kk when (Lip) and (M) hold for the rate gg [142].

Hence, by the relation 2ab=infϵ>0{ϵa2+ϵ1b2}2ab=\inf_{\epsilon>0}\big\{\epsilon a^{2}+\epsilon^{-1}b^{2}\big\} for a,b>0a,b>0, we have

Nd/2H(x/N)τxV(η),ϕνk,\displaystyle\big\langle N^{-d/2}H(x/N)\tau_{x}V(\eta),\phi_{\ell}\big\rangle_{\nu_{k,\ell}}
ϵ2NdH2(x/N)N2C022τxVL2(νk,CLOSE2+ϵ1N22Dx,(ϕ,νk,).\displaystyle\quad\quad\leq\ \frac{\epsilon}{2}N^{-d}H^{2}(x/N)N^{-2}C_{0}^{2}\ell^{2}\big\|\tau_{x}V\big\|^{2}_{L^{2}(\nu_{k,\ell}}+\frac{\epsilon^{-1}N^{2}}{2}D_{x,\ell}(\phi_{\ell};\nu_{k,\ell}).

Note, by unraveling the measures, that

k0P(k,)Dx,(ϕ,νk,)\displaystyle\sum_{k\geq 0}P(k,\ell)D_{x,\ell}(\phi_{\ell};\nu_{k,\ell}) =z,z+yB,xp(y)Eνρ[g(η(z))(ϕ(ηz,z+y)ϕ(η))2]\displaystyle=\sum_{z,z+y\in B_{\ell,x}}p(y)E_{\nu_{\rho}}\Big[g(\eta(z))\big(\phi(\eta^{z,z+y})-\phi(\eta)\big)^{2}\Big]
:=Dx,(ϕ,νρ).\displaystyle:=D_{x,\ell}(\phi;\nu_{\rho}).

Also, by estimating the overcount of terms over bonds (z,z+y)(z,z+y), we have

xDx,(ϕ,νρ)C1dD(ϕ),\sum_{x}D_{x,\ell}(\phi;\nu_{\rho})\ \leq\ C_{1}\ell^{d}D(\phi),

where the full Dirichlet form is evaluated

D(ϕ)=z,ydp(y)Eνρ[g(η(z))(ϕ(ηz,z+y)ϕ(η))2].D(\phi)=\sum_{z,y\in\mathbb{Z}^{d}}p(y)E_{\nu_{\rho}}\Big[g(\eta(z))\big(\phi(\eta^{z,z+y})-\phi(\eta)\big)^{2}\Big].

In addition, k0P(k,)τxVL2(νk,)2=VL2(νρ)2\sum_{k\geq 0}P(k,\ell)\big\|\tau_{x}V\big\|^{2}_{L^{2}(\nu_{k,\ell})}\ =\ \big\|V\big\|^{2}_{L^{2}(\nu_{\rho})}.

Then, coming back to (12.3), summing over xx, we have

𝔄1,ϕνρ\displaystyle\big\langle{\mathfrak{A}}_{1},\phi\big\rangle_{\nu_{\rho}} =xdk0P(k,)Nd/2H(x/N)τxV,ϕνk,\displaystyle=\sum_{x\in\mathbb{Z}^{d}}\sum_{k\geq 0}P(k,\ell)\big\langle N^{-d/2}H(x/N)\tau_{x}V,\phi_{\ell}\big\rangle_{\nu_{k,\ell}}
ϵ2NdC22N2xH2(x/N)k0P(k,)τxVνk,2\displaystyle\leq\frac{\epsilon}{2N^{d}}\frac{C^{2}\ell^{2}}{N^{2}}\sum_{x}H^{2}(x/N)\sum_{k\geq 0}P(k,\ell)\big\|\tau_{x}V\big\|^{2}_{\nu_{k,\ell}}
+ϵ1N22xk0P(k,)Dx,(ϕ;νk,)\displaystyle\quad\quad+\frac{\epsilon^{-1}N^{2}}{2}\sum_{x}\sum_{k\geq 0}P(k,\ell)D_{x,\ell}(\phi_{\ell};\nu_{k,\ell})
ϵ2NdC22N2xH2(x/N)τxVνρ2+ϵ1N22CdD(ϕ)\displaystyle\leq\frac{\epsilon}{2N^{d}}\frac{C^{2}\ell^{2}}{N^{2}}\sum_{x}H^{2}(x/N)\big\|\tau_{x}V\big\|^{2}_{\nu_{\rho}}+\frac{\epsilon^{-1}N^{2}}{2}\cdot C\ell^{d}D(\phi)
CVL2(νρ)HL2(d)d/2+1N(N2D(ϕ))1/2,\displaystyle\leq C\|V\|_{L^{2}(\nu_{\rho})}\|H\|_{L^{2}(\mathbb{R}^{d})}\frac{\ell^{d/2+1}}{N}\big(N^{2}D(\phi)\big)^{1/2},

after optimizing on ϵ>0\epsilon>0. Here, we used translation-invariance to yield τxVνρ=Vνρ\|\tau_{x}V\|_{\nu_{\rho}}=\|V\|_{\nu_{\rho}} and the constant CC may have changed line to line.

Hence, the H1H_{-1} norm of 𝔄1{\mathfrak{A}}_{1} is bounded

𝔜1(N)=CVL2(νρ)HL2(d)d/2+1N=O(d/2+1/N),{\mathfrak{Y}}_{1}(N)=C\|V\|_{L^{2}(\nu_{\rho})}\|H\|_{L^{2}(\mathbb{R}^{d})}\frac{\ell^{d/2+1}}{N}=O(\ell^{d/2+1}/N),

and therefore the variance of A1A_{1} by Lemma 12.2.1 is bounded

𝔼νρ[(A1)2]CtVL2(νρ)2HL2(νρ)2d+2N2.0,\displaystyle\mathbb{E}_{\nu_{\rho}}\big[(A_{1})^{2}\big]\leq Ct\|V\|^{2}_{L^{2}(\nu_{\rho})}\|H\|^{2}_{L^{2}(\nu_{\rho})}\frac{\ell^{d+2}}{N^{2}}.\rightarrow 0, (12.3.3)

as NN\uparrow\infty for each \ell fixed.

12.3.2. Bound on A2A_{2}

Since HH is smooth, we may replace η(x)\eta(x) with η(x)\eta^{\ell}(x) in A2A_{2}. By invariance of νρ\nu_{\rho}, adding and subtracting ρ\rho, and Schwarz inequality,

limN𝔼νρ[|0t1Nd/2xH(x/N)[ηN2s(x)ηN2s(x)]𝑑s|2]\displaystyle\lim_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho}}\Big[\Big|\int_{0}^{t}\frac{1}{N^{d/2}}\sum_{x}H(x/N)\Big[\eta_{N^{2}s}(x)-\eta^{\ell}_{N^{2}s}(x)\Big]ds\Big|^{2}\Big]
=limN𝔼νρ[|0t1Nd/2x\displaystyle=\ \lim_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho}}\Big[\Big|\int_{0}^{t}\frac{1}{N^{d/2}}\sum_{x}
1(2+1)dyB,x[H(x/N)H((yx)/N)](ηN2s(x)ρ)ds|2]\displaystyle\quad\quad\quad\frac{1}{(2\ell+1)^{d}}\sum_{y\in B_{\ell,x}}\Big[H(x/N)-H((y-x)/N)\Big](\eta_{N^{2}s}(x)-\rho)ds\Big|^{2}\Big]
C(ρ,H,t)2N2 0.\displaystyle\leq\ C(\rho,H,t)\ell^{2}N^{-2}\ \rightarrow\ 0.

Then, by Schwarz inequality, using invariance and translation-invariance of νρ\nu_{\rho}, we have

𝔼νρ[|0txNd/2H(x/N)\displaystyle\mathbb{E}_{\nu_{\rho}}\Big[\Big|\int_{0}^{t}\sum_{x}N^{-d/2}H(x/N) (12.3.4)
×{𝔼νρ[g(ηN2s(x))|yB,xηN2s(y)]Ψρ)Ψ(ρ)(ηN2s(x)ρ)}ds|2]\displaystyle\quad\quad\quad\times\Big\{\mathbb{E}_{\nu_{\rho}}\big[g(\eta_{N^{2}s}(x))\big|\sum_{y\in B_{\ell,x}}\eta_{N^{2}s}(y)\big]-\Psi\rho)-\Psi^{\prime}(\rho)\big(\eta_{N^{2}s}^{\ell}(x)-\rho\big)\Big\}ds\Big|^{2}\Big]
Ct2d(1NdxH2(x/N))\displaystyle\ \leq\ Ct^{2}\ell^{d}\Big(\frac{1}{N^{d}}\sum_{x}H^{2}(x/N)\Big)
×Eνρ[(Eνρ[g(η(0))|yB,0η(y)]Ψ(ρ)Ψ(ρ)(η(0)ρ))2]\displaystyle\quad\quad\quad\times E_{\nu_{\rho}}\Big[\Big(E_{\nu_{\rho}}[g(\eta(0))|\sum_{y\in B_{\ell,0}}\eta(y)]-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta^{\ell}(0)-\rho\big)\Big)^{2}\Big]
C(t,H)dEνρ[(Eνρ[g(η(0))|yB,0η(y)]Ψ(ρ)Ψ(ρ)(η(0)ρ))2].\displaystyle\ \leq\ C(t,H)\ell^{d}E_{\nu_{\rho}}\Big[\Big(E_{\nu_{\rho}}[g(\eta(0))|\sum_{y\in B_{\ell,0}}\eta(y)]-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta^{\ell}(0)-\rho\big)\Big)^{2}\Big].

The factor d\ell^{d} arises since the summands over xx are independent only when they are separated by distance 2+12\ell+1.

We now estimate the mean-square of

Eνρ[g(η(0))Ψ(ρ)Ψ(ρ)(η(0)ρ)|yB,0η(y)].E_{\nu_{\rho}}\Big[g(\eta(0))-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta^{\ell}(0)-\rho\big)\Big|\sum_{y\in B_{\ell,0}}\eta(y)\Big].
Outside truncation

We first truncate the number of particles in B,0B_{\ell,0}. Let K=ρ/2K=\rho/2. Recall g(η(0))a0η(0)g(\eta(0))\leq a_{0}\eta(0). Then, by Schwarz inequality,

Eνρ[(Eνρ[g(η(0))Ψ(ρ)Ψ(ρ)(η(0)ρ)|yB,0η(y)])21(|η(0)ρ|>K)]\displaystyle E_{\nu_{\rho}}\Big[\Big(E_{\nu_{\rho}}\Big[g(\eta(0))-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta^{\ell}(0)-\rho\big)\Big|\sum_{y\in B_{\ell,0}}\eta(y)\Big]\Big)^{2}1\big(|\eta^{\ell}(0)-\rho|>K)\Big]
C(a0,ρ)Pνρ(η(0)>K)1/2C(a0,ρ)2dK4.\displaystyle\quad\leq C(a_{0},\rho)P_{\nu_{\rho}}\big(\eta^{\ell}(0)>K\big)^{1/2}\ \leq\ \frac{C(a_{0},\rho)}{\ell^{2d}K^{4}}. (12.3.5)

Here, we used Chebychev to bound Pνρ(|η(0)ρ|>K)Eνρ[(η(0)ρ)8]/K8P_{\nu_{\rho}}\big(|\eta^{\ell}(0)-\rho|>K\big)\leq E_{\nu_{\rho}}[(\eta^{\ell}(0)-\rho)^{8}]/K^{8}.

Inserting into (12.3.4), we see that the multiplying d\ell^{d} factor is compensated, and the cost of truncation is small, uniformly over NN, for large \ell.

Inside truncation

We now use a Taylor expansion and a local central limit theorem. For M=yB,0η(y)M=\sum_{y\in B_{\ell,0}}\eta(y), let M/(2+1)d:=M¯M/(2\ell+1)^{d}:=\bar{M}_{\ell}. Given the truncation, we have that ρ/2M¯3ρ/2\rho/2\leq\bar{M}_{\ell}\leq 3\rho/2 is bounded away from 00 and \infty uniformly in \ell.

Since νρ\nu_{\rho} is a product measure with marginals in the form given in Subsection 4.3, the conditional expectation Eνρ[h|yB,0η(y)=M]E_{\nu_{\rho}}[h|\sum_{y\in B_{\ell,0}}\eta(y)=M] does not depend on the density ρ\rho and can be changed to another, say M¯\bar{M}_{\ell}; see near (5.4.4) for a similar discussion with respect to the 11-block hydrodynamics lemma. Recall the calculation in Exercise 4.3.1,

Eνa[g(η(0)h(η)]=Ψ(a)Eνa[h(η+δ0)]E_{\nu_{a}}\big[g(\eta(0)h(\eta)]=\Psi(a)E_{\nu_{a}}[h(\eta+\delta_{0})]

where δ0\delta_{0} is the configuration with a single particle at 00. Then,

Eνρ[g(η(0)|yB,0η(y)=M]\displaystyle E_{\nu_{\rho}}\big[g(\eta(0)\big|\sum_{y\in B_{\ell,0}}\eta(y)=M\big] =EνM¯[g(η(0)|yB,0η(y)=M]\displaystyle=E_{\nu_{\bar{M}_{\ell}}}\big[g(\eta(0)\big|\sum_{y\in B_{\ell,0}}\eta(y)=M\big] (12.3.6)
=Ψ(M¯)PνM¯[yB,0η(y)=M1]PνM¯[yB,0η(y)=M].\displaystyle=\Psi(\bar{M}_{\ell})\frac{P_{\nu_{\bar{M}_{\ell}}}[\sum_{y\in B_{\ell,0}}\eta(y)=M-1]}{P_{\nu_{\bar{M}_{\ell}}}[\sum_{y\in B_{\ell,0}}\eta(y)=M]}.

Recall σ2(M¯)=EνM¯[(η(0)M¯)2]\sigma^{2}(\bar{M}_{\ell})=E_{\nu_{\bar{M}_{\ell}}}\big[(\eta(0)-\bar{M}_{\ell})^{2}\big]. By the local central limit Theorem VII.13 in [167] (applied with k=3k=3 there), when |SM|<|S-M|<\infty and M¯\bar{M}_{\ell} is bounded uniformly away from 00 and \infty, we have for z=(SM)/(κ(2+1)d/2)z=(S-M)/(\kappa(2\ell+1)^{d/2}) and large \ell,

|σ(M¯)(2+1)d/2PνM¯[yB,0η(y)=S]12πez22|=o(d/2).\displaystyle\Big|\sigma(\bar{M}_{\ell})(2\ell+1)^{d/2}P_{\nu_{\bar{M}_{\ell}}}[\sum_{y\in B_{\ell,0}}\eta(y)=S]-\frac{1}{\sqrt{2\pi}}e^{-\frac{z^{2}}{2}}\Big|\ =\ o(\ell^{-d/2}).

For S=M1S=M-1, we see z=κ1(2+1)d/2z=-\kappa^{-1}(2\ell+1)^{-d/2}, whereas for S=MS=M, we have z=0z=0, in which case σ(M¯)(2+1)d/2PνM¯(yB,0η(y)=M)(2π)1/2\sigma(\bar{M}_{\ell})(2\ell+1)^{d/2}P_{\nu_{\bar{M}_{\ell}}}\big(\sum_{y\in B_{\ell,0}}\eta(y)=M\big)\sim(2\pi)^{-1/2} for large \ell.

Hence, multiplying and dividing (12.3.6) by σ(M¯)(2+1)d/2\sigma(\bar{M}_{\ell})(2\ell+1)^{d/2}, on the set {ρ/2η(0)=M¯3ρ/2}\big\{\rho/2\leq\eta^{\ell}(0)=\bar{M}_{\ell}\leq 3\rho/2\big\}, we have

EνM¯[g(η(0))|yB,0η(y)=M]\displaystyle E_{\nu_{\bar{M}_{\ell}}}\big[g(\eta(0))\big|\sum_{y\in B_{\ell,0}}\eta(y)=M\big] =\displaystyle= Ψ(M¯)(1+o(d/2)).\displaystyle\Psi(\bar{M}_{\ell})\big(1+o(\ell^{-d/2})\big).

Then,

|Eνρ[g(η(0))Ψ(ρ)Ψ(ρ)(η(0)ρ)|yB,0η(y)]|21(|η(0)ρ|ρ/2)\displaystyle\Big|E_{\nu_{\rho}}\Big[g(\eta(0))-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta^{\ell}(0)-\rho\big)\Big|\sum_{y\in B_{\ell,0}}\eta(y)\Big]\Big|^{2}1\big(|\eta^{\ell}(0)-\rho|\leq\rho/2\big)
=|Ψ(M¯)Ψ(ρ)Ψ(ρ)[η(0)ρ)+o(d/2)|21(|η(0)ρ|ρ/2)\displaystyle\quad=\Big|\Psi(\bar{M}_{\ell})-\Psi(\rho)-\Psi^{\prime}(\rho)\big[\eta^{\ell}(0)-\rho\big)+o(\ell^{-d/2})\Big|^{2}1\big(|\eta^{\ell}(0)-\rho|\leq\rho/2\big)
sup|aρ|ρ/2|Ψ(a)|2[η(0)ρ]4+o(d),\displaystyle\quad\leq\sup_{|a-\rho|\leq\rho/2}|\Psi^{\prime}(a)|^{2}\big[\eta^{\ell}(0)-\rho\big]^{4}+o(\ell^{-d}),

from Taylor approximation.

Since Eνρ[(η(0)ρ)4]=O(2d)E_{\nu_{\rho}}\big[(\eta^{\ell}(0)-\rho)^{4}\big]=O(\ell^{-2d}), we observe

Eνρ[|Eνρ[g(η(0))Ψ(ρ)Ψ(ρ)(η(0)ρ)|yB,0η(y)]|21(|η(0)ρ|ρ/2)]\displaystyle E_{\nu_{\rho}}\Big[\Big|E_{\nu_{\rho}}\Big[g(\eta(0))-\Psi(\rho)-\Psi^{\prime}(\rho)\big(\eta^{\ell}(0)-\rho\big)\Big|\sum_{y\in B_{\ell,0}}\eta(y)\Big]\Big|^{2}1\big(|\eta^{\ell}(0)-\rho|\leq\rho/2\big)\Big]
=o(d).\displaystyle\quad=o(\ell^{-d}). (12.3.7)

Hence, with respect to (12.3.4), the quantity (12.3.2) multiplied by d\ell^{d} vanishes, uniformly in NN.

Finally, with estimates (12.3.2) and (12.3.2), inserting into (12.3.4), we have

limlimN𝔼νρ[(A2)2]=0.\displaystyle\lim_{\ell\uparrow\infty}\lim_{N\uparrow\infty}\mathbb{E}_{\nu_{\rho}}\big[(A_{2})^{2}\big]=0. (12.3.8)

12.3.3. Proof of Theorem 12.1.1

We need only show that 𝔼νρ[(Ai)2]\mathbb{E}_{\nu_{\rho}}\big[(A_{i})^{2}\big], for i=1,2i=1,2, vanish as NN\uparrow\infty and \ell\uparrow\infty, where A1,A2A_{1},A_{2} are given in (12.3). These limits are furnished in (12.3.3) and (12.3.8), concluding the argument.∎

12.4. Spectral gap

One can define the ‘spectral gap’ for a reversible process generator Lk,L_{k,\ell} in terms of a Poincare inequality:

Varνk,[f]𝔐(k,)Eνk,[f(Lk,)f].{\rm Var}_{\nu_{k,\ell}}[f]\ \leq\ {{\mathfrak{M}}}(k,\ell)E_{\nu_{k,\ell}}\big[f(-L_{k,\ell})f\big].

Then, the gap would be the reciprocal of the smallest 𝔐(k,){{\mathfrak{M}}}(k,\ell) for which the inequality is true for all ff.

Equivalently, the gap is the difference between the two largest eigenvalues of Lk,-L_{k,\ell}. Since 00 is the largest eigenvalue, the gap would be the negative of the second largest eigenvalue, λ2-\lambda_{2}. Since Lk,L_{k,\ell} is a matrix, one can in principle compute it exactly, but this is usually hard to do when the state space gets large.

The spectral gap has connections with the mixing time of the process. Recall that

Varνk,(Ptf)Ceλ2t.{\rm Var}_{\nu_{k,\ell}}(P_{t}f)\ \leq\ Ce^{\lambda_{2}t}.

The larger λ2-\lambda_{2}, the faster the approach of PtfP_{t}f to its mean Eνk,[f]E_{\nu_{k,\ell}}[f].

In zero-range processes, since the jump times are controlled by the rate gg, one expects the orders of the mixing time to depend on gg. This is in fact the case. When g(k)=kg(k)=k, the independent case, the mixing is rapid, and corresponds to the mixing time of a single random walk on B,0B_{\ell,0} which is O(2)O(\ell^{-2}). For instance, consider d=1d=1, then a nearest-neighbor walk, in moving from one end of the interval to the other, has to take \ell steps which usually takes 2\ell^{2} units of time.

If gg is not too different from the independent case, one expects similar behavior, not dependent on the number of particles, and this is the result quoted and used above, valid under our assumptions (Lip) and (M) [142].

If gg is sublinear, that is g(k)=kγg(k)=k^{\gamma} for 0<γ<10<\gamma<1, then it has been shown the spectral gap depends on the number of particles kk, namely the gap is O((1+ρ)γ2)O((1+\rho)^{-\gamma}\ell^{-2}) where ρ=k/(2+1)d\rho=k/(2\ell+1)^{d} [163]. For instance, if ρ\rho\uparrow\infty, movement becomes difficult, and the gap vanishes!

If g(k)=1(k1)g(k)=1(k\geq 1), then it can be seen that the gap is O((1+ρ)22)O((1+\rho)^{-2}\ell^{-2}) [162]. When d=1d=1, this is the case where there is a connection between the zero-range process and simple exclusion: The number of spaces between particles in simple exclusion correspond to the number of particles in the zero-range process.

It seems to be an open problem to characterize the gap when gg is bounded in general. One presumably expects the behavior as in the last case.

12.5. Notes

The Boltzmann-Gibbs principle, under a stationary measure, was named and proved first by Brox and Rost [33] which did not use a spectral gap assumption. See also [130] for a presentation along this line. The notion of using the spectral gap estimate to prove the Boltzmann-Gibbs principle seems to be newer; see also [97], [98].

While equilibrium fluctuations of particle systems with finite-range symmetric interactions is relatively well understood (cf. [130], [133], [206]), a main open problem is to understand ‘nonequilibrium’ fluctuations of the density field in a general class of particle systems. A main difficulty is to perform the needed ‘replacement’ estimates in the fluctuation scales. Results in dimension d=1d=1 are known for finite-range symmetric models; see [43], [74]. Recently, these results have been generalized to d3d\leq 3, for a class of particle systems [123]; see also [53], [86], [119], and discussions therein.

There are many works on mixing time, spectral gap and related log-Sobolev estimates. See for instance [28], [34], [35], [36], [37], [54], [60], [92], [109], [134], [174], [187] and references therein.

Beyond fluctuations, other scalings and limit fields have been considered. We mention in passing, cogent to the present narrative, these include the ‘Navier-Stokes’ corrections [140], and large deviations of the empirical density and ,currents [23], [24], [30], [132], [156], [172], [214].

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