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arXiv:2305.01081v3 [math.AP] 20 Jun 2026

Generalized Snell’s law and Maxwell equationsThanks: 2020 AMS Math Subject Classification: 78A40, 35Q61, 35D30.Thanks:  C.E.G was partially supported by NSF Grant DMS-1600578, and A. S. was partially supported by the University Research Board, Grants 104107 and 104631 from the American University of Beirut. August 11, 2026

Cristian E. Gutiérrez and Ahmad Sabra
August 11, 2026
Address: Department of Mathematics
Temple University
Philadelphia, PA 19122
Email address: gutierre@temple.edu Address: Department of Mathematics
American University of Beirut
Beirut, Lebanon
Email address: asabra@aub.edu.lb
Abstract.

This paper examines the Maxwell system of electrodynamics within the framework of distributions. A primary objective is to establish general boundary conditions for fields at interfaces when the charge and current densities are measures localized on the interface. From this analysis, the paper presents a derivation of the generalized Snell’s law, along with formulas for the amplitudes of the reflected and transmitted waves in terms of the incident amplitude.

Key words and phrases: 
Electromagnetism, Generalized functions, Generalized Snell’s law, Metasurfaces

1. Introduction

Metasurfaces or metalenses are ultra-thin layers built with nano-materials that can steer light in unconventional ways. In beam shaping, the subject of metasurfaces is a rapidly growing area of research with diverse practical applications. Central to this field is the generalized Snell’s law of refraction and reflection, which explains how beams propagate across metasurfaces. The law was introduced in the influential works [16] and [1] for planar geometries. Its formulation involves a function defined in a small neighborhood of the metasurface, called the phase discontinuity, and is further discussed in [15]. A rigorous mathematical derivation of the law for non-planar geometries was first obtained using wave fronts in [7, Sect. 3] and later by applying the Fermat principle of least action in [8, Sect. 2]. These works also demonstrate the existence of phase discontinuities for various geometric configurations and multiple applications.

Let us recall precisely the generalized Snell’s law in vector form. Given a surface Γ\Gamma separating two media II and IIII with refractive indices n1n_{1} and n2n_{2} respectively, and ff a phase function defined on Γ\Gamma, the generalized Snell’s law of refraction states that if a wave in medium II with unit direction vector 𝐤i{\mathbf{k}}_{i} strikes Γ\Gamma at a point PP, then the wave is refracted into medium IIII with unit direction vector 𝐤t{\mathbf{k}}_{t} satisfying

(1.1) n1𝐤in2𝐤t=λ𝐧(P)+f(P)n_{1}\,{\mathbf{k}}_{i}-n_{2}\,{\mathbf{k}}_{t}=\lambda\,{\mathbf{n}}(P)+\nabla f(P)

where 𝐧(P){\mathbf{n}}(P) is the unit normal to Γ\Gamma at PP, and λ\lambda\in{\mathbb{R}}, see [8, Equation (2.4)]. On the other hand, a wave reflected back into medium II has unit direction vector 𝐤r{\mathbf{k}}_{r} and satisfies the generalized law of reflection

(1.2) n1𝐤in1𝐤r=λ𝐧(P)+f(P).n_{1}\,{\mathbf{k}}_{i}-n_{1}\,{\mathbf{k}}_{r}=\lambda^{\prime}\,{\mathbf{n}}(P)+\nabla f(P).

A primary goal of this paper is to explore Maxwell’s equations from a distributional perspective and derive relationships between the electric and magnetic fields on either side of a boundary or interface—that is, boundary conditions—when the current and charge densities are measures concentrated on the interface. While Maxwell’s equations are well understood in the classical sense, analyzing them in the setting of generalized functions (or distributions) becomes essential when dealing with discontinuous fields across surfaces; see, for example, [10] and [9]. The main result of this part is Theorem 3.1, which we believe has independent interest, since the discontinuities of the fields are assumed to be measures concentrated on the interface, a novel assumption in this generality.

Using this analysis, the second objective of the paper is to derive the generalized laws of refraction and reflection directly from Maxwell’s equations, which is a novel approach in the metasurface setting. To achieve this, we propose representing the transmitted and reflected electric fields as nonlinear waves incorporating the phase discontinuity. This representation—detailed in equations (4.3) and (4.4)—enables us to deduce the generalized Snell’s laws from the boundary conditions established in Theorem 3.1. Because the electric fields must satisfy the Maxwell system, this imposes constraints on the phase discontinuity, and the main result of this part is Theorem 4.3. Using the boundary conditions obtained, a third objective is to calculate the amplitudes of the transmitted and reflected waves in terms of incident wave, Proposition 6.1. This is possible under the necessary and sufficient condition (6.3) between the amplitude of the incident wave and the wave vectors. This is also a new result in the paper.

To place the results in broader context, it is worth noting that metasurfaces that refract or reflect beams according to prescribed energy patterns are closely connected to Monge–Ampère type partial differential equations, as discussed in [5]. The analysis of chromatic aberration in metalenses is carried out in [8], with further insights available in [16]. For applications related to tunable metasurfaces using graphene, see [2]. Recent developments and applications in the field can also be found in [12], [11], and [14].

The paper is organized as follows. In Section 2, we recall results concerning distributions, outline the assumptions on the fields, and establish formulas needed later. These are applied in Section 3 to prove Theorem 3.1, which provides general boundary conditions.

The derivation of the generalized Snell law from the Maxwell’s system is the subject of Section 4, where we employ Theorem 3.1. In Section 5, we obtain boundary conditions for the magnetic fields, which, combined with the previously derived conditions, are used in Section 6 to derive explicit formulas for the wave amplitudes. Finally, the Appendix 7 contains a proof of the exponential Lemma 4.2.

2. Preliminaries

In this section, we revisit concepts related to distributions that are essential for analyzing the Maxwell system in this context. Specifically, we derive the formulas that are subsequently utilized to establish general boundary conditions in Theorem 3.1. These formulas are presented in Propositions 2.1 and 2.4.

Let Ω3\Omega\subset{\mathbb{R}}^{3} be an open and bounded domain. A generalized function or distribution in Ω\Omega is a complex-valued continuous linear functional defined in the class of test functions 𝒟(Ω)=C0(Ω)\mathcal{D}(\Omega)=C_{0}^{\infty}(\Omega) that are infinitely differentiable in Ω\Omega having compact support in Ω\Omega . As usual, 𝒟(Ω)\mathcal{D}^{\prime}(\Omega) denotes the class of distributions in Ω\Omega [13]. If g𝒟(Ω)g\in\mathcal{D}^{\prime}(\Omega), then, as usual, g,φ\langle g,\varphi\rangle denotes the value of the distribution gg on the test function φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega).

We say that 𝐆=(G1,G2,G3){\bf G}=(G_{1},G_{2},G_{3}) is a vector valued distribution in Ω\Omega if each component Gi𝒟(Ω)G_{i}\in\mathcal{D}^{\prime}(\Omega), 1i31\leq i\leq 3. The divergence of 𝐆{\bf G} is the scalar distribution defined by

(2.3) 𝐆,φ=i=13Gi,φxi,\langle\nabla\cdot{\bf G},\varphi\rangle=-\sum_{i=1}^{3}\langle G_{i},\varphi_{x_{i}}\rangle,

and the curl of 𝐆{\bf G} is the vector valued distribution in Ω\Omega defined by

(2.4) ×𝐆,φ=(G2,φx3G3,φx2)𝐢(G1,φx3G3,φx1)𝐣+(G1,φx2G2,φx1)𝐤.\langle\nabla\times{\bf G},\varphi\rangle=\left(\langle G_{2},\varphi_{x_{3}}\rangle-\langle G_{3},\varphi_{x_{2}}\rangle\right){\bf i}-\left(\langle G_{1},\varphi_{x_{3}}\rangle-\langle G_{3},\varphi_{x_{1}}\rangle\right){\bf j}+\left(\langle G_{1},\varphi_{x_{2}}\rangle-\langle G_{2},\varphi_{x_{1}}\rangle\right){\bf k}.

Then it follows that

(2.5) (×𝐆)=0,\nabla\cdot(\nabla\times{\bf G})=0,

in the sense of distributions. When the distribution 𝐆=(G1,G2,G3){\bf G}=(G_{1},G_{2},G_{3}) is locally integrable in Ω\Omega we obtain from (2.3), and (2.4) that

𝐆,φ=Ω𝐆φdx,×𝐆,φ=Ω𝐆×φdx.\langle\nabla\cdot{\bf G},\varphi\rangle=-\int_{\Omega}{\bf G}\cdot\nabla\varphi\,dx,\qquad\langle\nabla\times{\bf G},\varphi\rangle=\int_{\Omega}{\bf G}\times\nabla\varphi\,dx.

We consider the following configuration. Ω\Omega is a smooth open and bounded domain in 3\mathbb{R}^{3} and Γ\Gamma is a smooth surface that splits Ω\Omega into two disjoint open parts Ω+\Omega_{+} and Ω\Omega_{-}, i.e., Ω=ΩΓΩ+\Omega=\Omega_{-}\cup\Gamma\cup\Omega_{+}, as follows: for every x0Γx_{0}\in\Gamma there exists a ball B(x0,r)ΩB(x_{0},r)\subset\Omega and γC1(B(x0,r))\gamma\in C^{1}\left(B(x_{0},r)\right) such that

ΩB(x0,r)\displaystyle\Omega_{-}\cap B(x_{0},r) ={(x1,x2,x3)B(x0,r):x3<γ(x1,x2)}\displaystyle=\{(x_{1},x_{2},x_{3})\in B(x_{0},r):x_{3}<\gamma(x_{1},x_{2})\}
Ω+B(x0,r)\displaystyle\Omega_{+}\cap B(x_{0},r) ={(x1,x2,x3)B(x0,r):x3>γ(x1,x2)}.\displaystyle=\{(x_{1},x_{2},x_{3})\in B(x_{0},r):x_{3}>\gamma(x_{1},x_{2})\}.
Ω\OmegaΩ\Omega_{-}Ω+\Omega_{+}Γ\Gamma
Figure 1. Ω=ΩΓΩ+.\Omega=\Omega_{-}\cup\Gamma\cup\Omega_{+}.

We are given fields 𝐆{\bf G}_{-} in Ω\Omega_{-} and 𝐆+{\bf G}_{+} in Ω+\Omega_{+} satisfying the following properties

  1. (F1)

    𝐆C1(Ω),𝐆+C1(Ω+){\bf G}_{-}\in C^{1}(\Omega_{-}),{\bf G}_{+}\in C^{1}(\Omega_{+}).

  2. (F2)

    The first order derivatives of 𝐆±{\bf G}_{\pm} are in L1(Ω±)L^{1}(\Omega_{\pm}), respectively.

  3. (F3)

    For every xΓx\in\Gamma, limyx,yΩ𝐆(y)\lim_{y\to x,y\in\Omega_{-}}{\bf G}_{-}(y) and limyx,yΩ+𝐆+(y)\lim_{y\to x,y\in\Omega_{+}}{\bf G}_{+}(y) exist and are finite.

As a consequence, each 𝐆{\mathbf{G}}_{-} and 𝐆+{\mathbf{G}}_{+} can be extended continuously to Γ\Gamma by setting

𝐆(x)=limyx,yΩ𝐆(y);𝐆+(x)=limyx,yΩ+𝐆+(y),{\mathbf{G}}_{-}(x)=\lim_{y\to x,y\in\Omega_{-}}{\bf G}_{-}(y);\qquad{\mathbf{G}}_{+}(x)=\lim_{y\to x,y\in\Omega_{+}}{\bf G}_{+}(y),

for each xΓx\in\Gamma. For such fields 𝐆{\bf G_{-}} and 𝐆+{\bf G_{+}}, the linear functional 𝐆{\mathbf{G}} given by

(2.6) 𝐆,φ=Ω𝐆(x)φ(x)𝑑x+Ω+𝐆+(x)φ(x)𝑑x\langle{\mathbf{G}},\varphi\rangle=\int_{\Omega_{-}}{\mathbf{G}}_{-}(x)\,\varphi(x)\,dx+\int_{\Omega_{+}}{\mathbf{G}}_{+}(x)\,\varphi(x)\,dx

is a well defined distribution for φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega). The jump of the fields in Γ\Gamma is defined by

[[𝐆(x)]]=𝐆+(x)𝐆(x),for xΓ.[[{\bf G}(x)]]={\bf G_{+}}(x)-{\bf G_{-}}(x),\quad\text{for $x\in\Gamma$}.

We then have the following expressions for the curl and divergence of 𝐆{\mathbf{G}}.

Proposition 2.1.

If the field 𝐆{\mathbf{G}} satisfies (F1)(F3), then for each φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega) we have

(2.7) 𝐆,φ\displaystyle\langle\nabla\cdot{\bf G},\varphi\rangle =Γφ(x)[[𝐆(x)]]𝐧dσ+Ωφ𝐆dx+Ω+φ𝐆+dx\displaystyle=\int_{\Gamma}\varphi(x)\,[[{\bf G}(x)]]\cdot{\bf n}\,d\sigma+\int_{\Omega_{-}}\varphi\,\nabla\cdot{\bf G_{-}}\,dx+\int_{\Omega_{+}}\varphi\nabla\cdot{\bf G_{+}}\,dx
(2.8) ×𝐆,φ\displaystyle\langle\nabla\times{\bf G},\varphi\rangle =Γφ(x)[[𝐆(x)]]×𝐧dσ+Ωφ×𝐆dx+Ω+φ×𝐆+dx\displaystyle=-\int_{\Gamma}\varphi(x)\,[[{\bf G}(x)]]\times{\bf n}\,d\sigma+\int_{\Omega_{-}}\varphi\nabla\times{\bf G_{-}}\,dx+\int_{\Omega_{+}}\varphi\nabla\times{\bf G_{+}}\,dx

with 𝐧{\bf n} the unit normal to Γ\Gamma pointing toward Ω+\Omega_{+}.

Proof.

Given ε>0\varepsilon>0, define

Ωε={xΩ:dist(x,Γ)>ε}Ω+ε={xΩ+:dist(x,Γ)>ε}.\Omega_{-}^{\varepsilon}=\{x\in\Omega_{-}:\text{dist}(x,\Gamma)>\varepsilon\}\qquad\qquad\Omega_{+}^{\varepsilon}=\{x\in\Omega_{+}:\text{dist}(x,\Gamma)>\varepsilon\}.

For φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega), we have from (2.3) and the definition of 𝐆{\mathbf{G}} in (2.6) that

𝐆,φ\displaystyle\langle\nabla\cdot{\bf G},\varphi\rangle =Ω𝐆φdxΩ+𝐆+φdx\displaystyle=-\int_{\Omega_{-}}{\bf G_{-}}\cdot\nabla\varphi\,dx-\int_{\Omega_{+}}{\bf G_{+}}\cdot\nabla\varphi\,dx
=Ωε𝐆φdxΩΩε𝐆φdxΩ+ε𝐆+φdxΩ+Ω+ε𝐆+φdx\displaystyle=-\int_{\Omega_{-}^{\varepsilon}}{\bf G_{-}}\cdot\nabla\varphi\,dx-\int_{\Omega_{-}\setminus\Omega_{-}^{\varepsilon}}{\bf G_{-}}\cdot\nabla\varphi\,dx-\int_{\Omega_{+}^{\varepsilon}}{\bf G_{+}}\cdot\nabla\varphi\,dx-\int_{\Omega_{+}\setminus\Omega_{+}^{\varepsilon}}{\bf G_{+}}\cdot\nabla\varphi\,dx
=(I+II+III+IV).\displaystyle=-(I+II+III+IV).

II,IV0II,IV\to 0 as ε0+\varepsilon\to 0^{+} because the extensions 𝐆±{\mathbf{G}}_{\pm} are locally bounded in Ω±Γ\Omega_{\pm}\cup\Gamma and φ\varphi is compactly supported in Ω\Omega. Since 𝐆{\mathbf{G}}_{-} is C1C^{1} in Ωε\Omega^{\varepsilon}_{-}, using the divergence theorem we obtain

I=Ωεφ𝐆𝐧εdσΩεφ𝐆dxI=\int_{\partial\Omega_{-}^{\varepsilon}}\varphi{\bf G_{-}}\cdot{\bf n_{-}^{\varepsilon}}\,d\sigma-\int_{\Omega_{-}^{\varepsilon}}\varphi{\bf\nabla\cdot G_{-}}\,dx\\

with 𝐧ε{\bf n}^{\varepsilon}_{-} the outward unit normal to Ωε\partial\Omega^{\varepsilon}_{-}. Since φ\varphi has compact support in Ω\Omega, 𝐆L1(Ω)\nabla\cdot{\bf G_{-}}\in L^{1}(\Omega_{-}), and 𝐆{\mathbf{G}}_{-} is locally bounded in ΩΓ\Omega_{-}\cup\Gamma, it follows that

IΓφ𝐆𝐧dσΩφ𝐆dx,I\to\int_{\Gamma}\varphi{\bf G_{-}}\cdot{\bf n}\,d\sigma-\int_{\Omega_{-}}\varphi\nabla\cdot{\bf G_{-}}\,dx,

with 𝐧{\bf n} is the unit normal to Γ\Gamma toward Ω+\Omega_{+}. Similarly we get

IIIΓφ𝐆+(𝐧)dσΩ+φ𝐆+dx,III\to\int_{\Gamma}\varphi{\bf G_{+}}\cdot({-\bf n})\,d\sigma-\int_{\Omega_{+}}\varphi\nabla\cdot{\bf G_{+}}\,dx,

with 𝐧-{\bf n} the unit normal to Γ\Gamma toward Ω\Omega_{-}. Hence (2.7) follows.

We next prove (2.8). Let φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega), we have from (2.4) and the definition of 𝐆{\bf G} in (2.6) that

×𝐆,φ\displaystyle\langle\nabla\times{\bf G},\varphi\rangle =Ω𝐆×φ𝑑x+Ω+𝐆+×φ𝑑x\displaystyle=\int_{\Omega_{-}}{\bf G_{-}}\times\nabla\varphi\,dx+\int_{\Omega_{+}}{\bf G_{+}}\times\nabla\varphi\,dx
=Ωε𝐆×φ𝑑x+ΩΩε𝐆×φ𝑑x+Ω+ε𝐆+×φ𝑑x+Ω+Ω+ε𝐆+×φ𝑑x\displaystyle=\int_{\Omega_{-}^{\varepsilon}}{\bf G_{-}}\times\nabla\varphi\,dx+\int_{\Omega_{-}\setminus\Omega_{-}^{\varepsilon}}{\bf G_{-}}\times\nabla\varphi\,dx+\int_{\Omega_{+}^{\varepsilon}}{\bf G_{+}}\times\nabla\varphi\,dx+\int_{\Omega_{+}\setminus\Omega_{+}^{\varepsilon}}{\bf G_{+}}\times\nabla\varphi\,dx
=I+II+III+IV\displaystyle=I+II+III+IV

II,IV0II,IV\to 0 as ε0+\varepsilon\to 0^{+} because the extensions 𝐆±{\mathbf{G}}_{\pm} are locally bounded in Ω±Γ\Omega_{\pm}\cup\Gamma and φ\varphi is compactly supported in Ω\Omega. We write I=(I1,I2,I3)I=(I_{1},I_{2},I_{3}), 𝐆=(G1,G2,G3){\bf G}_{-}=(G_{1}^{-},G_{2}^{-},G_{3}^{-}), and 𝐧ε=(n1ε,n2ε,n3ε){\bf n^{\varepsilon}_{-}}=(n_{1}^{\varepsilon},n_{2}^{\varepsilon},n_{3}^{\varepsilon}) the outward unit normal to Ωε\partial\Omega^{\varepsilon}_{-}. Using the divergence theorem

I1\displaystyle I_{1} =ΩεG2φx3G3φx2𝑑x\displaystyle=\int_{\Omega_{-}^{\varepsilon}}G_{2}^{-}\varphi_{x_{3}}-G_{3}^{-}\varphi_{x_{2}}\,dx
=(ΩεφG2n3ε𝑑σΩε(G2)x3φ𝑑x)(ΩεφG3n2ε𝑑σΩε(G3)x2φ𝑑x)\displaystyle=\left(\int_{\partial\Omega_{-}^{\varepsilon}}\varphi G_{2}^{-}n_{3}^{\varepsilon}\,d\sigma-\int_{\Omega_{-}^{\varepsilon}}(G_{2}^{-})_{x_{3}}\varphi\,dx\right)-\left(\int_{\partial\Omega_{-}^{\varepsilon}}\varphi G_{3}^{-}n_{2}^{\varepsilon}\,d\sigma-\int_{\Omega_{-}^{\varepsilon}}(G_{3}^{-})_{x_{2}}\varphi\,dx\right)
=Ωεφ(G2n3εG3n2ε)𝑑σ+Ωεφ((G3)x2(G2)x3)𝑑x.\displaystyle=\int_{\partial\Omega^{\varepsilon}_{-}}\varphi(G_{2}^{-}n_{3}^{\varepsilon}-G_{3}^{-}n_{2}^{\varepsilon})\,d\sigma+\int_{\Omega^{\varepsilon}_{-}}\varphi((G_{3}^{-})_{x_{2}}-(G_{2}^{-})_{x_{3}})\,dx.

Similarly

I2\displaystyle I_{2} =ΩεG1φx3+G3φx1dx=Ωεφ(G3n1εG1n3ε)dσ+Ωεφ((G1)x3(G3)x1)dx.\displaystyle=\int_{\Omega_{-}^{\varepsilon}}-G_{1}^{-}\varphi_{x_{3}}+G_{3}^{-}\varphi_{x_{1}}\,dx=\int_{\partial\Omega^{\varepsilon}_{-}}\varphi(G_{3}^{-}n_{1}^{\varepsilon}-G_{1}^{-}n_{3}^{\varepsilon})\,d\sigma+\int_{\Omega^{\varepsilon}_{-}}\varphi((G_{1}^{-})_{x_{3}}-(G_{3}^{-})_{x_{1}})\,dx.

and

I3=ΩεG1φx2G2φx1𝑑x=Ωεφ(G1n2εG2n1ε)𝑑σ+Ωεφ((G2)x1(G1)x2)𝑑x.\displaystyle I_{3}=\int_{\Omega_{-}^{\varepsilon}}G_{1}^{-}\varphi_{x_{2}}-G_{2}^{-}\varphi_{x_{1}}\,dx=\int_{\partial\Omega^{\varepsilon}_{-}}\varphi(G_{1}^{-}n_{2}^{\varepsilon}-G_{2}^{-}n_{1}^{\varepsilon})\,d\sigma+\int_{\Omega^{\varepsilon}_{-}}\varphi((G_{2}^{-})_{x_{1}}-(G_{1}^{-})_{x_{2}})\,dx.

Combining the above calculations, we deduce that

I=Ωεφ𝐆×𝐧εdσ+Ωεφ×𝐆dx.I=\int_{\partial\Omega_{-}^{\varepsilon}}\varphi{\bf G_{-}}\times{\bf n_{-}^{\varepsilon}}\,d\sigma+\int_{\Omega^{\varepsilon}_{-}}\varphi\nabla\times{\bf G_{-}}\,dx.

Since φ\varphi is compactly supported in Ω\Omega, 𝐆{\bf G_{-}} is locally bounded in ΩΓ\Omega_{-}\cup\Gamma , and ×𝐆L1(Ω)\nabla\times{\bf G_{-}}\in L^{1}(\Omega_{-}) then

IΓφ𝐆×𝐧dσ+Ωφ×𝐆dx.I\to\int_{\Gamma}\varphi{\bf G}_{-}\times{\bf n}\,d\sigma+\int_{\Omega_{-}}\varphi\nabla\times{\bf G_{-}}\,dx.

Similarly we get

III=Ω+εφ𝐆+×𝐧+εdσ+Ω+εφ×𝐆+dxΓφ𝐆+×(𝐧)dσ+Ω+φ×𝐆+dx.III=\int_{\partial\Omega_{+}^{\varepsilon}}\varphi{\bf G_{+}}\times{\bf n}^{\varepsilon}_{+}\,d\sigma+\int_{\Omega^{\varepsilon}_{+}}\varphi\nabla\times{\bf G_{+}}\,dx\to\int_{\Gamma}\varphi{\bf G}_{+}\times({\bf-n})\,d\sigma+\int_{\Omega_{+}}\varphi\nabla\times{\bf G_{+}}\,dx.

Hence (2.8) follows. ∎

2.1. Distributions depending on a parameter

Since the fields satisfying Maxwell’s equations depend on time, we consider vector-valued distributions in Ω\Omega depending on a parameter tt\in\mathbb{R}, that is, for each tt\in\mathbb{R}, g(,t)𝒟(Ω)g(\cdot,t)\in\mathcal{D}^{\prime}(\Omega), see [4, Appendix 2, p. 147]. We need the following.

Definition 2.2.

Let g(,t)g(\cdot,t) be a distribution in Ωn\Omega\subseteq\mathbb{R}^{n} depending on the parameter tt\in{\mathbb{R}}. We say that the derivative of g(,t)g(\cdot,t) with respect to the parameter tt exists if for each test function φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega), the function g(,t),φ\langle g(\cdot,t),\varphi\rangle is differentiable in tt, and there exists a distribution h(,t)h(\cdot,t) depending on the parameter tt such that

h(,t),φ=ddtg(,t),φ.\langle h(\cdot,t),\varphi\rangle=\dfrac{d}{dt}\langle g(\cdot,t),\varphi\rangle.

We write h(x,t)=gt(x,t).h(x,t)=\dfrac{\partial g}{\partial t}(x,t).

Proposition 2.3.

Given a distribution g(,t)g(\cdot,t) in Ω\Omega, tt\in\mathbb{R}, if gt(,t)\dfrac{\partial g}{\partial t}(\cdot,t) exists for each tt\in\mathbb{R}, then for every multi-index α=(α1,,αn)\alpha=(\alpha_{1},\cdots,\alpha_{n}) with αi0\alpha_{i}\in{\mathbb{Z}}_{\geq 0}, the derivative with respect to tt of the distribution DαgD^{\alpha}g exists and we have

(Dαg)t=Dα(gt),\dfrac{\partial(D^{\alpha}g)}{\partial t}=D^{\alpha}\left(\dfrac{\partial g}{\partial t}\right),

with Dα=α1α2αnx1α1x2α2xnαnD^{\alpha}=\dfrac{\partial^{\alpha_{1}}\partial^{\alpha_{2}}\cdots\partial^{\alpha_{n}}}{\partial x_{1}^{\alpha_{1}}\partial x_{2}^{\alpha_{2}}\cdots\partial x_{n}^{\alpha_{n}}}.

Proof.

If h(,t)=gth(\cdot,t)=\dfrac{\partial g}{\partial t} and φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega), then g(,t),φ\langle g(\cdot,t),\varphi\rangle is differentiable in tt. Since

Dαg(,t),φ=(1)|α|g(,t),Dαφ,\langle D^{\alpha}g(\cdot,t),\varphi\rangle=(-1)^{|\alpha|}\langle g(\cdot,t),D^{\alpha}\varphi\rangle,

with |α|=α1++αn|\alpha|=\alpha_{1}+\cdots+\alpha_{n}, and Dαφ𝒟(Ω)D^{\alpha}\varphi\in\mathcal{D}(\Omega), then Dαg(,t),φ\langle D^{\alpha}g(\cdot,t),\varphi\rangle is differentiable in tt and

ddtDαg(,t),φ=(1)|α|ddtg(,t),Dαφ=(1)|α|h(,t),Dαφ=Dαh,φ.\dfrac{d}{dt}\langle D^{\alpha}g(\cdot,t),\varphi\rangle=(-1)^{|\alpha|}\dfrac{d}{dt}\langle g(\cdot,t),D^{\alpha}\varphi\rangle=(-1)^{|\alpha|}\langle h(\cdot,t),D^{\alpha}\varphi\rangle=\langle D^{\alpha}h,\varphi\rangle.

Recalling the set up at the beginning of this section in Figure 1, Ω\Omega is a smooth open and bounded domain in 3\mathbb{R}^{3}, and Γ\Gamma is a smooth surface that splits Ω\Omega into two disjoint open parts Ω+\Omega_{+} and Ω\Omega_{-}, i.e., Ω=ΩΓΩ+\Omega=\Omega_{-}\cup\Gamma\cup\Omega_{+}. For tt\in\mathbb{R}, we are given a function g(,t)g(\cdot,t) satisfying

  1. (H1)

    g(,t)Lloc1(Ω)g(\cdot,t)\in L^{1}_{loc}(\Omega) for every tt,

  2. (H2)

    for each fixed xΩ±x\in\Omega_{\pm} the function g(x,)g(x,\cdot) is differentiable with respect to tt and there exists a function ψL1(Ω+Ω)\psi\in L^{1}(\Omega_{+}\cup\Omega_{-}) such that |gt(x,t)|ψ(x)\left|\dfrac{\partial g}{\partial t}(x,t)\right|\leq\psi(x) for a.e. xΩ±x\in\Omega_{\pm} and for each tt.

For every tt, the linear functional g(,t)g(\cdot,t) given by

g(,t),φ=Ωg(x,t)φ(x)𝑑x,\langle g(\cdot,t),\varphi\rangle=\int_{\Omega}g(x,t)\varphi(x)\,dx,

is then a well defined distribution by Item (H1).

Proposition 2.4.

If 𝐆(,t)=(g1(,t),g2(,t),g3(,t)){\mathbf{G}}(\cdot,t)=(g_{1}(\cdot,t),g_{2}(\cdot,t),g_{3}(\cdot,t)) is a vector-valued distribution with each gig_{i} satisfying (H1) and (H2), then the distribution 𝐆(,t){\mathbf{G}}(\cdot,t) has a derivative with respect to the parameter tt, and

𝐆t(,t),φ=Ω𝐆t(x,t)φ(x)𝑑x+Ω+𝐆t(x,t)φ(x)𝑑x.\left\langle\dfrac{\partial{\mathbf{G}}}{\partial t}(\cdot,t),\varphi\right\rangle=\int_{\Omega_{-}}\dfrac{\partial{\mathbf{G}}}{\partial t}(x,t)\varphi(x)\,dx+\int_{\Omega_{+}}\dfrac{\partial{\mathbf{G}}}{\partial t}(x,t)\varphi(x)\,dx.
Proof.

Let us denote by g(,t)g(\cdot,t) any of the components of 𝐆{\mathbf{G}}. We write for φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega) and tt\in{\mathbb{R}}

g(,t),φ=Ωg(x,t)φ(x)𝑑x=Ωg(x,t)φ(x)𝑑x+Ω+g(x,t)φ(x)𝑑x,\displaystyle\langle g(\cdot,t),\varphi\rangle=\int_{\Omega}g(x,t)\,\varphi(x)\,dx=\int_{\Omega_{-}}g(x,t)\,\varphi(x)\,dx+\int_{\Omega_{+}}g(x,t)\,\varphi(x)\,dx,

since from (H1), the integral Γg(x,t)φ(x)𝑑x=0\int_{\Gamma}g(x,t)\,\varphi(x)\,dx=0. Using condition (H2) and the Lebesgue dominated convergence theorem, we can justify differentiation under the integral sign and obtain that g(,t),φ\langle g(\cdot,t),\varphi\rangle is differentiable in tt, and that

ddtg(,t),φ=Ωgt(x,t)φ(x)𝑑x+Ω+gt(x,t)φ(x)𝑑x.\displaystyle\dfrac{d}{dt}\langle g(\cdot,t),\varphi\rangle=\int_{\Omega_{-}}\dfrac{\partial g}{\partial t}(x,t)\,\varphi(x)\,dx+\int_{\Omega_{+}}\dfrac{\partial g}{\partial t}(x,t)\,\varphi(x)\,dx.

From (H2), the linear functional h(,t)h(\cdot,t) given by

h(,t),φ=Ωgt(x,t)φ(x)𝑑x+Ω+gt(x,t)φ(x)𝑑x,\langle h(\cdot,t),\varphi\rangle=\int_{\Omega_{-}}\dfrac{\partial g}{\partial t}(x,t)\,\varphi(x)\,dx+\int_{\Omega_{+}}\dfrac{\partial g}{\partial t}(x,t)\,\varphi(x)\,dx,

is a well defined distribution and hence we obtain h(,t)=gt(,t)h(\cdot,t)=\dfrac{\partial g}{\partial t}(\cdot,t). ∎

3. Maxwell equations in distributional sense and general boundary conditions

We are given Ω\Omega open and bounded domain in 3\mathbb{R}^{3}, and Γ\Gamma a smooth surface separating Ω\Omega into two open parts Ω+\Omega_{+} and Ω\Omega_{-} as in Section 2. We are interested in the Maxwell system [3, Sections 1.1 and 1.2] which written in Gaussian (or cgs) units has the form

(3.1) {×𝐇=4πc𝐉+1c𝐃t𝐃=4πρ×𝐄=1c𝐁t𝐁=0,\begin{cases}\nabla\times{\bf H}=\dfrac{4\pi}{c}{\bf J}+\dfrac{1}{c}\dfrac{\partial{\bf D}}{\partial t}\\ \nabla\cdot{\bf D}=4\pi\rho\\ \nabla\times{\bf E}=-\dfrac{1}{c}\dfrac{\partial{\bf B}}{\partial t}\\ \nabla\cdot{\bf B}=0\end{cases},

where the curl and divergence are understood in the sense of distributions as in Section 2, and the fields 𝐇,𝐉,𝐃,𝐄,𝐁\bf H,J,D,E,B are vector valued distributions in Ω\Omega depending on the parameter tt\in{\mathbb{R}} in the sense of Section 2.1, with 𝐉{\mathbf{J}} given, and ρ\rho is scalar distribution in Ω\Omega, also given, depending also on the parameter tt\in{\mathbb{R}}.

The purpose of this section is to show that under general assumptions on the current density field 𝐉{\mathbf{J}} and the charge density ρ\rho each equation in the Maxwell system (3.1), understood in distributional sense, implies a boundary condition at the interface Γ\Gamma and the solutions are classical solutions away from Γ\Gamma. Viceversa, classical solutions in Ω±\Omega_{\pm} discontinuous across Γ\Gamma, give rise to distributions solutions in Ω\Omega. This is the contents of the following theorem.

Theorem 3.1.

Let us assume that 𝐉{\mathbf{J}} and ρ\rho satisfy

  1. (a)

    𝐉(x,t)=𝐉0(x,t)+νt{\mathbf{J}}(x,t)={\mathbf{J}}_{0}(x,t)+\nu_{t} with 𝐉0(x,t){\mathbf{J}}_{0}(x,t) a locally integrable 3{\mathbb{C}}^{3}-valued function for xΩx\in\Omega for each tt; and νt\nu_{t} is a family of 3{\mathbb{C}}^{3}-valued Borel measures in Ω\Omega depending on the parameter tt that are all concentrated on Γ\Gamma, that is, the support of νt\nu_{t} is contained in Γ\Gamma;

  2. (b)

    ρ(x,t)=ρ0(x,t)+μt\rho(x,t)=\rho_{0}(x,t)+\mu_{t} with ρ0(x,t)\rho_{0}(x,t) locally integrable in Ω\Omega for each tt, and μt\mu_{t} are Borel measures in Ω\Omega depending on the parameter tt that are all concentrated on the surface Γ\Gamma.

Suppose also that 𝐁{\mathbf{B}} and 𝐃{\mathbf{D}} are given fields satisfying (F1), (F2), (F3), (H1), and (H2); and 𝐄{\mathbf{E}} and 𝐇{\mathbf{H}} are also given fields satisfying (F1), (F2), and (F3); 𝐧{\bf n} denotes the unit normal to Γ\Gamma toward Ω+\Omega_{+}.

Then we have the following

  1. (1)

    If 𝐃{\mathbf{D}} satisfies 𝐃=4πρ\nabla\cdot{\mathbf{D}}=4\pi\rho in Ω\Omega in the sense of distributions, then 𝐃±(x,t)=4πρ0(x,t)\nabla\cdot{\mathbf{D}}_{\pm}(x,t)=4\pi\rho_{0}(x,t) for a.e. xΩ±x\in\Omega_{\pm} and for each tt, and

    (3.2) dμt(x)=14π[[𝐃(x,t)]]𝐧(x)dσ(x),d\mu_{t}(x)=\frac{1}{4\pi}[[{\mathbf{D}}(x,t)]]\cdot{\bf n}(x)\,d\sigma(x),

    where dσd\sigma denotes the surface measure on Γ\Gamma. Reciprocally, if 𝐃±=4πρ0\nabla\cdot{\mathbf{D}}_{\pm}=4\pi\rho_{0} holds point-wise in Ω±\Omega_{\pm} and (3.2) holds, then 𝐃=χΩ𝐃+χΩ+𝐃+{\mathbf{D}}=\chi_{\Omega_{-}}{\mathbf{D}}_{-}+\chi_{\Omega_{+}}{\mathbf{D}}_{+} satisfies the equation 𝐃=4πρ\nabla\cdot{\mathbf{D}}=4\pi\rho in Ω\Omega in the sense of distributions; as usual, χE\chi_{E} denotes the characteristic function of the set EE.

  2. (2)

    If 𝐁{\mathbf{B}} satisfies 𝐁=0\nabla\cdot{\mathbf{B}}=0 in Ω\Omega in the sense of distributions, then 𝐁±(x,t)=0\nabla\cdot{\mathbf{B}}_{\pm}(x,t)=0 point-wise xΩ±x\in\Omega_{\pm} and for each tt and

    (3.3) [[𝐁(x,t)]]𝐧(x)=0for a.e. xΓ (with respect to surface measure) for all t.[[{\mathbf{B}}(x,t)]]\cdot{\bf n}(x)=0\quad\text{for a.e. $x\in\Gamma$ (with respect to surface measure) for all $t$.}

    Reciprocally, if 𝐁±=0\nabla\cdot{\mathbf{B}}_{\pm}=0 holds point-wise in Ω±\Omega_{\pm} and (3.3) holds, then 𝐁=χΩ𝐁+χΩ+𝐁+{\mathbf{B}}=\chi_{\Omega_{-}}{\mathbf{B}}_{-}+\chi_{\Omega_{+}}{\mathbf{B}}_{+} satisfies the equation 𝐁=0\nabla\cdot{\mathbf{B}}=0 in the sense of distributions.

  3. (3)

    If 𝐇{\mathbf{H}} and 𝐃{\mathbf{D}} satisfy ×𝐇=4πc𝐉+1c𝐃t\nabla\times{\mathbf{H}}=\dfrac{4\pi}{c}{\mathbf{J}}+\dfrac{1}{c}\dfrac{\partial{\mathbf{D}}}{\partial t} in Ω\Omega in the sense of distributions, then ×𝐇±(x,t)=4πc𝐉0(x,t)+1c𝐃±t(x,t)\nabla\times{\mathbf{H}}_{\pm}(x,t)=\dfrac{4\pi}{c}{\mathbf{J}}_{0}(x,t)+\dfrac{1}{c}\dfrac{\partial{\mathbf{D}}_{\pm}}{\partial t}(x,t) point-wise for xΩ±x\in\Omega_{\pm} and

    (3.4) dνt(x)=c4π[[𝐇(x,t)]]×𝐧(x)dσ(x).d\nu_{t}(x)=-\dfrac{c}{4\pi}[[{\mathbf{H}}(x,t)]]\times{\bf n}(x)\,d\sigma(x).

    Reciprocally, if the equation holds point-wise in Ω±\Omega_{\pm} and (3.4) also holds, then the distributional equation holds for 𝐇=χΩ𝐇+χΩ+𝐇+{\mathbf{H}}=\chi_{\Omega_{-}}{\mathbf{H}}_{-}+\chi_{\Omega_{+}}{\mathbf{H}}_{+} and 𝐃=χΩ𝐃+χΩ+𝐃+{\mathbf{D}}=\chi_{\Omega_{-}}{\mathbf{D}}_{-}+\chi_{\Omega_{+}}{\mathbf{D}}_{+}.

  4. (4)

    If 𝐄{\mathbf{E}} and 𝐁{\mathbf{B}} satisfy ×𝐄=1c𝐁t\nabla\times{\mathbf{E}}=-\dfrac{1}{c}\dfrac{\partial{\mathbf{B}}}{\partial t} in Ω\Omega in the sense of distributions, then ×𝐄±(x,t)=1c𝐁±t(x,t)\nabla\times{\mathbf{E}}_{\pm}(x,t)=-\dfrac{1}{c}\dfrac{\partial{\mathbf{B}}_{\pm}}{\partial t}(x,t) point-wise in Ω±\Omega_{\pm} and

    (3.5) [[𝐄(x,t)]]×𝐧(x)=𝟎for a.e. xΓ (with respect to surface measure) for all t.[[{\mathbf{E}}(x,t)]]\times{\bf n}(x)={\bf 0}\quad\text{for a.e. $x\in\Gamma$ (with respect to surface measure) for all $t$.}

    Reciprocally, if the equation holds point-wise in Ω±\Omega_{\pm} and (3.5) also holds, then the distributional equation holds for 𝐄=χΩ𝐄+χΩ+𝐄+{\mathbf{E}}=\chi_{\Omega_{-}}{\mathbf{E}}_{-}+\chi_{\Omega_{+}}{\mathbf{E}}_{+} and 𝐁=χΩ𝐁+χΩ+𝐁+{\mathbf{B}}=\chi_{\Omega_{-}}{\mathbf{B}}_{-}+\chi_{\Omega_{+}}{\mathbf{B}}_{+}.

Proof.

(1) From (b)(b), ρ(,t)\rho(\cdot,t) is a distribution depending on tt given by

ρ(,t),φ=Ωρ0(x,t)φ(x)𝑑x+Ωφ(x)dμt(x)=Ωρ0(x,t)φ(x)𝑑x+Γφ(x)dμt(x),\langle\rho(\cdot,t),\varphi\rangle=\int_{\Omega}\rho_{0}(x,t)\,\varphi(x)\,dx+\int_{\Omega}\varphi(x)\,d\mu_{t}(x)=\int_{\Omega}\rho_{0}(x,t)\,\varphi(x)dx+\int_{\Gamma}\varphi(x)\,d\mu_{t}(x),

for each φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega); and 𝐃\nabla\cdot{\mathbf{D}} is a distribution that acting on a test function φ\varphi is given by (2.7). We have

𝐃(,t),φ=4πρ(,t),φ\langle\nabla\cdot{\mathbf{D}}(\cdot,t),\varphi\rangle=4\pi\langle\rho(\cdot,t),\varphi\rangle

for each tt. If supp(φ)Ω\text{supp}(\varphi)\subset\Omega_{-} or supp(φ)Ω+\text{supp}(\varphi)\subset\Omega_{+}, then from (2.7)

Ωφ(x)𝐃(x,t)dx+Ω+φ(x)𝐃+(x,t)dx=4πΩρ0(x,t)φ(x)dx,\int_{\Omega_{-}}\varphi(x)\,\nabla\cdot{{\mathbf{D}}_{-}(x,t)}\,dx+\int_{\Omega_{+}}\varphi(x)\,\nabla\cdot{{\mathbf{D}}_{+}(x,t)}\,dx=4\pi\int_{\Omega}\rho_{0}(x,t)\,\varphi(x)\,dx,

which implies 𝐃±(x,t)=4πρ0(x,t) for a.e. xΩ± and for each t.\nabla\cdot{\mathbf{D}}_{\pm}(x,t)=4\pi\rho_{0}(x,t)\text{ for a.e. $x\in\Omega_{\pm}$ and for each $t$.} That is, the equation 𝐃=4πρ\nabla\cdot{\mathbf{D}}=4\pi\rho is satisfied pointwise a.e. in Ω±\Omega_{\pm}. If supp(φ)Γ\text{supp}(\varphi)\cap\Gamma\neq\emptyset, we then get again from (2.7) that

Γφ(x)[[𝐃(x,t)]]𝐧(x)𝑑σ(x)=4πΓφ(x)dμt(x),\int_{\Gamma}\varphi(x)\,[[{\mathbf{D}}(x,t)]]\cdot{\bf n}(x)\,d\sigma(x)=4\pi\int_{\Gamma}\varphi(x)\,d\mu_{t}(x),

that is, the measure μt\mu_{t} has density 14π[[𝐃(x,t)]]𝐧(x)\dfrac{1}{4\pi}[[{\mathbf{D}}(x,t)]]\cdot{\bf n}(x), and (3.2) follows. Notice that this part only uses that 𝐃{\mathbf{D}} satisfies (F1)(F3).

For the converse, applying (2.7) to 𝐃{\mathbf{D}} yields

𝐃,φ\displaystyle\langle\nabla\cdot{\mathbf{D}},\varphi\rangle =Γφ(x)[[𝐃(x)]]𝐧dσ+Ωφ𝐃dx+Ω+φ𝐃+dx\displaystyle=\int_{\Gamma}\varphi(x)\,[[{\mathbf{D}}(x)]]\cdot{\bf n}\,d\sigma+\int_{\Omega_{-}}\varphi\,\nabla\cdot{\mathbf{D}}_{-}\,dx+\int_{\Omega_{+}}\varphi\nabla\cdot{\mathbf{D}}_{+}\,dx
=4πΓφ(x)dμt+4πΩφρ0dx+Ω+φρ0dxfrom (3.2)\displaystyle=4\pi\,\int_{\Gamma}\varphi(x)\,d\mu_{t}+4\pi\,\int_{\Omega_{-}}\varphi\,\rho_{0}\,dx+\int_{\Omega_{+}}\varphi\,\rho_{0}\,dx\quad\text{from \eqref{eq:density of mut bis}}
=4πΓφ(x)dμt+4πΩφρ0𝑑x=4πρ,φ.\displaystyle=4\pi\,\int_{\Gamma}\varphi(x)\,d\mu_{t}+4\pi\,\int_{\Omega}\varphi\,\rho_{0}\,dx=4\pi\,\langle\rho,\varphi\rangle.

(2) We proceed as in the proof of (1) and in this way we obtain 𝐁±(x,t)=0\nabla\cdot{\mathbf{B}}_{\pm}(x,t)=0 for a.e. xΩ±x\in\Omega_{\pm} and for each tt; and (3.3). Reciprocally, 𝐁=χΩ𝐁+χΩ+𝐁+{\mathbf{B}}=\chi_{\Omega_{-}}{\mathbf{B}}_{-}+\chi_{\Omega_{+}}{\mathbf{B}}_{+} satisfies the equation 𝐁=0\nabla\cdot{\mathbf{B}}=0 in the sense of distributions.

(3) The equation reads

×𝐇,φ=4πc𝐉,φ+1c𝐃t,φ,\left\langle\nabla\times{\mathbf{H}},\varphi\right\rangle=\dfrac{4\pi}{c}\left\langle{\mathbf{J}},\varphi\right\rangle+\dfrac{1}{c}\left\langle\dfrac{\partial{\mathbf{D}}}{\partial t},\varphi\right\rangle,

for each φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega). From Proposition 2.4

𝐃t,φ=Ω𝐃(x,t)tφ(x)𝑑x+Ω+𝐃+(x,t)tφ(x)𝑑x.\left\langle\dfrac{\partial{\mathbf{D}}}{\partial t},\varphi\right\rangle=\int_{\Omega_{-}}\dfrac{\partial{\mathbf{D}}_{-}(x,t)}{\partial t}\varphi(x)\,dx+\int_{\Omega_{+}}\dfrac{\partial{\mathbf{D}}_{+}(x,t)}{\partial t}\varphi(x)\,dx.

If supp(φ)Ω\text{supp}(\varphi)\subset\Omega_{-} or supp(φ)Ω+\text{supp}(\varphi)\subset\Omega_{+}, then from (2.8)

Ωφ(x)×𝐇(x,t)dx+Ω+φ(x)×𝐇+(x,t)dx\displaystyle\int_{\Omega_{-}}\varphi(x)\,\nabla\times{\mathbf{H}}_{-}(x,t)\,dx+\int_{\Omega_{+}}\varphi(x)\,\nabla\times{\mathbf{H}}_{+}(x,t)\,dx
=4πcΩ𝐉0(x,t)φ(x)𝑑x+1cΩ𝐃t(x,t)φ(x)𝑑x+1cΩ+𝐃+t(x,t)φ(x)𝑑x,\displaystyle\qquad=\dfrac{4\pi}{c}\int_{\Omega}{\mathbf{J}}_{0}(x,t)\,\varphi(x)\,dx+\dfrac{1}{c}\int_{\Omega_{-}}\dfrac{\partial{\mathbf{D}}_{-}}{\partial t}(x,t)\varphi(x)\,dx+\dfrac{1}{c}\int_{\Omega_{+}}\dfrac{\partial{\mathbf{D}}_{+}}{\partial t}(x,t)\varphi(x)\,dx,

which implies ×𝐇±(x,t)=4πc𝐉0(x,t)+1c𝐃±t(x,t) for a.e. xΩ± and all t\nabla\times{\mathbf{H}}_{\pm}(x,t)=\dfrac{4\pi}{c}{\mathbf{J}}_{0}(x,t)+\dfrac{1}{c}\dfrac{\partial{\mathbf{D}}_{\pm}}{\partial t}(x,t)\text{ for a.e. $x\in\Omega_{\pm}$ and all $t$}. If supp(φ)Γ\text{supp}(\varphi)\cap\Gamma\neq\emptyset, we then get again from (2.8) that

Γφ(x)[[𝐇(x,t)]]×𝐧(x)dσ(x)=4πcΓφ(x)dνt(x),-\int_{\Gamma}\varphi(x)\,[[{\mathbf{H}}(x,t)]]\times{\bf n}(x)\,d\sigma(x)=\dfrac{4\pi}{c}\int_{\Gamma}\varphi(x)\,d\nu_{t}(x),

that is, the measure νt\nu_{t} has density c4π[[𝐇(x,t)]]×𝐧(x)-\dfrac{c}{4\pi}[[{\mathbf{H}}(x,t)]]\times{\bf n}(x), so (3.4) follows.

If each equation ×𝐇±=4πc𝐉0+1c𝐃±t\nabla\times{\mathbf{H}}_{\pm}=\dfrac{4\pi}{c}{\mathbf{J}}_{0}+\dfrac{1}{c}\dfrac{\partial{\mathbf{D}}_{\pm}}{\partial t} holds in Ω±\Omega_{\pm} in the classical sense and (3.4) holds, then the equation ×𝐇=4πc𝐉+1c𝐃t\nabla\times{\mathbf{H}}=\dfrac{4\pi}{c}{\mathbf{J}}+\dfrac{1}{c}\dfrac{\partial{\mathbf{D}}}{\partial t} is satisfied in Ω\Omega in the sense of distributions where 𝐇{\mathbf{H}} is the distribution given by the locally integrable function χΩ𝐇+χΩ+𝐇+\chi_{\Omega_{-}}{\mathbf{H}}_{-}+\chi_{\Omega_{+}}{\mathbf{H}}_{+}. In fact, from (2.8) and (3.4)

×𝐇,φ\displaystyle\langle\nabla\times{\mathbf{H}},\varphi\rangle =Γφ(x)[[𝐇(x)]]×𝐧dσ+Ωφ×𝐇dx+Ω+φ×𝐇+dx\displaystyle=-\int_{\Gamma}\varphi(x)\,[[{\mathbf{H}}(x)]]\times{\bf n}\,d\sigma+\int_{\Omega_{-}}\varphi\,\nabla\times{\mathbf{H}}_{-}\,dx+\int_{\Omega_{+}}\varphi\,\nabla\times{\mathbf{H}}_{+}\,dx
=4πcΓφ(x)dνt+4πcΩφ𝐉0𝑑x+1cΩφ𝐃t𝑑x+1cΩ+φ𝐃+t𝑑x\displaystyle=\dfrac{4\pi}{c}\int_{\Gamma}\varphi(x)\,d\nu_{t}+\dfrac{4\pi}{c}\int_{\Omega}\varphi\,{\mathbf{J}}_{0}\,dx+\dfrac{1}{c}\int_{\Omega_{-}}\varphi\,\dfrac{\partial{\mathbf{D}}_{-}}{\partial t}\,dx+\dfrac{1}{c}\int_{\Omega_{+}}\varphi\,\dfrac{\partial{\mathbf{D}}_{+}}{\partial t}\,dx
=4πc𝐉,φ+1c𝐃t,φ.\displaystyle=\dfrac{4\pi}{c}\langle{\mathbf{J}},\varphi\rangle+\dfrac{1}{c}\left\langle\dfrac{\partial{\mathbf{D}}}{\partial t},\varphi\right\rangle.

(4) The equation reads

×𝐄,φ=1c𝐁t,φ,\left\langle\nabla\times{\mathbf{E}},\varphi\right\rangle=-\dfrac{1}{c}\left\langle\dfrac{\partial{\mathbf{B}}}{\partial t},\varphi\right\rangle,

for each φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega). From Proposition 2.4

𝐁t,φ=Ω𝐁(x,t)tφ(x)𝑑x+Ω+𝐁(x,t)tφ(x)𝑑x.\left\langle\dfrac{\partial{\mathbf{B}}}{\partial t},\varphi\right\rangle=\int_{\Omega_{-}}\dfrac{\partial{\mathbf{B}}(x,t)}{\partial t}\varphi(x)\,dx+\int_{\Omega_{+}}\dfrac{\partial{\mathbf{B}}(x,t)}{\partial t}\varphi(x)\,dx.

If supp(φ)Ω\text{supp}(\varphi)\subset\Omega_{-} or supp(φ)Ω+\text{supp}(\varphi)\subset\Omega_{+}, then from (2.8)

Ωφ(x)×𝐄(x,t)dx+Ω+φ(x)×𝐄+(x,t)dx\displaystyle\int_{\Omega_{-}}\varphi(x)\,\nabla\times{\mathbf{E}}_{-}(x,t)\,dx+\int_{\Omega_{+}}\varphi(x)\,\nabla\times{\mathbf{E}}_{+}(x,t)\,dx
=1cΩ𝐁t(x,t)φ(x)dx1cΩ+𝐁+t(x,t)φ(x)dx,\displaystyle\qquad=-\dfrac{1}{c}\int_{\Omega_{-}}\dfrac{\partial{\mathbf{B}}_{-}}{\partial t}(x,t)\varphi(x)\,dx-\dfrac{1}{c}\int_{\Omega_{+}}\dfrac{\partial{\mathbf{B}}_{+}}{\partial t}(x,t)\varphi(x)\,dx,

which implies ×𝐄±(x,t)=1c𝐁±t(x,t)\nabla\times{\mathbf{E}}_{\pm}(x,t)=-\dfrac{1}{c}\dfrac{\partial{\mathbf{B}}_{\pm}}{\partial t}(x,t) for a.e. xΩ±x\in\Omega_{\pm} and all tt. If supp(φ)Γ\text{supp}(\varphi)\cap\Gamma\neq\emptyset, we then get again from (2.8) that

×𝐄,φ\displaystyle\langle\nabla\times{\mathbf{E}},\varphi\rangle =Γφ(x)[[𝐄(x,t)]]×𝐧dσ+Ωφ×𝐄dx+Ω+φ×𝐄+dx\displaystyle=-\int_{\Gamma}\varphi(x)\,[[{\mathbf{E}}(x,t)]]\times{\bf n}\,d\sigma+\int_{\Omega_{-}}\varphi\nabla\times{\mathbf{E}}_{-}\,dx+\int_{\Omega_{+}}\varphi\nabla\times{\mathbf{E}}_{+}\,dx
=Γφ(x)[[𝐄(x,t)]]×𝐧dσ1cΩφ𝐁t(x,t)dx1cΩ+φ𝐁+t(x,t)dx\displaystyle=-\int_{\Gamma}\varphi(x)\,[[{\mathbf{E}}(x,t)]]\times{\bf n}\,d\sigma-\dfrac{1}{c}\int_{\Omega_{-}}\varphi\dfrac{\partial{\mathbf{B}}_{-}}{\partial t}(x,t)\,dx-\dfrac{1}{c}\int_{\Omega_{+}}\varphi\dfrac{\partial{\mathbf{B}}_{+}}{\partial t}(x,t)\,dx
=Γφ(x)[[𝐄(x,t)]]×𝐧dσ1c𝐁t,φ\displaystyle=-\int_{\Gamma}\varphi(x)\,[[{\mathbf{E}}(x,t)]]\times{\bf n}\,d\sigma-\dfrac{1}{c}\left\langle\dfrac{\partial{\mathbf{B}}}{\partial t},\varphi\right\rangle

implying that

Γφ(x)[[𝐄(x,t)]]×𝐧𝑑σ=0\int_{\Gamma}\varphi(x)\,[[{\mathbf{E}}(x,t)]]\times{\bf n}\,d\sigma=0

for all test functions φ𝒟(Ω)\varphi\in\mathcal{D}(\Omega) and all tt, therefore (3.5) holds.

Reciprocally, if (3.5) holds we obtain that ×𝐄=1c𝐁t\nabla\times{\mathbf{E}}=-\dfrac{1}{c}\dfrac{\partial{\mathbf{B}}}{\partial t} holds in Ω\Omega in the sense of distributions.

3.1. Compatibility condition

Let us assume that (3.1) holds with vector valued distributions 𝐄,𝐇,𝐃,𝐁,𝐉{\mathbf{E}},{\mathbf{H}},{\mathbf{D}},{\mathbf{B}},{\mathbf{J}} depending on the parameter tt, with 𝐁,𝐃,𝐉{\mathbf{B}},{\mathbf{D}},{\mathbf{J}} also differentiable with respect to this parameter. Hence from the first and second Maxwell equations in (3.1), (2.5), and Proposition 2.3 we have in the distributional sense the continuity equation

(3.6) 0=(×𝐇)=4πc𝐉+1c𝐃t=4πc𝐉+1cρt.0=\nabla\cdot(\nabla\times{\bf H})=\dfrac{4\pi}{c}\nabla\cdot{\bf J}+\dfrac{1}{c}\nabla\cdot\dfrac{\partial{\bf D}}{\partial t}=\dfrac{4\pi}{c}\nabla\cdot{\bf J}+\dfrac{1}{c}\dfrac{\partial\rho}{\partial t}.

When 𝐉{\mathbf{J}} and ρ\rho satisfy the assumptions in Theorem 3.1, equation (3.6) leads to the following compatibility condition between the current 𝐉{\mathbf{J}} and the density ρ\rho:

4πc(𝐉0+νt)+1c(ρ0t+μtt)=0,\dfrac{4\pi}{c}\left(\nabla\cdot{\mathbf{J}}_{0}+\nabla\cdot\nu_{t}\right)+\dfrac{1}{c}\left(\dfrac{\partial\rho_{0}}{\partial t}+\dfrac{\partial\mu_{t}}{\partial t}\right)=0,

in the sense of distributions.

4. Generalized Snell’s law deduced from Maxwell equations

Letting as usual [3, Section 1.1.2] the material or constitutive equations

(4.1) 𝐃=ϵ𝐄,𝐁=μ𝐇,{\mathbf{D}}=\epsilon\,{\mathbf{E}},\qquad{\mathbf{B}}=\mu\,{\mathbf{H}},

we obtain from (3.1)

(M.1) ϵ𝐄\displaystyle\nabla\cdot\epsilon{\mathbf{E}} =4πρ,\displaystyle=4\,\pi\,\rho,\quad
(M.2) μ𝐇\displaystyle\nabla\cdot\mu{\mathbf{H}} =0,\displaystyle=0,\quad
(M.3) ×𝐄\displaystyle\nabla\times{\mathbf{E}} =μc𝐇t,\displaystyle=-\dfrac{\mu}{c}\dfrac{\partial{\mathbf{H}}}{\partial t},\quad
(M.4) ×𝐇\displaystyle\nabla\times{\mathbf{H}} =4πc𝐉+ϵc𝐄t,\displaystyle=\dfrac{4\pi}{c}\,{\mathbf{J}}+\dfrac{\epsilon}{c}\dfrac{\partial{\mathbf{E}}}{\partial t},

where ρ(x,t)\rho(x,t) is the charge density, 𝐉(x,t){\mathbf{J}}(x,t) is the current density vector, 𝐄{\mathbf{E}} is the electric field, 𝐇{\mathbf{H}} is the magnetic field, and ϵ,μ\epsilon,\mu are constants, the permittivity and permeability of the media (isotropic), respectively. If ϵ0,μ0\epsilon_{0},\mu_{0} are the permittivity and permeability of vacuum, then ϵrel=ϵ/ϵ0\epsilon_{\text{rel}}=\epsilon/\epsilon_{0} and , μrel=μ/μ0\mu_{\text{rel}}=\mu/\mu_{0} denote the relative permittivity and relative permeability, respectively, and n=ϵrelμreln=\sqrt{\epsilon_{\text{rel}}\mu_{\text{rel}}} is the refractive index of the media. Since the speed of light in vacuum is c=1/ϵ0μ0c=1/\sqrt{\epsilon_{0}\mu_{0}}, and the phase velocity of light in the media is v=1/ϵμv=1/\sqrt{\epsilon\mu}, then v=c/nv=c/n.

Let Γ\Gamma be the plane x3=0x_{3}=0, and let Ω+\Omega_{+}, Ω\Omega_{-} denote the regions above Γ\Gamma and below Γ\Gamma respectively, with Ω\Omega_{-} filled with medium II and Ω+\Omega_{+} filled with medium IIII. The constants ϵ,μ\epsilon,\mu in the Maxwell system (M.1)–(M.4) may be different in media II and IIII, and they are denoted by ϵ,μ\epsilon_{-},\mu_{-} in medium II, and ϵ+,μ+\epsilon_{+},\mu_{+} in medium IIII. Suppose the incoming incident electric field in media II is a plane wave with the form

(4.2) 𝐄i(x,t)=𝐀ieiω(𝐤ixv1t){\mathbf{E}}_{i}(x,t)={\bf A}_{i}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{i}\cdot x}{v_{1}}-t\right)}

where 𝐤i{\mathbf{k}}_{i} is the incident unit vector, v1v_{1} is the velocity of propagation in medium II, 𝐀i{\bf A}_{i} is a three dimensional constant complex vector, the amplitude, and ω\omega is a constant (the angular frequency). Here x=(x1,x2,x3)x=(x_{1},x_{2},x_{3}). As usual, the Roman numeral i\rm i in the exponentials denotes the unit imaginary number. This wave is defined for x3<0x_{3}<0, i.e., the field is incident to the plane Γ\Gamma from below and defined in Ω\Omega_{-}. This wave strikes the plane Γ\Gamma and it is then transmitted into medium IIII as a nonlinear wave and the ansatz is to assume it has the form

(4.3) 𝐄t(x,t)=𝐀teiω(𝐤txv2+f(x)t){\mathbf{E}}_{t}(x,t)={\bf A}_{t}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{t}\cdot x}{v_{2}}+f(x)-t\right)}

where now 𝐤t{\mathbf{k}}_{t} is the refracted unit vector, v2v_{2} is the velocity of propagation in medium IIII, 𝐀t{\bf A}_{t} is the amplitude, a constant vector, the wave is defined for x3>0x_{3}>0, i.e., on Ω+\Omega_{+}, and f(x)f(x) is a C2C^{2} function defined in a neighborhood of the plane Γ\Gamma. There is also a wave reflected back into medium II that will be assumed to have also a similar form

(4.4) 𝐄r(x,t)=𝐀reiω(𝐤rxv1+f(x)t),{\mathbf{E}}_{r}(x,t)={\bf A}_{r}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot x}{v_{1}}+f(x)-t\right)},

with 𝐀r{\bf A}_{r} a constant vector, 𝐤r{\mathbf{k}}_{r} is the reflected back unit vector, v1v_{1} is the velocity of propagation in medium II, the wave is defined for x3<0x_{3}<0, i.e., on Ω\Omega_{-}. We are assuming that ff depends only on x1,x2x_{1},x_{2}, i.e., the gradient of ff is tangential to the plane Γ\Gamma; we then denote f=(fx1,fx2,0)\nabla f=(f_{x_{1}},f_{x_{2}},0). In addition, and without loss of generality, we assume that f(0)=0f(0)=0, otherwise that simply changes the values of the amplitudes.

PPν=(0,0,1)\nu=(0,0,1)𝐤i,(𝐄i,𝐇i){\mathbf{k}}_{i},\ ({\mathbf{E}}_{i},{\mathbf{H}}_{i})𝐤r,(𝐄r,𝐇r){\mathbf{k}}_{r},\ ({\mathbf{E}}_{r},{\mathbf{H}}_{r})𝐤t,(𝐄t,𝐇t){\mathbf{k}}_{t},\ ({\mathbf{E}}_{t},{\mathbf{H}}_{t})Ω+\Omega_{+}Ω\Omega_{-}medium IIIIϵ+,μ+\epsilon_{+},\mu_{+}medium IIϵ,μ\epsilon_{-},\mu_{-}Γ={x3=0}\Gamma=\{x_{3}=0\}
Figure 2. Reflection and transmission at the planar interface Γ={x3=0}\Gamma=\{x_{3}=0\} separating medium II from medium IIII

The plan of this section is the following:

  1. (1)

    The fields 𝐄i,𝐄t,𝐄r{\mathbf{E}}_{i},{\mathbf{E}}_{t},{\mathbf{E}}_{r} have corresponding magnetic fields 𝐇i,𝐇t,𝐇r{\mathbf{H}}_{i},{\mathbf{H}}_{t},{\mathbf{H}}_{r} so that the Maxwell system (M.1)–(M.4) is satisfied; these are calculated in Section 4.1. These magnetic fields are used in Section 5 to obtain boundary conditions for them.

  2. (2)

    Section 4.2 contains the proof of the main result, Theorem 4.3. The proof uses Theorem 3.1 to obtain the boundary conditions (4.10), (4.11), and (4.15) for the electric field (equations that will be used later in Section 6). As a consequence of these we obtain the generalized Snell law for the first two components of the wave vectors, Equation (4.8). It also contains the statement of Lemma 4.2 used to prove Theorem 4.3 . The proof of this lemma is given in the Appendix 7.

  3. (3)

    In Section 4.3 we deduce from the previous items the generalized Snell law for refraction (1.1) and the generalized law of reflection (1.2).

  4. (4)

    In Section 4.4 we show relationships for the third components of the wave vectors, Corollary 4.4.

  5. (5)

    In Section 4.5 we deduce orthogonality conditions for the amplitudes that are used later in Section 6 to calculate the amplitudes of the transmitted and reflected waves.

We use the following notation throughout the paper

(4.5) 𝐦i=ω𝐤iv1,𝐦r=ω𝐤rv1,𝐦t=ω𝐤tv2,{\mathbf{m}}_{i}=\omega\frac{{\mathbf{k}}_{i}}{v_{1}},\qquad{\mathbf{m}}_{r}=\omega\frac{{\mathbf{k}}_{r}}{v_{1}},\qquad{\mathbf{m}}_{t}=\omega\dfrac{{\mathbf{k}}_{t}}{v_{2}},

and write 𝐦=(m1,m2,m3){\mathbf{m}}_{\ell}=(m_{1}^{\ell},m_{2}^{\ell},m_{3}^{\ell}), with =i,r,t\ell=i,r,t.

4.1. Calculation of the corresponding magnetic fields

The values of these magnetic fields are given in the following lemma.

Lemma 4.1.

Suppose the electric fields 𝐄i,𝐄t,𝐄r{\mathbf{E}}_{i},{\mathbf{E}}_{t},{\mathbf{E}}_{r} are given by (4.2), (4.3), and (4.4), respectively. If the field 𝐇(x,t){\mathbf{H}}^{\prime}(x,t) solves

×(𝐄i+𝐄r)=μc𝐇t\nabla\times\left({\mathbf{E}}_{i}+{\mathbf{E}}_{r}\right)=-\dfrac{\mu_{-}}{c}\dfrac{\partial{\mathbf{H}}^{\prime}}{\partial t}

in Ω\Omega_{-}, and the field 𝐇t(x,t){\mathbf{H}}_{t}(x,t) solves

×𝐄t=μ+c𝐇tt\nabla\times{\mathbf{E}}_{t}=-\dfrac{\mu_{+}}{c}\dfrac{\partial{\mathbf{H}}_{t}}{\partial t}

in Ω+\Omega_{+}, then 𝐇=𝐇i+𝐇r{\mathbf{H}}^{\prime}={\mathbf{H}}_{i}+{\mathbf{H}}_{r} with

𝐇i=cμ𝐄i×𝐤iv1;𝐇r=cμ𝐄r×(𝐤rv1+f(x)),{\mathbf{H}}_{i}=-\dfrac{c}{\mu_{-}}\,{\mathbf{E}}_{i}\times\dfrac{{\mathbf{k}}_{i}}{v_{1}};\quad{\mathbf{H}}_{r}=-\dfrac{c}{\mu_{-}}\,{\mathbf{E}}_{r}\times\left(\dfrac{{\mathbf{k}}_{r}}{v_{1}}+\nabla f(x)\right),

and

𝐇t=cμ+𝐄t×(𝐤tv2+f(x)),{\mathbf{H}}_{t}=-\dfrac{c}{\mu_{+}}\,{\mathbf{E}}_{t}\times\left(\dfrac{{\mathbf{k}}_{t}}{v_{2}}+\nabla f(x)\right),

modulo fields only depending on xx which we assume to be zero. We have denoted f(x)=(fx1(x),fx2(x),0)\nabla f(x)=\left(f_{x_{1}}(x),f_{x_{2}}(x),0\right).

Proof.

Calculation of 𝐇{\mathbf{H}}^{\prime}. We have from (4.2) and (4.4)

×(𝐄i+𝐄r)=iω(𝐀i×𝐤iv1)eiω(𝐤ixv1t)iω𝐀r×(𝐤rv1+f(x))eiω(𝐤rxv1+f(x)t).\nabla\times\left({\mathbf{E}}_{i}+{\mathbf{E}}_{r}\right)=-{\rm i}\,\omega\,\left({\bf A}_{i}\times\dfrac{{\mathbf{k}}_{i}}{v_{1}}\right)\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{i}\cdot x}{v_{1}}-t\right)}-{\rm i}\,\omega\,{\bf A}_{r}\times\left(\dfrac{{\mathbf{k}}_{r}}{v_{1}}+\nabla f(x)\right)\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot x}{v_{1}}+f(x)-t\right)}.

Integrating yields

𝐇\displaystyle{\mathbf{H}}^{\prime} =cμ×(𝐄i+𝐄r)dt\displaystyle=-\dfrac{c}{\mu_{-}}\int\nabla\times\left({\mathbf{E}}_{i}+{\mathbf{E}}_{r}\right)\,dt
=cμ(𝐀i×𝐤iv1)eiω(𝐤ixv1t)cμ𝐀r×(𝐤rv1+f(x))eiω(𝐤rxv1+f(x)t)\displaystyle=-\dfrac{c}{\mu_{-}}\,\left({\bf A}_{i}\times\dfrac{{\mathbf{k}}_{i}}{v_{1}}\right)\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{i}\cdot x}{v_{1}}-t\right)}-\dfrac{c}{\mu_{-}}\,{\bf A}_{r}\times\left(\dfrac{{\mathbf{k}}_{r}}{v_{1}}+\nabla f(x)\right)\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot x}{v_{1}}+f(x)-t\right)}
=cμ𝐄i×𝐤iv1cμ𝐄r×(𝐤rv1+f(x)),\displaystyle=-\dfrac{c}{\mu_{-}}\,{\mathbf{E}}_{i}\times\dfrac{{\mathbf{k}}_{i}}{v_{1}}-\dfrac{c}{\mu_{-}}\,{\mathbf{E}}_{r}\times\left(\dfrac{{\mathbf{k}}_{r}}{v_{1}}+\nabla f(x)\right),

modulo a field only depending on xx which we assume to be zero.

Similarly, the calculation of 𝐇t{\mathbf{H}}_{t} follows by integration using (4.3).

4.2. Main result and the generalized Snell law

In this section, we shall prove Theorem 4.3 showing that the phase function ff in the scattered waves (4.3) and (4.4) is necessarily affine and we prove relationships between the components of the wave vectors 𝐤i,𝐤r{\mathbf{k}}_{i},{\mathbf{k}}_{r} and 𝐤t{\mathbf{k}}_{t} and f\nabla f, that imply the generalized Snell law (1.1) and (1.2). The proof of Theorem 4.3 requires the following lemma whose proof is given in the Appendix 7.

Lemma 4.2.

Suppose that the equation

(4.6) aei𝐦iX+bei(𝐦rX+ψ(X))+cei(𝐦tX+ψ(X))=0a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}+b\,e^{{\rm i}\,\left({\mathbf{m}}_{r}\cdot X+\psi(X)\right)}+c\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}=0

holds for all X=(x1,x2,0)X=(x_{1},x_{2},0), where a,b,ca,b,c are fixed complex constants, 𝐦=(m1,m2,m3){\mathbf{m}}_{\ell}=\left(m_{1}^{\ell},m_{2}^{\ell},m_{3}^{\ell}\right) for =i,r,t\ell=i,r,t, and ψ\psi is a real-valued C2C^{2}-function; we use the notation ψ(X)=ψ(x1,x2)\psi(X)=\psi(x_{1},x_{2}). We have

  1. (i)

    If a0a\neq 0, b0b\neq 0, and c0c\neq 0, then ψ\psi is an affine function and

    mjimjr=ψxj, and mjimjt=ψxj,j=1,2.m_{j}^{i}-m_{j}^{r}=\psi_{x_{j}},\text{ and }m_{j}^{i}-m_{j}^{t}=\psi_{x_{j}},\quad j=1,2.
  2. (ii)

    If a=0a=0, b0b\neq 0, and c0c\neq 0, then mjr=mjtm_{j}^{r}=m_{j}^{t} for j=1,2j=1,2.

  3. (iii)

    If a0a\neq 0, b=0b=0, and c0c\neq 0, then ψ\psi is affine and

    mjimjt=ψxj,j=1,2.m_{j}^{i}-m_{j}^{t}=\psi_{x_{j}},\quad j=1,2.
  4. (iv)

    If a0a\neq 0, b0b\neq 0, and c=0c=0, then ψ\psi is affine and

    mjimjr=ψxj,j=1,2.m_{j}^{i}-m_{j}^{r}=\psi_{x_{j}},\quad j=1,2.

Now, let us proceed to state and the prove the main result of the section.

Theorem 4.3.

Recall the definitions of the fields 𝐄i,𝐄r{\mathbf{E}}_{i},{\mathbf{E}}_{r} and 𝐄t{\mathbf{E}}_{t} from (4.2)–(4.4), and the corresponding magnetic fields 𝐇i,𝐇r{\mathbf{H}}_{i},{\mathbf{H}}_{r} and 𝐇t{\mathbf{H}}_{t} from Lemma 4.1. Let

(4.7) 𝐄(x,t)=𝐄i(x,t)+𝐄r(x,t),𝐇(x,t)=𝐇i(x,t)+𝐇r(x,t),{\mathbf{E}}^{\prime}(x,t)={\mathbf{E}}_{i}(x,t)+{\mathbf{E}}_{r}(x,t),\quad{\mathbf{H}}^{\prime}(x,t)={\mathbf{H}}_{i}(x,t)+{\mathbf{H}}_{r}(x,t),

and define 𝐄(x,t)=χΩ𝐄(x,t)+χΩ+𝐄t(x,t){\mathbf{E}}(x,t)=\chi_{\Omega_{-}}{\mathbf{E}}^{\prime}(x,t)+\chi_{\Omega_{+}}{\mathbf{E}}_{t}(x,t), and 𝐇(x,t)=χΩ𝐇(x,t)+χΩ+𝐇t(x,t){\mathbf{H}}(x,t)=\chi_{\Omega_{-}}{\mathbf{H}}^{\prime}(x,t)+\chi_{\Omega_{+}}{\mathbf{H}}_{t}(x,t).

Then the fields 𝐄,𝐇,𝐄t{\mathbf{E}}^{\prime},{\mathbf{H}}^{\prime},{\mathbf{E}}_{t} and 𝐇t{\mathbf{H}}_{t} satisfy conditions (F1), (F2), and (F3).

If 𝐄{\mathbf{E}} and 𝐇{\mathbf{H}} are distributional solutions to (M.3), and 𝐄{\mathbf{E}} is a distributional solution to (M.1) with ρ\rho non-singular, i.e. ρ\rho is as in Theorem 3.1(b) with μt=0\mu_{t}=0, then the function ff must be affine, i.e., a linear function of x1,x2x_{1},x_{2} plus a constant, and

(4.8) kjiv1kjrv1=fxjandkjiv1kjtv2=fxjj=1,2,\frac{k_{j}^{i}}{v_{1}}-\frac{k_{j}^{r}}{v_{1}}=f_{x_{j}}\quad\text{and}\quad\frac{k_{j}^{i}}{v_{1}}-\frac{k_{j}^{t}}{v_{2}}=f_{x_{j}}\quad\quad j=1,2,

with 𝐤=(k1,k2,k3){\mathbf{k}}_{\ell}=\left(k_{1}^{\ell},k_{2}^{\ell},k_{3}^{\ell}\right) with =i,r,t\ell=i,r,t.

Proof.

The proof uses Lemma 4.2 below and Theorem 3.1.

From the explicit form of the fields, it is clear that 𝐄,𝐇,𝐄t{\mathbf{E}}^{\prime},{\mathbf{H}}^{\prime},{\mathbf{E}}_{t} and 𝐇t{\mathbf{H}}_{t} satisfy conditions (F1), (F2), and (F3). Since we assume that 𝐄{\mathbf{E}} and 𝐇{\mathbf{H}} are distributional solutions to (M.3), it follows that Theorem 3.1, Part (4), is applicable.

Therefore, the jump of the electric field equals

[[𝐄(X,t)]]\displaystyle[[{\mathbf{E}}(X,t)]] =limxX,xΩ+𝐄(x,t)limxX,xΩ𝐄(x,t)\displaystyle=\lim_{x\to X,x\in\Omega_{+}}{\mathbf{E}}(x,t)-\lim_{x\to X,x\in\Omega_{-}}{\mathbf{E}}(x,t)
=𝐀teiω(𝐤tXv2+f(X)t)𝐀ieiω(𝐤iXv1t)𝐀reiω(𝐤rXv1+f(X)t)\displaystyle={\bf A}_{t}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{t}\cdot X}{v_{2}}+f(X)-t\right)}-{\bf A}_{i}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{i}\cdot X}{v_{1}}-t\right)}-{\bf A}_{r}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot X}{v_{1}}+f(X)-t\right)}\,

with X=(x1,x2,0)X=(x_{1},x_{2},0), and from the boundary condition (3.5)

(4.9) (𝐀t×𝐧)eiω(𝐤tXv2+f(X)t)(𝐀i×𝐧)eiω(𝐤iXv1t)(𝐀r×𝐧)eiω(𝐤rXv1+f(X)t)=𝟎,\left({\bf A}_{t}\times{\mathbf{n}}\right)\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{t}\cdot X}{v_{2}}+f(X)-t\right)}-\left({\bf A}_{i}\times{\mathbf{n}}\right)\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{i}\cdot X}{v_{1}}-t\right)}-\left({\bf A}_{r}\times{\mathbf{n}}\right)\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot X}{v_{1}}+f(X)-t\right)}={\bf 0},

for all XΓX\in\Gamma.

If we write the components of A=(A1,A2,A3)A_{\ell}=\left(A_{1}^{\ell},A_{2}^{\ell},A_{3}^{\ell}\right) with =i,r,t\ell=i,r,t, then A×𝐧=(A2,A1,0)A_{\ell}\times{\mathbf{n}}=\left(A_{2}^{\ell},-A_{1}^{\ell},0\right). Also, if we set ψ(X)=ωf(X)\psi(X)=\omega f(X) and recall (4.5), then (4.9) is the system of two scalar equations

(4.10) A2iei(𝐦iX)A2rei(𝐦rX+ψ(X))+A2tei(𝐦tX+ψ(X))=0,-A_{2}^{i}\,e^{{\rm i}\,\left({\mathbf{m}}_{i}\cdot X\right)}-A_{2}^{r}\,e^{{\rm i}\,\left({\mathbf{m}}_{r}\cdot X+\psi(X)\right)}+A_{2}^{t}\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}=0,
(4.11) A1iei(𝐦iX)+A1rei(𝐦rX+ψ(X))A1tei(𝐦tX+ψ(X))=0.A_{1}^{i}\,e^{{\rm i}\,\left({\mathbf{m}}_{i}\cdot X\right)}+A_{1}^{r}\,e^{{\rm i}\,\left({\mathbf{m}}_{r}\cdot X+\psi(X)\right)}-A_{1}^{t}\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}=0.

To prove the desired result we shall use Lemma 4.2. Let us first assume that

(4.12) 𝐀i×𝐧0,𝐀r×𝐧0,and 𝐀t×𝐧0.{\bf A}_{i}\times{\mathbf{n}}\neq 0,\quad{\bf A}_{r}\times{\mathbf{n}}\neq 0,\quad\text{and }{\bf A}_{t}\times{\mathbf{n}}\neq 0.

From (4.12) we have that A20A_{2}^{\ell}\neq 0 or A10A_{1}^{\ell}\neq 0 for =i,r,t\ell=i,r,t. Notice that in (4.10) if one coefficient is different from zero then at least one of the other two must be different from zero; and likewise in (4.11). If in (4.10) A20A_{2}^{\ell}\neq 0 for =i,r,t\ell=i,r,t, then applying Lemma 4.2 (i) it follows that ψ\psi is affine and (4.8) holds. Likewise, if in (4.11) A10A_{1}^{\ell}\neq 0 for =i,r,t\ell=i,r,t, then applying Lemma 4.2 (i) it follows that ψ\psi is affine and (4.8) holds. If in (4.10) A2i0A_{2}^{i}\neq 0, then A2r0A_{2}^{r}\neq 0 or A2t0A_{2}^{t}\neq 0. If A2r0A_{2}^{r}\neq 0 and A2t=0A_{2}^{t}=0, by Lemma 4.2 (iv) we have ψ\psi is affine and mjimjr=ψxjm_{j}^{i}-m_{j}^{r}=\psi_{x_{j}}, j=1,2j=1,2. Since 𝐀t×𝐧0{\bf A}_{t}\times{\mathbf{n}}\neq 0, if A2t=0A_{2}^{t}=0 we then must have A1t0A_{1}^{t}\neq 0 and from (4.11) A1i0A_{1}^{i}\neq 0 or A1r0A_{1}^{r}\neq 0. If A1i0A_{1}^{i}\neq 0 and A1r=0A_{1}^{r}=0, then by Lemma 4.2 (iii) mjimjt=ψxjm_{j}^{i}-m_{j}^{t}=\psi_{x_{j}} for j=1,2j=1,2; so (4.8) follows. On the other hand, if A1i=0A_{1}^{i}=0 and A1r0A_{1}^{r}\neq 0, then by Lemma 4.2 (ii) mjr=mjtm_{j}^{r}=m_{j}^{t} for j=1,2j=1,2 and so also (4.8) follows. In general, all the possibilities for the values of the coefficients with their conclusions are summarized in the following table:

A2iA_{2}^{i} A2rA_{2}^{r} A2tA_{2}^{t} A1iA_{1}^{i} A1rA_{1}^{r} A1tA_{1}^{t} Conclusion
0\neq 0 0\neq 0 0 0 0\neq 0 0\neq 0 𝐦i𝐦r=ψ,{\mathbf{m}}_{i}-{\mathbf{m}}_{r}=\nabla\psi, and 𝐦r=𝐦t{\mathbf{m}}_{r}={\mathbf{m}}_{t} by Lemma 4.2 (iv) (ii)
0 0\neq 0 0\neq 0 0\neq 0 0 0\neq 0 𝐦r=𝐦t{\mathbf{m}}_{r}={\mathbf{m}}_{t} and 𝐦i𝐦t=ψ,{\mathbf{m}}_{i}-{\mathbf{m}}_{t}=\nabla\psi, by Lemma 4.2 (ii) (iii)
0\neq 0 0 0\neq 0 0 0\neq 0 0\neq 0 𝐦i𝐦t=ψ,{\mathbf{m}}_{i}-{\mathbf{m}}_{t}=\nabla\psi, and 𝐦r=𝐦t{\mathbf{m}}_{r}={\mathbf{m}}_{t} by Lemma 4.2 (iii) (ii)
0\neq 0 0 0\neq 0 0\neq 0 0\neq 0 0 𝐦i𝐦t=ψ,{\mathbf{m}}_{i}-{\mathbf{m}}_{t}=\nabla\psi, and 𝐦i𝐦r=ψ{\mathbf{m}}_{i}-{\mathbf{m}}_{r}=\nabla\psi by Lemma 4.2 (iii) (iv)
0 0\neq 0 0\neq 0 0\neq 0 0\neq 0 0 𝐦r=𝐦t,{\mathbf{m}}_{r}={\mathbf{m}}_{t}, and 𝐦i𝐦r=ψ{\mathbf{m}}_{i}-{\mathbf{m}}_{r}=\nabla\psi by Lemma 4.2 (ii) (iv)
0 0\neq 0 0\neq 0 0\neq 0 0 0\neq 0 𝐦r=𝐦t,{\mathbf{m}}_{r}={\mathbf{m}}_{t}, and 𝐦i𝐦t=ψ{\mathbf{m}}_{i}-{\mathbf{m}}_{t}=\nabla\psi by Lemma 4.2 (ii) (iii)

Therefore ψ\psi is affine and (4.8) follows when (4.12) holds since ψ=ωf\psi=\omega f.

It remains to prove (4.8) when (4.12) does not hold. That is, suppose

(4.13) 𝐀i×𝐧=0, or 𝐀r×𝐧=0, or 𝐀t×𝐧=0.{\bf A}_{i}\times{\mathbf{n}}=0,\text{ or }{\bf A}_{r}\times{\mathbf{n}}=0,\text{ or }{\bf A}_{t}\times{\mathbf{n}}=0.

Here we use the constitutive equations (4.1) and Part (1) of Theorem 3.1. Notice that the permittivity constant for Ω\Omega_{-} is ϵ\epsilon_{-} and for Ω+\Omega_{+} is ϵ+\epsilon_{+}. We recall the assumption that the field 𝐃=ϵχΩ(𝐄i+𝐄r)+ϵ+χΩ+𝐄t=ϵχΩ𝐄+ϵ+χΩ+𝐄t{\bf D}=\epsilon_{-}\,\chi_{\Omega_{-}}\left({\bf E}_{i}+{\bf E}_{r}\right)+\epsilon_{+}\,\chi_{\Omega_{+}}{\bf E}_{t}=\epsilon_{-}\,\chi_{\Omega_{-}}{\mathbf{E}}^{\prime}+\epsilon_{+}\,\chi_{\Omega_{+}}{\bf E}_{t} is a distributional solution to the second equation in (3.1) with ρ\rho having singular part equals zero. Then Part (1) of Theorem 3.1 is applicable with μt=0\mu_{t}=0 and we have

(4.14) [[𝐃(X,t)]]𝐧=0,[[{\bf D}(X,t)]]\cdot{\bf n}=0,

where

[[𝐃(X,t)]]=limxX,xΩ+ϵ+𝐄t(x,t)limxX,xΩϵ𝐄(x,t).[[{\bf D}(X,t)]]=\lim_{x\to X,x\in\Omega_{+}}\epsilon_{+}{\mathbf{E}}_{t}(x,t)-\lim_{x\to X,x\in\Omega_{-}}\epsilon_{-}{\mathbf{E}}^{\prime}(x,t).

Since 𝐧=(0,0,1){\bf n}=(0,0,1), we then have from the form of the fields 𝐄t{\mathbf{E}}_{t} and 𝐄{\mathbf{E}}^{\prime} that the equation (4.14) reads (ψ=ωf\psi=\omega f)

(4.15) ϵA3iei𝐦iX+ϵA3rei(𝐦rX+ψ(X))ϵ+A3tei(𝐦tX+ψ(X))=0,\epsilon_{-}\,A_{3}^{i}e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}+\epsilon_{-}\,A_{3}^{r}e^{{\rm i}\,\left({\mathbf{m}}_{r}\cdot X+\psi(X)\right)}-\epsilon_{+}\,A_{3}^{t}e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}=0,

which will be used to deal with the case (4.13). To begin with let us assume 𝐀i×𝐧=0{\bf A}_{i}\times{\mathbf{n}}=0, that is, A1i=0A_{1}^{i}=0 and A2i=0A_{2}^{i}=0. Since 𝐀i0{\bf A}_{i}\neq 0, it follows that A3i0A_{3}^{i}\neq 0. Hence from (4.15) it follows that A3r0A_{3}^{r}\neq 0 or A3t0A_{3}^{t}\neq 0. If A3r0A_{3}^{r}\neq 0 and A3t0A_{3}^{t}\neq 0, then by Lemma 4.2 (i) we get that ψ\psi is affine and (4.8) holds. If A3i0A_{3}^{i}\neq 0, A3r0A_{3}^{r}\neq 0 and A3t=0A_{3}^{t}=0, by Lemma 4.2 (iv) it follows that mjimjr=ψxjm_{j}^{i}-m_{j}^{r}=\psi_{x_{j}} for j=1,2j=1,2. But if A3t=0A_{3}^{t}=0, since the amplitude 𝐀t0{\bf A}_{t}\neq 0, we must have A1t0A_{1}^{t}\neq 0 or A2t0A_{2}^{t}\neq 0. If A1t0A_{1}^{t}\neq 0 and A2t=0A_{2}^{t}=0, then using (4.11) we must have A1r0A_{1}^{r}\neq 0, and by Lemma 4.2 (ii) mjr=mjtm_{j}^{r}=m_{j}^{t} for j=1,2j=1,2 and so (4.8) follows. If A1t=0A_{1}^{t}=0 and A2t0A_{2}^{t}\neq 0, then from (4.10) A2r0A_{2}^{r}\neq 0 so by Lemma 4.2 (ii) mjr=mjtm_{j}^{r}=m_{j}^{t} for j=1,2j=1,2 and so (4.8) follows.

If A3i0A_{3}^{i}\neq 0, A3r=0A_{3}^{r}=0 and A3t0A_{3}^{t}\neq 0, by Lemma 4.2 (iii) it follows that mjimjt=ψxjm_{j}^{i}-m_{j}^{t}=\psi_{x_{j}} for j=1,2j=1,2. But if A3r=0A_{3}^{r}=0, since the amplitude 𝐀r0{\bf A}_{r}\neq 0, we must have A1r0A_{1}^{r}\neq 0 or A2r0A_{2}^{r}\neq 0. If A1r0A_{1}^{r}\neq 0 and A2r=0A_{2}^{r}=0, then using (4.11) we must have A1t0A_{1}^{t}\neq 0, and by Lemma 4.2 (ii) mjr=mjtm_{j}^{r}=m_{j}^{t} for j=1,2j=1,2 and so (4.8) follows. If A1r=0A_{1}^{r}=0 and A2r0A_{2}^{r}\neq 0, then from (4.10) A2t0A_{2}^{t}\neq 0 so by Lemma 4.2 (ii) mjr=mjtm_{j}^{r}=m_{j}^{t} for j=1,2j=1,2 and so again (4.8) follows.

The remaining cases in (4.13) are treated similarly. ∎

4.3. Deduction of the generalized Snell law for a general phase discontinuity

Let us now consider a general phase discontinuity function ϕ\phi defined on the plane x3=0x_{3}=0 and let 𝐄i{\mathbf{E}}_{i} be the incident electric field given by (4.2). For a point PP on the plane x3=0x_{3}=0, we model the scattering of the wave taking into account the value of the gradient of ϕ\phi, in other words, the function ff in (4.3) and (4.4) is chosen to be f(x)=ϕ(P)xf(x)=\nabla\phi(P)\cdot x; x=(x1,x2)x=(x_{1},x_{2}). We will prove in Section 6 that the amplitudes of the scattered waves (4.3) and (4.4) depend on the choice of the function ff and therefore in this case will depend of the point PP. Applying Theorem 4.2 with this choice of ff we then obtain from (4.8) the generalized Snell’s law for refraction (1.1) and the generalized law of reflection (1.2). In fact, since ni=c/vin_{i}=c/v_{i}, from (4.8) we have n1kjin2kjt=cfxjn_{1}k_{j}^{i}-n_{2}k_{j}^{t}=cf_{x_{j}} for j=1,2j=1,2 and since 𝐧=(0,0,1){\mathbf{n}}=(0,0,1) taking λ=n1k3in2k3t\lambda=n_{1}k_{3}^{i}-n_{2}k_{3}^{t}, (1.1) follows with ff replaced by cfcf. Similarly, (1.2) follows with λ=n1k3in1k3r\lambda^{\prime}=n_{1}k_{3}^{i}-n_{1}k_{3}^{r}.

We can now extend this argument as follows. Suppose we take a finite number of points P1,,PNP_{1},\cdots,P_{N} on the plane x3=0x_{3}=0, and for each point PjP_{j} we choose the phase function ϕ(Pj)x\nabla\phi(P_{j})\cdot x. Each of these phases gives rise to a transmitted and a reflected back waves. Then by superposition, the scattered waves for all the points PjP_{j} will have the form

j=1N𝐀t(Pj)eiω(𝐤txv2+ϕ(Pj)xt),\sum_{j=1}^{N}{\bf A}_{t}(P_{j})\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{t}\cdot x}{v_{2}}+\nabla\phi(P_{j})\cdot x-t\right)},

for the transmitted wave and

j=1N𝐀r(Pj)eiω(𝐤rxv1+ϕ(Pj)xt)\sum_{j=1}^{N}{\bf A}_{r}(P_{j})\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot x}{v_{1}}+\nabla\phi(P_{j})\cdot x-t\right)}

for the wave reflected back.

4.4. Calculation of the third components of the wave vectors

Recalling the notation (4.5), and from (4.8) we have

mjimjr=ωfxj,mjimjt=ωfxjj=1,2.m_{j}^{i}-m_{j}^{r}=\omega f_{x_{j}},\quad m_{j}^{i}-m_{j}^{t}=\omega f_{x_{j}}\qquad j=1,2.

The following corollary, shows formulas for the third component m3m_{3}^{\ell} for =r,t\ell=r,t as a function of m1im_{1}^{i}, m2im_{2}^{i} and ff.

Corollary 4.4.

Under the assumptions of Theorem 4.3, and if

(4.16) (m1iωfx1)2+(m2iωfx2)2min{ωv1,ωv2},\sqrt{\left(m_{1}^{i}-\omega f_{x_{1}}\right)^{2}+\left(m_{2}^{i}-\omega f_{x_{2}}\right)^{2}}\leq\min\left\{\frac{\omega}{v_{1}},\frac{\omega}{v_{2}}\right\},

then

(4.17) m3r=(ωv1)2(m1iωfx1)2(m2iωfx2)2\displaystyle m_{3}^{r}=-\sqrt{\left(\frac{\omega}{v_{1}}\right)^{2}-\left(m_{1}^{i}-\omega f_{x_{1}}\right)^{2}-\left(m_{2}^{i}-\omega f_{x_{2}}\right)^{2}}
(4.18) m3t=(ωv2)2(m1iωfx1)2(m2iωfx2)2.\displaystyle m_{3}^{t}=\sqrt{\left(\frac{\omega}{v_{2}}\right)^{2}-\left(m_{1}^{i}-\omega f_{x_{1}}\right)^{2}-\left(m_{2}^{i}-\omega f_{x_{2}}\right)^{2}}.
Proof.

From (4.8)

(4.19) 𝐦i𝐦r=λ𝐧+ω(fx1,fx2,0),{\mathbf{m}}_{i}-{\mathbf{m}}_{r}=\lambda\,{\mathbf{n}}+\omega\left(f_{x_{1}},f_{x_{2}},0\right),

where 𝐧{\bf n} is the vertical unit direction, and λ=m3im3r\lambda=m_{3}^{i}-m_{3}^{r}. Dotting (4.19) with 𝐦i{\mathbf{m}}_{i} and with 𝐦r{\mathbf{m}}_{r} yields

𝐦i𝐦i𝐦r𝐦i\displaystyle{\mathbf{m}}_{i}\cdot{\mathbf{m}}_{i}-{\mathbf{m}}_{r}\cdot{\mathbf{m}}_{i} =λm3i+ω(fx1,fx2,0)𝐦i\displaystyle=\lambda m_{3}^{i}+\omega\left(f_{x_{1}},f_{x_{2}},0\right)\cdot{\mathbf{m}}_{i}
𝐦i𝐦r𝐦r𝐦r\displaystyle{\mathbf{m}}_{i}\cdot{\mathbf{m}}_{r}-{\mathbf{m}}_{r}\cdot{\mathbf{m}}_{r} =λm3r+ω(fx1,fx2,0)𝐦r,\displaystyle=\lambda m_{3}^{r}+\omega\left(f_{x_{1}},f_{x_{2}},0\right)\cdot{\mathbf{m}}_{r},

and adding these equations, we obtain that

|𝐦i|2|𝐦r|2=λ(m3i+m3r)+ω((m1i+m1r)fx1+(m2i+m2r)fx2).|{\mathbf{m}}_{i}|^{2}-|{\mathbf{m}}_{r}|^{2}=\lambda\,(m_{3}^{i}+m_{3}^{r})+\omega\left((m_{1}^{i}+m_{1}^{r})f_{x_{1}}+(m_{2}^{i}+m_{2}^{r})f_{x_{2}}\right).

Since |𝐦i|2=|𝐦r|2=ω2/v12|{\mathbf{m}}_{i}|^{2}=|{\mathbf{m}}_{r}|^{2}=\omega^{2}/v_{1}^{2}, it follows that

(4.20) λ(m3i+m3r)+ω((m1i+m1r)fx1+(m2i+m2r)fx2)=0.\lambda\,\left(m_{3}^{i}+m_{3}^{r}\right)+\omega\left((m_{1}^{i}+m_{1}^{r})f_{x_{1}}+(m_{2}^{i}+m_{2}^{r})f_{x_{2}}\right)=0.

Hence, from (4.19)

(m3i)2(m3r)2+ω((m1i+m1r)fx1+(m2i+m2r)fx2)=0.\left(m_{3}^{i}\right)^{2}-\left(m_{3}^{r}\right)^{2}+\omega\left((m_{1}^{i}+m_{1}^{r})f_{x_{1}}+(m_{2}^{i}+m_{2}^{r})f_{x_{2}}\right)=0.

Since 𝐤r{\mathbf{k}}_{r} is the unit direction of the ray reflected back in medium II, we have m3r=ωv1k3r<0m_{3}^{r}=\dfrac{\omega}{v_{1}}k_{3}^{r}<0 and so solving for m3rm_{3}^{r} gives

m3r=(m3i)2+ω((m1i+m1r)fx1+(m2i+m2r)fx2).m_{3}^{r}=-\sqrt{\left(m_{3}^{i}\right)^{2}+\omega\left((m_{1}^{i}+m_{1}^{r})f_{x_{1}}+(m_{2}^{i}+m_{2}^{r})f_{x_{2}}\right)}.

Since 𝐤i{\mathbf{k}}_{i} is a unit vector with k3i>0k_{3}^{i}>0, it follows that m3i=(ω/v1)2(m1i)2(m2i)2m_{3}^{i}=\sqrt{\left(\omega/v_{1}\right)^{2}-(m_{1}^{i})^{2}-(m_{2}^{i})^{2}} and from the fact that mjr=mjiωfxjm_{j}^{r}=m_{j}^{i}-\omega f_{x_{j}} for j=1,2j=1,2 we get

m3r\displaystyle m_{3}^{r} =(ωv1)2(m1i)2(m2i)2+ω((2m1iωfx1)fx1+((2m2iωfx2)fx2)CLOSE\displaystyle=-\sqrt{\left(\frac{\omega}{v_{1}}\right)^{2}-(m_{1}^{i})^{2}-(m_{2}^{i})^{2}+\omega\left((2m_{1}^{i}-\omega f_{x_{1}})f_{x_{1}}+((2m_{2}^{i}-\omega f_{x_{2}})f_{x_{2}}\right)}
=(ωv1)2(m1iωfx1)2(m2iωfx2)2,\displaystyle=-\sqrt{\left(\frac{\omega}{v_{1}}\right)^{2}-\left(m_{1}^{i}-\omega f_{x_{1}}\right)^{2}-\left(m_{2}^{i}-\omega f_{x_{2}}\right)^{2}},

which proves (4.17).

To prove (4.18), we proceed similarly using (4.8) and that 𝐦t=ωv2𝐤t{\mathbf{m}}_{t}=\dfrac{\omega}{v_{2}}{\mathbf{k}}_{t}, |𝐤t|=1|{\mathbf{k}}_{t}|=1, with m3t>0m_{3}^{t}>0. ∎

Remark 4.5.

In the standard case, i.e., when f=0f=0, (4.16) obviously reads (m1i)2+(m2i)2min{ω/v1,ω/v2}\sqrt{(m_{1}^{i})^{2}+(m_{2}^{i})^{2}}\leq\min\left\{\omega/v_{1},\omega/v_{2}\right\}. In particular, when the refractive index of medium II is smaller than the one for medium IIII, that is, when v1>v2v_{1}>v_{2}, this always happens since |𝐦i|=ω/v1|{\mathbf{m}}_{i}|=\omega/v_{1}. On the other hand, if v1<v2v_{1}<v_{2}, given an incident wave satisfying (4.16) to avoid total internal reflection, the third component must satisfy

𝐤i𝐧=v1ωm3i=v1ω(ωv1)2(m1i)2(m2i)2v1ω(ωv1)2(ωv2)2=1(v1v2)2.{\mathbf{k}}_{i}\cdot{\bf n}=\dfrac{v_{1}}{\omega}m_{3}^{i}=\dfrac{v_{1}}{\omega}\sqrt{\left(\dfrac{\omega}{v_{1}}\right)^{2}-(m_{1}^{i})^{2}-(m_{2}^{i})^{2}}\geq\dfrac{v_{1}}{\omega}\sqrt{\left(\dfrac{\omega}{v_{1}}\right)^{2}-\left(\dfrac{\omega}{v_{2}}\right)^{2}}=\sqrt{1-\left(\dfrac{v_{1}}{v_{2}}\right)^{2}}.

This condition agrees with the one obtained for the standard Snell’s law, see [6, Section 2]. On the other hand, when f0f\neq 0, the compatibility conditions for 𝐦i{\mathbf{m}}_{i} and ff in (4.16) must be satisfied in order to have reflected and transmitted waves.

We also remark that from (4.17) and (4.18) the following relation between the third components of 𝐦r{\mathbf{m}}_{r} and 𝐦t{\mathbf{m}}_{t} holds:

(4.21) m3t=ω2/v22ω2/v12+(m3r)2.m_{3}^{t}=\sqrt{\omega^{2}/v_{2}^{2}-\omega^{2}/v_{1}^{2}+\left(m_{3}^{r}\right)^{2}}.

4.5. Orthogonality conditions for the amplitudes

The following conditions must be satisfied by the amplitudes, which will be utilized in Section 6.

Lemma 4.6.

Recall from (4.7) the definitions of 𝐄{\mathbf{E}}^{\prime} and 𝐇{\mathbf{H}}^{\prime} and the fields 𝐄(x,t)=χΩ𝐄(x,t)+χΩ+𝐄t(x,t){\mathbf{E}}(x,t)=\chi_{\Omega_{-}}{\mathbf{E}}^{\prime}(x,t)+\chi_{\Omega_{+}}{\mathbf{E}}_{t}(x,t), and 𝐇(x,t)=χΩ𝐇(x,t)+χΩ+𝐇t(x,t){\mathbf{H}}(x,t)=\chi_{\Omega_{-}}{\mathbf{H}}^{\prime}(x,t)+\chi_{\Omega_{+}}{\mathbf{H}}_{t}(x,t).

If 𝐄{\mathbf{E}} and 𝐇{\mathbf{H}} are distributional solutions to (M.3), and 𝐄{\mathbf{E}} is a distributional solution to (M.1) with ρ\rho non-singular, then the amplitudes satisfy the following orthogonality conditions

(4.22) A1im1i+A2im2i+A3im3i=0,A_{1}^{i}m_{1}^{i}+A_{2}^{i}m_{2}^{i}+A_{3}^{i}m_{3}^{i}=0,
(4.23) A1rm1i+A2rm2i+A3rm3r=0,A_{1}^{r}m_{1}^{i}+A_{2}^{r}m_{2}^{i}+A_{3}^{r}m_{3}^{r}=0,

and

(4.24) A1tm1i+A2tm2i+A3tm3t=0.A_{1}^{t}m_{1}^{i}+A_{2}^{t}m_{2}^{i}+A_{3}^{t}m_{3}^{t}=0.
Proof.

From Theorem 4.3, (4.8) holds and from the form of the fields (4.2), (4.3), (4.4), and the notation (4.5) it follows that

𝐄i(x,t)\displaystyle{\mathbf{E}}_{i}(x,t) =𝐀iei(m1ix1+m2ix2+m3ix3ωt),𝐄r(x,t)=𝐀rei(m1ix1+m2ix2+m3rx3ωt)\displaystyle={\bf A}_{i}e^{{\rm i}\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}+m_{3}^{i}x_{3}-\omega\,t\right)},\quad{\mathbf{E}}_{r}(x,t)={\bf A}_{r}e^{{\rm i}\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}+m_{3}^{r}x_{3}-\omega\,t\right)}
𝐄t(x,t)\displaystyle{\mathbf{E}}_{t}(x,t) =𝐀tei(m1ix1+m2ix2+m3tx3ωt).\displaystyle={\bf A}_{t}e^{{\rm i}\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}+m_{3}^{t}x_{3}-\omega\,t\right)}.

Since 𝐄{\mathbf{E}} is a distributional solution to (M.1), it follows that 𝐄{\mathbf{E}}^{\prime} satisfies (M.1) pointwise in Ω\Omega_{-} and 𝐄t{\mathbf{E}}_{t} satisfies (M.1) pointwise in Ω+\Omega_{+}. We then have for x3<0x_{3}<0 that

0\displaystyle 0 =div𝐄=div𝐄i+div𝐄r\displaystyle=\text{\rm div}\,{\mathbf{E}}^{\prime}=\text{\rm div}\,{\mathbf{E}}_{i}+\text{\rm div}\,{\mathbf{E}}_{r}
=i(m1i,m2i,m3i)𝐀iei(m1ix1+m2ix2+m3ix3ωt)+i(m1i,m2i,m3r)𝐀rei(m1ix1+m2ix2+m3rx3ωt)\displaystyle={\rm i}\,\left(m_{1}^{i},m_{2}^{i},m_{3}^{i}\right)\cdot{\bf A}_{i}\,e^{{\rm i}\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}+m_{3}^{i}x_{3}-\omega\,t\right)}+{\rm i}\,\left(m_{1}^{i},m_{2}^{i},m_{3}^{r}\right)\cdot{\bf A}_{r}\,e^{{\rm i}\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}+m_{3}^{r}x_{3}-\omega\,t\right)}
=iei(m1ix1+m2ix2ωt)((m1i,m2i,m3i)𝐀ieim3ix3+(m1i,m2i,m3r)𝐀reim3rx3)\displaystyle={\rm i}\,e^{{\rm i}\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}-\omega\,t\right)}\left(\left(m_{1}^{i},m_{2}^{i},m_{3}^{i}\right)\cdot{\bf A}_{i}\,e^{{\rm i}m_{3}^{i}x_{3}}+\left(m_{1}^{i},m_{2}^{i},m_{3}^{r}\right)\cdot{\bf A}_{r}\,e^{{\rm i}m_{3}^{r}x_{3}}\right)

which implies

(m1i,m2i,m3i)𝐀ieim3ix3+(m1i,m2i,m3r)𝐀reim3rx3=0\left(m_{1}^{i},m_{2}^{i},m_{3}^{i}\right)\cdot{\bf A}_{i}\,e^{{\rm i}\,m_{3}^{i}x_{3}}+\left(m_{1}^{i},m_{2}^{i},m_{3}^{r}\right)\cdot{\bf A}_{r}\,e^{{\rm i}\,m_{3}^{r}x_{3}}=0

for all x3<0x_{3}<0. Since m3i>0m_{3}^{i}>0 and m3r<0m_{3}^{r}<0, the exponentials in the last identity are linearly independent and therefore the coefficients must be zero, that is, (4.22) and (4.23) follow.

Since div𝐄t=0\text{\rm div}\,{\mathbf{E}}_{t}=0 for x3>0x_{3}>0, (4.24) also follows.

5. Boundary conditions for the magnetic fields

In this section, we derive the boundary conditions for the magnetic fields presented in Lemma 4.1 from Theorem 3.1. These boundary conditions will be utilized in Section 6 in the calculation of the amplitudes.

Proposition 5.1.

Under the assumptions of Theorem 4.3, if 𝐄{\mathbf{E}} and 𝐇{\mathbf{H}} are solutions to (M.4), with current density 𝐉{\bf J} satisfying the assumptions in Theorem 3.1 with νt=0\nu_{t}=0, then

(5.1) (1/μ+)(A3tm1im3tA1t)+(1/μ)(A3im1im3iA1i+A3rm1im3rA1r)\displaystyle-(1/\mu_{+})\left(A_{3}^{t}m_{1}^{i}-m_{3}^{t}A_{1}^{t}\right)+(1/\mu_{-})\left(A_{3}^{i}m_{1}^{i}-m_{3}^{i}A_{1}^{i}+A_{3}^{r}m_{1}^{i}-m_{3}^{r}A_{1}^{r}\right) =0\displaystyle=0
(5.2) (1/μ+)(A3tm2im3tA2t)+(1/μ)(A3im2im3iA2i+A3rm2im3rA2r)\displaystyle-(1/\mu_{+})\left(A_{3}^{t}m_{2}^{i}-m_{3}^{t}A_{2}^{t}\right)+(1/\mu_{-})\left(A_{3}^{i}m_{2}^{i}-m_{3}^{i}A_{2}^{i}+A_{3}^{r}m_{2}^{i}-m_{3}^{r}A_{2}^{r}\right) =0.\displaystyle=0.
Proof.

From (4.1) we recall that 𝐃=ϵ𝐄{\mathbf{D}}=\epsilon_{-}\,{\mathbf{E}} in Ω\Omega_{-}, 𝐃=ϵ+𝐄{\mathbf{D}}=\epsilon_{+}\,{\mathbf{E}} in Ω+\Omega_{+}, and 𝐁=μ𝐇{\mathbf{B}}=\mu_{-}\,{\mathbf{H}} in Ω\Omega_{-}, 𝐁=μ+𝐇{\mathbf{B}}=\mu_{+}\,{\mathbf{H}} in Ω+\Omega_{+}. Since 𝐉{\mathbf{J}} has not a singular part, then Theorem 3.1 Part (3) is applicable and we get that

(5.3) [[𝐇(X,t)]]×𝐧(X)=0[[{\mathbf{H}}(X,t)]]\times{\mathbf{n}}(X)=0

for XX in the interface plane Γ={x3=0}\Gamma=\{x_{3}=0\}.

From the expression of the electric fields in (4.2), (4.3), (4.4), and the corresponding magnetic fields obtained in Lemma 4.1, we have that for every X=(x1,x2,0)ΓX=(x_{1},x_{2},0)\in\Gamma

limxX,xΩ𝐇(x,t)\displaystyle\lim_{x\to X,x\in\Omega_{-}}{\mathbf{H}}^{\prime}(x,t) =cμ(𝐀i×𝐤iv1eiω(𝐤iXv1t)+𝐀r×(𝐤rv1+f(X))eiω(𝐤rXv1+f(X)t))\displaystyle=-\dfrac{c}{\mu_{-}}\left({\bf A}_{i}\times\frac{{\mathbf{k}}_{i}}{v_{1}}\,\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{i}\cdot X}{v_{1}}-t\right)}+{\bf A}_{r}\times\left(\frac{{\mathbf{k}}_{r}}{v_{1}}+\nabla f(X)\right)\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot X}{v_{1}}+f(X)-t\right)}\right)
limxX,xΩ+𝐇t(x,t)\displaystyle\lim_{x\to X,x\in\Omega_{+}}{\mathbf{H}}_{t}(x,t) =cμ+𝐀t×(𝐤tv2+f(X))eiω(𝐤tXv2+f(X)t),\displaystyle=-\dfrac{c}{\mu_{+}}\,{\bf A}_{t}\times\left(\dfrac{{\mathbf{k}}_{t}}{v_{2}}+\nabla f(X)\right)\,e^{{\rm i}\omega\left(\frac{{\mathbf{k}}_{t}\cdot X}{v_{2}}+f(X)-t\right)},

where f(X)=(fx1,fx2,0)\nabla f(X)=\left(f_{x_{1}},f_{x_{2}},0\right). Substituting these into (5.3), we get

0\displaystyle 0 =cμ+(𝐀t×(𝐤tv2+f(X)))×𝐧eiω(𝐤tXv2+f(X)t)\displaystyle=-\dfrac{c}{\mu_{+}}\,\left({\bf A}_{t}\times\left(\dfrac{{\mathbf{k}}_{t}}{v_{2}}+\nabla f(X)\right)\right)\times{\mathbf{n}}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{t}\cdot X}{v_{2}}+f(X)-t\right)}
+cμ((𝐀i×𝐤iv1)×𝐧eiω(𝐤iXv1t)+(𝐀r×(𝐤rv1+f(X)))×𝐧eiω(𝐤rXv1+f(X)t)).\displaystyle\qquad+\dfrac{c}{\mu_{-}}\,\left(\left({\bf A}_{i}\times\frac{{\mathbf{k}}_{i}}{v_{1}}\right)\times{\mathbf{n}}\,\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{i}\cdot X}{v_{1}}-t\right)}+\left({\bf A}_{r}\times\left(\frac{{\mathbf{k}}_{r}}{v_{1}}+\nabla f(X)\right)\right)\times{\mathbf{n}}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot X}{v_{1}}+f(X)-t\right)}\right).

Then from (4.8)

cμ+(𝐀t×(ki1v1,ki2v1,kt3v2))×𝐧eiω(𝐤rXv1+f(X))\displaystyle-\dfrac{c}{\mu_{+}}\,\left({\bf A}_{t}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{t}^{3}}{v_{2}}\right)\right)\times{\mathbf{n}}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot X}{v_{1}}+f(X)\right)}
+cμ((𝐀i×(ki1v1,ki2v1,ki3v1))×𝐧eiω(𝐤rXv1+f(X)X)+(𝐀r×(ki1v1,ki2v1,kr3v2))×𝐧eiω(𝐤rXv1+f(X)))=0.\displaystyle\quad+\dfrac{c}{\mu_{-}}\,\left(\left({\bf A}_{i}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{i}^{3}}{v_{1}}\right)\right)\times{\mathbf{n}}\,\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot X}{v_{1}}+\nabla f(X)\cdot X\right)}+\left({\bf A}_{r}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{r}^{3}}{v_{2}}\right)\right)\times{\mathbf{n}}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot X}{v_{1}}+f(X)\right)}\right)=0.

From Theorem 4.3, f(X)f(X) is affine, and since f(0)=0f(0)=0 we have f(X)=f(X)Xf(X)=\nabla f(X)\cdot X. So canceling the exponential and the constant cc in the last equation we obtain

(5.4) 1μ+(𝐀t×(ki1v1,ki2v1,kt3v2))×𝐧+1μ((𝐀i×(ki1v1,ki2v1,ki3v1))×𝐧+(𝐀r×(ki1v1,ki2v1,kr3v2))×𝐧)=0.-\dfrac{1}{\mu_{+}}\,\left({\bf A}_{t}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{t}^{3}}{v_{2}}\right)\right)\times{\mathbf{n}}+\dfrac{1}{\mu_{-}}\,\left(\left({\bf A}_{i}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{i}^{3}}{v_{1}}\right)\right)\times{\mathbf{n}}+\left({\bf A}_{r}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{r}^{3}}{v_{2}}\right)\right)\times{\mathbf{n}}\right)=0.

Let us calculate the triple cross products, we use the formula (a×b)×c=b(ca)a(bc)(a\times b)\times c=b(c\cdot a)-a(b\cdot c) and obtain

(𝐀t×(ki1v1,ki2v1,kt3v2))×𝐧\displaystyle\left({\bf A}_{t}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{t}^{3}}{v_{2}}\right)\right)\times{\mathbf{n}} =(𝐀t𝐧)(ki1v1,ki2v1,kt3v2)((ki1v1,ki2v1,kt3v2)𝐧)𝐀t\displaystyle=\left({\bf A}_{t}\cdot{\mathbf{n}}\right)\,\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{t}^{3}}{v_{2}}\right)-\left(\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{t}^{3}}{v_{2}}\right)\cdot{\mathbf{n}}\right)\,{\bf A}_{t}
=(A3tk1iv1k3tv2A1t,A3tk2iv1k3tv2A2t,0)\displaystyle=\left(A_{3}^{t}\frac{k_{1}^{i}}{v_{1}}-\frac{k_{3}^{t}}{v_{2}}A_{1}^{t},A_{3}^{t}\frac{k_{2}^{i}}{v_{1}}-\frac{k_{3}^{t}}{v_{2}}A_{2}^{t},0\right)
(𝐀r×(ki1v1,ki2v1,kr3v2))×𝐧\displaystyle\left({\bf A}_{r}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{r}^{3}}{v_{2}}\right)\right)\times{\mathbf{n}} =(A3rk1iv1k3rv1A1r,A3rk2iv1k3rv1A2r,0)\displaystyle=\left(A_{3}^{r}\frac{k_{1}^{i}}{v_{1}}-\frac{k_{3}^{r}}{v_{1}}A_{1}^{r},A_{3}^{r}\frac{k_{2}^{i}}{v_{1}}-\frac{k_{3}^{r}}{v_{1}}A_{2}^{r},0\right)
(𝐀i×(ki1v1,ki2v1,ki3v1))×𝐧\displaystyle\left({\bf A}_{i}\times\left(\dfrac{k_{i}^{1}}{v_{1}},\dfrac{k_{i}^{2}}{v_{1}},\dfrac{k_{i}^{3}}{v_{1}}\right)\right)\times{\mathbf{n}} =(A3ik1iv1k3iv1A1i,A3ik2iv1k3iv1A2i,0).\displaystyle=\left(A_{3}^{i}\frac{k_{1}^{i}}{v_{1}}-\frac{k_{3}^{i}}{v_{1}}A_{1}^{i},A_{3}^{i}\frac{k_{2}^{i}}{v_{1}}-\frac{k_{3}^{i}}{v_{1}}A_{2}^{i},0\right).

Replacing the obtained formulas above in (5.4), and using the notation (4.5), equations (5.1) and (5.2) follow. ∎

Remark 5.2.

We observe that analyzing the boundary condition (3.3) does not provide any additional information. Specifically, assume that the magnetic field 𝐇{\bf H} presented in Theorem 4.3 is a distributional solution to (M.2). The jump on 𝐁{\mathbf{B}} is given by

[[𝐁(X,t)]]=limxX,xΩ+μ+𝐇t(x,t)limxX,xΩμ𝐇(x,t),XΓ,[[{\mathbf{B}}(X,t)]]=\lim_{x\to X,x\in\Omega_{+}}\mu_{+}{\mathbf{H}}_{t}(x,t)-\lim_{x\to X,x\in\Omega_{-}}\mu_{-}{\mathbf{H}}^{\prime}(x,t),\quad X\in\Gamma,

and so from Lemma 4.1 and (3.3)

[[𝐁(X,t)]]𝐧\displaystyle[[{\mathbf{B}}(X,t)]]\cdot{\mathbf{n}} =c(𝐀t×(𝐤tv2+f(X)))𝐧eiω(𝐤tXv2+f(X)t)\displaystyle=-c\,\left({\bf A}_{t}\times\left(\dfrac{{\mathbf{k}}_{t}}{v_{2}}+\nabla f(X)\right)\right)\cdot{\mathbf{n}}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{t}\cdot X}{v_{2}}+f(X)-t\right)}
+c((𝐀i×𝐤iv1)𝐧eiω(𝐤iXv1t)+(𝐀r×(𝐤rv1+f(X)))𝐧eiω(𝐤rXv1+f(X)t))=0.\displaystyle\qquad+c\,\left(\left({\bf A}_{i}\times\frac{{\mathbf{k}}_{i}}{v_{1}}\right)\cdot{\mathbf{n}}\,\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{i}\cdot X}{v_{1}}-t\right)}+\left({\bf A}_{r}\times\left(\frac{{\mathbf{k}}_{r}}{v_{1}}+\nabla f(X)\right)\right)\cdot{\mathbf{n}}\,e^{{\rm i}\,\omega\left(\frac{{\mathbf{k}}_{r}\cdot X}{v_{1}}+f(X)-t\right)}\right)=0.

As in the proof of Proposition 5.1, the exponentials are all equal and so cancelling them yields

(𝐀t×(𝐤tv2+f(X)))𝐧+(𝐀i×𝐤iv1)𝐧+(𝐀r×(𝐤rv1+f(X)))𝐧=0.-\left({\bf A}_{t}\times\left(\dfrac{{\mathbf{k}}_{t}}{v_{2}}+\nabla f(X)\right)\right)\cdot{\mathbf{n}}+\left({\bf A}_{i}\times\frac{{\mathbf{k}}_{i}}{v_{1}}\right)\cdot{\mathbf{n}}+\left({\bf A}_{r}\times\left(\frac{{\mathbf{k}}_{r}}{v_{1}}+\nabla f(X)\right)\right)\cdot{\mathbf{n}}=0.

From the triple product formula a(b×c)=b(c×a)a\cdot(b\times c)=b\cdot(c\times a) and (4.8), it follows that

0\displaystyle 0 =𝐀t((k1iv1,k2iv1,k3tv2)×𝐧)+𝐀i((k1iv1,k2iv1,k3iv1)×𝐧)+𝐀r((k1iv1,k2iv1,k3rv1)×𝐧)\displaystyle=-{\bf A}_{t}\cdot\left(\left(\dfrac{k_{1}^{i}}{v_{1}},\dfrac{k_{2}^{i}}{v_{1}},\dfrac{k_{3}^{t}}{v_{2}}\right)\times{\mathbf{n}}\right)+{\bf A}_{i}\cdot\left(\left(\frac{k_{1}^{i}}{v_{1}},\frac{k_{2}^{i}}{v_{1}},\frac{k_{3}^{i}}{v_{1}}\right)\times{\mathbf{n}}\right)+{\bf A}_{r}\cdot\left(\left(\frac{k_{1}^{i}}{v_{1}},\frac{k_{2}^{i}}{v_{1}},\frac{k_{3}^{r}}{v_{1}}\right)\times{\mathbf{n}}\right)
=𝐀t(k2iv1,k1iv1,0)+𝐀i(k2iv1,k1iv1,0)+𝐀r(k2iv1,k1iv1,0)\displaystyle=-{\bf A}_{t}\cdot\left(\frac{k_{2}^{i}}{v_{1}},-\frac{k_{1}^{i}}{v_{1}},0\right)+{\bf A}_{i}\cdot\left(\frac{k_{2}^{i}}{v_{1}},-\frac{k_{1}^{i}}{v_{1}},0\right)+{\bf A}_{r}\cdot\left(\frac{k_{2}^{i}}{v_{1}},-\frac{k_{1}^{i}}{v_{1}},0\right)
=(𝐀t+𝐀i+𝐀r)(k2iv1,k1iv1,0)\displaystyle=\left(-{\bf A}_{t}+{\bf A}_{i}+{\bf A}_{r}\right)\left(\frac{k_{2}^{i}}{v_{1}},-\frac{k_{1}^{i}}{v_{1}},0\right)

which written in terms of mm’s is

(5.5) m2i(A1t+A1i+A1r)m1i(A2t+A2i+A2r)=0.m_{2}^{i}\,\left(-A_{1}^{t}+A_{1}^{i}+A_{1}^{r}\right)-m_{1}^{i}\,\left(-A_{2}^{t}+A_{2}^{i}+A_{2}^{r}\right)=0.

From equations (4.10) and (4.11), equation (5.5) is satisfied. Consequently, the boundary condition (3.3) does not provide any additional equations for the amplitudes.

6. Calculation of the amplitude coefficients

Recall these amplitudes are 𝐀i=(A1i,A2i,A3i),𝐀r=(A1r,A2r,A3r){\bf A}_{i}=(A_{1}^{i},A_{2}^{i},A_{3}^{i}),{\bf A}_{r}=(A_{1}^{r},A_{2}^{r},A_{3}^{r}), and 𝐀t=(A1t,A2t,A3t){\bf A}_{t}=(A_{1}^{t},A_{2}^{t},A_{3}^{t}), where the unknowns are 𝐀r{\bf A}_{r} and 𝐀t{\bf A}_{t}. The purpose of the section is to find explicit formulas for 𝐀r{\bf A}_{r} and 𝐀t{\bf A}_{t} in terms of 𝐀i{\bf A}_{i} and the wave vectors. Listing all the relationships obtained for the amplitudes in a table we get

A1rA2rA3rA1tA2tA3tA1iA2iA3iFrom equation100100100(4.11)010010010(4.10)00ϵ00ϵ+00ϵ(4.15)m3r/μ0m1i/μm3t/μ+0m1i/μ+m3i/μ0m1i/μ(5.1)0m3r/μm2i/μ0m3t/μ+m2i/μ+0m3i/μm2i/μ(5.2)000000m1im2im3i(4.22)m1im2im3r000000(4.23)000m1im2im3t000(4.24).\begin{matrix}A_{1}^{r}&A_{2}^{r}&A_{3}^{r}&A_{1}^{t}&A_{2}^{t}&A_{3}^{t}&A_{1}^{i}&A_{2}^{i}&A_{3}^{i}&\text{From equation}\\ \hline\cr 1&0&0&-1&0&0&1&0&0&\eqref{eq:equation first components}\\ 0&-1&0&0&1&0&0&-1&0&\eqref{eq:equation second components}\\ 0&0&\epsilon_{-}&0&0&-\epsilon_{+}&0&0&\epsilon_{-}&\eqref{eq:equation third components}\\ -m_{3}^{r}/\mu_{-}&0&m_{1}^{i}/\mu_{-}&m_{3}^{t}/\mu_{+}&0&-m_{1}^{i}/\mu_{+}&-m_{3}^{i}/\mu_{-}&0&m_{1}^{i}/\mu_{-}&\eqref{eq:relations with mupmA}\\ 0&-m_{3}^{r}/\mu_{-}&m_{2}^{i}/\mu_{-}&0&m_{3}^{t}/\mu_{+}&-m_{2}^{i}/\mu_{+}&0&-m_{3}^{i}/\mu_{-}&m_{2}^{i}/\mu_{-}&\eqref{eq:relations with mupmB}\\ 0&0&0&0&0&0&m_{1}^{i}&m_{2}^{i}&m_{3}^{i}&\eqref{eq:orthogonality for Ai}\\ m_{1}^{i}&m_{2}^{i}&m_{3}^{r}&0&0&0&0&0&0&\eqref{eq:orthogonality for Ar}\\ 0&0&0&m_{1}^{i}&m_{2}^{i}&m_{3}^{t}&0&0&0&\eqref{eq:orthogonality for At}\end{matrix}.

We remark that the first five rows in the table, (4.11), (4.10), (4.15), (5.1), and (5.2) are all consequences of the boundary conditions, and the last three rows in the table, (4.22), (4.23), and (4.24), are orthogonality type conditions derived in Lemma 4.6 from the fact that 𝐄,𝐇{\mathbf{E}},{\mathbf{H}} satisfy the Maxwell system. Notice that we have six unknowns, the components of 𝐀t{\bf A}_{t} and 𝐀r{\bf A}_{r}, and eight equations. The system will be first reduced to solve (6.2) for 𝐀t{\bf A}_{t}, and substitute this value in (6.1) to get 𝐀r{\bf A}_{r}. A necessary and sufficient condition for the solvability of the system (6.2) is given in the following section. The coefficient matrix of the system is then

M=[10010010001001001000ϵ00ϵ+00ϵm3r/μ0m1i/μm3t/μ+0m1i/μ+m3i/μ0m1i/μ0m3r/μm2i/μ0m3t/μ+m2i/μ+0m3i/μm2i/μ000000m1im2im3im1im2im3r000000000m1im2im3t000].M=\begin{bmatrix}1&0&0&-1&0&0&1&0&0\\ 0&-1&0&0&1&0&0&-1&0\\ 0&0&\epsilon_{-}&0&0&-\epsilon_{+}&0&0&\epsilon_{-}\\ -m_{3}^{r}/\mu_{-}&0&m_{1}^{i}/\mu_{-}&m_{3}^{t}/\mu_{+}&0&-m_{1}^{i}/\mu_{+}&-m_{3}^{i}/\mu_{-}&0&m_{1}^{i}/\mu_{-}\\ 0&-m_{3}^{r}/\mu_{-}&m_{2}^{i}/\mu_{-}&0&m_{3}^{t}/\mu_{+}&-m_{2}^{i}/\mu_{+}&0&-m_{3}^{i}/\mu_{-}&m_{2}^{i}/\mu_{-}\\ 0&0&0&0&0&0&m_{1}^{i}&m_{2}^{i}&m_{3}^{i}\\ m_{1}^{i}&m_{2}^{i}&m_{3}^{r}&0&0&0&0&0&0\\ 0&0&0&m_{1}^{i}&m_{2}^{i}&m_{3}^{t}&0&0&0\end{bmatrix}.

For the calculation of the amplitudes it is convenient to write this matrix in terms of blocks. If we set

M1\displaystyle M_{1} =[10001000ϵ],M2=[10001000ϵ+]\displaystyle=\begin{bmatrix}1&0&0\\ 0&-1&0\\ 0&0&\epsilon_{-}\end{bmatrix},\qquad M_{2}=\begin{bmatrix}-1&0&0\\ 0&1&0\\ 0&0&-\epsilon_{+}\end{bmatrix}
N1\displaystyle N_{1} =[m3r/μ0m1i/μ0m3r/μm2i/μ000m1im2im3r000],N2=[m3t/μ+0m1i/μ+0m3t/μ+m2i/μ+000000m1im2im3t],\displaystyle=\begin{bmatrix}-m_{3}^{r}/\mu_{-}&0&m_{1}^{i}/\mu_{-}\\ 0&-m_{3}^{r}/\mu_{-}&m_{2}^{i}/\mu_{-}\\ 0&0&0\\ m_{1}^{i}&m_{2}^{i}&m_{3}^{r}\\ 0&0&0\end{bmatrix},\qquad N_{2}=\begin{bmatrix}m_{3}^{t}/\mu_{+}&0&-m_{1}^{i}/\mu_{+}\\ 0&m_{3}^{t}/\mu_{+}&-m_{2}^{i}/\mu_{+}\\ 0&0&0\\ 0&0&0\\ m_{1}^{i}&m_{2}^{i}&m_{3}^{t}\end{bmatrix},
N3\displaystyle N_{3} =[m3i/μ0m1i/μ0m3i/μm2i/μm1im2im3i000000],\displaystyle=\begin{bmatrix}-m_{3}^{i}/\mu_{-}&0&m_{1}^{i}/\mu_{-}\\ 0&-m_{3}^{i}/\mu_{-}&m_{2}^{i}/\mu_{-}\\ m_{1}^{i}&m_{2}^{i}&m_{3}^{i}\\ 0&0&0\\ 0&0&0\end{bmatrix},

then we can write M=[M1M2M1N1N2N3]M=\begin{bmatrix}M_{1}&M_{2}&M_{1}\\ N_{1}&N_{2}&N_{3}\end{bmatrix}. Therefore the amplitudes must verify the equations, written with 𝐀r,𝐀t,𝐀i{\bf A}_{r},{\bf A}_{t},{\bf A}_{i} column 3-vectors,

[M1M2M1N1N2N3][𝐀r𝐀t𝐀i]=08\begin{bmatrix}M_{1}&M_{2}&M_{1}\\ N_{1}&N_{2}&N_{3}\end{bmatrix}\begin{bmatrix}{\bf A}_{r}\\ {\bf A}_{t}\\ {\bf A}_{i}\end{bmatrix}=0\in{\mathbb{R}}^{8}

which means

M1𝐀r+M2𝐀t+M1𝐀i=03,N1𝐀r+N2𝐀t+N3𝐀i=05.M_{1}{\bf A}_{r}+M_{2}{\bf A}_{t}+M_{1}{\bf A}_{i}=0\in{\mathbb{R}}^{3},\qquad N_{1}{\bf A}_{r}+N_{2}{\bf A}_{t}+N_{3}{\bf A}_{i}=0\in{\mathbb{R}}^{5}.

From the first equation and since the matrix M1M_{1} is invertible

(6.1) 𝐀r=M11M2𝐀t𝐀i{\bf A}_{r}=-M_{1}^{-1}M_{2}{\bf A}_{t}-{\bf A}_{i}

which substituted in the second equation yields

(6.2) (N2N1M11M2)𝐀t=(N1N3)𝐀i.\left(N_{2}-N_{1}M_{1}^{-1}M_{2}\right){\bf A}_{t}=\left(N_{1}-N_{3}\right){\bf A}_{i}.

Now

P=N2N1M11M2=[m3rμ+m3tμ+0(ϵ+ϵμ1μ+)m1i0m3rμ+m3tμ+(ϵ+ϵμ1μ+)m2i000m1im2iϵ+m3rϵm1im2im3t]P=N_{2}-N_{1}M_{1}^{-1}M_{2}=\begin{bmatrix}-\dfrac{m_{3}^{r}}{\mu_{-}}+\dfrac{m_{3}^{t}}{\mu_{+}}&0&\left(\dfrac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\dfrac{1}{\mu_{+}}\right)m_{1}^{i}\\ 0&-\dfrac{m_{3}^{r}}{\mu_{-}}+\dfrac{m_{3}^{t}}{\mu_{+}}&\left(\dfrac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\dfrac{1}{\mu_{+}}\right)m_{2}^{i}\\ 0&0&0\\ m_{1}^{i}&m_{2}^{i}&\dfrac{\epsilon_{+}m_{3}^{r}}{\epsilon_{-}}\\ m_{1}^{i}&m_{2}^{i}&m_{3}^{t}\end{bmatrix}

and

Q=N1N3=[m3im3rμ000m3im3rμ0m1im2im3im1im2im3r000].Q=N_{1}-N_{3}=\begin{bmatrix}\dfrac{m_{3}^{i}-m_{3}^{r}}{\mu_{-}}&0&0\\ 0&\dfrac{m_{3}^{i}-m_{3}^{r}}{\mu_{-}}&0\\ -m_{1}^{i}&-m_{2}^{i}&-m_{3}^{i}\\ m_{1}^{i}&m_{2}^{i}&m_{3}^{r}\\ 0&0&0\end{bmatrix}.

Next

Q𝐀i=[A1i(m3im3r)μA2i(m3im3r)μA1im1iA2im2iA3im3iA1im1i+A2im2i+A3im3r0]=[A1i(m3im3r)μA2i(m3im3r)μ0A3i(m3rm3i)0].Q{\bf A}_{i}=\begin{bmatrix}\displaystyle\frac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ \displaystyle\frac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ -A_{1}^{i}m_{1}^{i}-A_{2}^{i}m_{2}^{i}-A_{3}^{i}m_{3}^{i}\\ A_{1}^{i}m_{1}^{i}+A_{2}^{i}m_{2}^{i}+A_{3}^{i}m_{3}^{r}\\ 0\end{bmatrix}=\begin{bmatrix}\displaystyle\frac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ \displaystyle\frac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ 0\\ A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\\ 0\end{bmatrix}.

Therefore, (6.2) has a solution 𝐀t{\bf A}_{t} if the vector QAiQA_{i} is in the column space of the matrix PP, and hence 𝐀r{\bf A}_{r} follows from (6.1).

6.1. Solvability of the system (6.2)

We shall prove the following proposition.

Proposition 6.1.

The system (6.2) is solvable if and only if

(6.3) A3im3i1μ=(δm3t+α1m1i+α2m2i)A3i1α3m3tA_{3}^{i}m_{3}^{i}\dfrac{1}{\mu_{-}}=\left(-\delta\,m_{3}^{t}+\alpha_{1}m_{1}^{i}+\alpha_{2}m_{2}^{i}\right)A_{3}^{i}\dfrac{1}{\alpha_{3}-m_{3}^{t}}

holds, where

δ=m3tμ+m3rμ,α1=(ϵ+ϵμ1μ+)m1i,α2\displaystyle\delta=\frac{m_{3}^{t}}{\mu_{+}}-\frac{m_{3}^{r}}{\mu_{-}},\quad\alpha_{1}=\left(\frac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\frac{1}{\mu_{+}}\right)m_{1}^{i},\quad\alpha_{2} =(ϵ+ϵμ1μ+)m2i,α3=ϵ+m3rϵ;\displaystyle=\left(\frac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\frac{1}{\mu_{+}}\right)m_{2}^{i},\quad\alpha_{3}=\frac{\epsilon_{+}m_{3}^{r}}{\epsilon_{-}};

notice that δ>0\delta>0 and α3<0\alpha_{3}<0 since m3t>0m_{3}^{t}>0 and m3r<0m_{3}^{r}<0. Moreover, we obtain the following formula for the amplitude 𝐀t{\bf A}_{t}:

(6.4) {A1t=m3im3rm3rμ+m3tμ+(A1iμ(ϵ+ϵμ1μ+)m1iϵϵm3tϵ+m3rA3i)A2t=m3im3rm3rμ+m3tμ+(A2iμ(ϵ+ϵμ1μ+)m2iϵϵm3tϵ+m3rA3i)A3t=ϵ(m3im3r)ϵm3tϵ+m3rA3i.\begin{cases}A_{1}^{t}&=\dfrac{m_{3}^{i}-m_{3}^{r}}{-\dfrac{m_{3}^{r}}{\mu_{-}}+\dfrac{m_{3}^{t}}{\mu_{+}}}\left(\dfrac{A_{1}^{i}}{\mu_{-}}-\left(\dfrac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\dfrac{1}{\mu_{+}}\right)m_{1}^{i}\dfrac{\epsilon_{-}}{\epsilon_{-}m_{3}^{t}-\epsilon_{+}m_{3}^{r}}A_{3}^{i}\right)\\ A_{2}^{t}&=\dfrac{m_{3}^{i}-m_{3}^{r}}{-\dfrac{m_{3}^{r}}{\mu_{-}}+\dfrac{m_{3}^{t}}{\mu_{+}}}\left(\dfrac{A_{2}^{i}}{\mu_{-}}-\left(\dfrac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\dfrac{1}{\mu_{+}}\right)m_{2}^{i}\dfrac{\epsilon_{-}}{\epsilon_{-}m_{3}^{t}-\epsilon_{+}m_{3}^{r}}A_{3}^{i}\right)\\ A_{3}^{t}&=\dfrac{\epsilon_{-}\left(m_{3}^{i}-m_{3}^{r}\right)}{\epsilon_{-}m_{3}^{t}-\epsilon_{+}m_{3}^{r}}A_{3}^{i}.\end{cases}

Inserting this value of 𝐀t{\bf A}_{t} into (6.1) we obtain the amplitude 𝐀r{\bf A}_{r}.

Proof.

Since the third row of the system (6.2) is zero, the system of equations to solve is

[m3rμ+m3tμ+0(ϵ+ϵμ1μ+)m1i0m3rμ+m3tμ+(ϵ+ϵμ1μ+)m2im1im2iϵ+m3rϵm1im2im3t][A1tA2tA3t]=[A1i(m3im3r)μA2i(m3im3r)μA3i(m3rm3i)0].\begin{bmatrix}-\dfrac{m_{3}^{r}}{\mu_{-}}+\dfrac{m_{3}^{t}}{\mu_{+}}&0&\left(\dfrac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\dfrac{1}{\mu_{+}}\right)m_{1}^{i}\\ 0&-\dfrac{m_{3}^{r}}{\mu_{-}}+\dfrac{m_{3}^{t}}{\mu_{+}}&\left(\dfrac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\dfrac{1}{\mu_{+}}\right)m_{2}^{i}\\ m_{1}^{i}&m_{2}^{i}&\dfrac{\epsilon_{+}m_{3}^{r}}{\epsilon_{-}}\\ m_{1}^{i}&m_{2}^{i}&m_{3}^{t}\end{bmatrix}\begin{bmatrix}A_{1}^{t}\\ A_{2}^{t}\\ A_{3}^{t}\end{bmatrix}=\begin{bmatrix}\displaystyle\frac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ \displaystyle\frac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\\ 0\end{bmatrix}.

Subtracting the third equation from the fourth we need to solve

[m3rμ+m3tμ+0(ϵ+ϵμ1μ+)m1i0m3rμ+m3tμ+(ϵ+ϵμ1μ+)m2im1im2iϵ+m3rϵ00m3tϵ+m3rϵ][A1tA2tA3t]=[A1i(m3im3r)μA2i(m3im3r)μA3i(m3rm3i)A3i(m3rm3i)],\begin{bmatrix}-\dfrac{m_{3}^{r}}{\mu_{-}}+\dfrac{m_{3}^{t}}{\mu_{+}}&0&\left(\dfrac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\dfrac{1}{\mu_{+}}\right)m_{1}^{i}\\ 0&-\dfrac{m_{3}^{r}}{\mu_{-}}+\dfrac{m_{3}^{t}}{\mu_{+}}&\left(\dfrac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\dfrac{1}{\mu_{+}}\right)m_{2}^{i}\\ m_{1}^{i}&m_{2}^{i}&\dfrac{\epsilon_{+}m_{3}^{r}}{\epsilon_{-}}\\ 0&0&m_{3}^{t}-\dfrac{\epsilon_{+}m_{3}^{r}}{\epsilon_{-}}\end{bmatrix}\begin{bmatrix}A_{1}^{t}\\ A_{2}^{t}\\ A_{3}^{t}\end{bmatrix}=\begin{bmatrix}\displaystyle\frac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ \displaystyle\frac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\\ -A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\end{bmatrix},

which written in terms of δ,α1,α2,α3\delta,\alpha_{1},\alpha_{2},\alpha_{3} is the system

[δ0α10δα2m1im2iα300m3tα3][A1tA2tA3t]=[A1i(m3im3r)μA2i(m3im3r)μA3i(m3rm3i)A3i(m3rm3i)].\begin{bmatrix}\delta&0&\alpha_{1}\\ 0&\delta&\alpha_{2}\\ m_{1}^{i}&m_{2}^{i}&\alpha_{3}\\ 0&0&m_{3}^{t}-\alpha_{3}\end{bmatrix}\begin{bmatrix}A_{1}^{t}\\ A_{2}^{t}\\ A_{3}^{t}\end{bmatrix}=\begin{bmatrix}\displaystyle\frac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ \displaystyle\frac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\mu_{-}}\\ A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\\ -A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\end{bmatrix}.

Dividing rows one and two by δ\delta gives

[10α1/δ01α2/δm1im2iα300m3tα3][A1tA2tA3t]=[A1i(m3im3r)δμA2i(m3im3r)δμA3i(m3rm3i)A3i(m3rm3i)];\begin{bmatrix}1&0&\alpha_{1}/\delta\\ 0&1&\alpha_{2}/\delta\\ m_{1}^{i}&m_{2}^{i}&\alpha_{3}\\ 0&0&m_{3}^{t}-\alpha_{3}\end{bmatrix}\begin{bmatrix}A_{1}^{t}\\ A_{2}^{t}\\ A_{3}^{t}\end{bmatrix}=\begin{bmatrix}\displaystyle\frac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}\\ \displaystyle\frac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}\\ A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\\ -A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\end{bmatrix};

multiplying the first row by m1i-m_{1}^{i} and add in it to the third row gives

[10α1/δ01α2/δ0m2iα3m1i(α1/δ)00m3tα3][A1tA2tA3t]=[A1i(m3im3r)δμA2i(m3im3r)δμA3i(m3rm3i)m1iA1i(m3im3r)δμA3i(m3rm3i)];\begin{bmatrix}1&0&\alpha_{1}/\delta\\ 0&1&\alpha_{2}/\delta\\ 0&m_{2}^{i}&\alpha_{3}-m_{1}^{i}(\alpha_{1}/\delta)\\ 0&0&m_{3}^{t}-\alpha_{3}\end{bmatrix}\begin{bmatrix}A_{1}^{t}\\ A_{2}^{t}\\ A_{3}^{t}\end{bmatrix}=\begin{bmatrix}\displaystyle\frac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}\\ \displaystyle\frac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}\\ A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)-m_{1}^{i}\dfrac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}\\ -A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\end{bmatrix};

multiplying the second row by m2i-m_{2}^{i} and add in it to the third row gives

[10α1/δ01α2/δ00α3m1i(α1/δ)m2i(α2/δ)00m3tα3][A1tA2tA3t]=[A1i(m3im3r)δμA2i(m3im3r)δμA3i(m3rm3i)m1iA1i(m3im3r)δμm2iA2i(m3im3r)δμA3i(m3rm3i)].\begin{bmatrix}1&0&\alpha_{1}/\delta\\ 0&1&\alpha_{2}/\delta\\ 0&0&\alpha_{3}-m_{1}^{i}(\alpha_{1}/\delta)-m_{2}^{i}(\alpha_{2}/\delta)\\ 0&0&m_{3}^{t}-\alpha_{3}\end{bmatrix}\begin{bmatrix}A_{1}^{t}\\ A_{2}^{t}\\ A_{3}^{t}\end{bmatrix}=\begin{bmatrix}\displaystyle\frac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}\\ \displaystyle\frac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}\\ A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)-m_{1}^{i}\dfrac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}-m_{2}^{i}\dfrac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}\\ -A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)\end{bmatrix}.

From the fourth equation, the value of A3tA_{3}^{t} is given by

A3t=A3i(m3rm3i)m3tα3.A_{3}^{t}=\dfrac{-A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)}{m_{3}^{t}-\alpha_{3}}.

We shall verify that (6.3) implies that this value of A3tA_{3}^{t} satisfies the third equation, i.e., under (6.3) equations three and four are equivalent. In fact, substituting this value of A3tA_{3}^{t} on the left hand side of the third equation we need to prove the identity

(α3m1i(α1/δ)m2i(α2/δ))A3i(m3im3r)m3tα3=A3i(m3rm3i)m1iA1i(m3im3r)δμm2iA2i(m3im3r)δμ.\left(\alpha_{3}-m_{1}^{i}(\alpha_{1}/\delta)-m_{2}^{i}(\alpha_{2}/\delta)\right)\dfrac{A_{3}^{i}\left(m_{3}^{i}-m_{3}^{r}\right)}{m_{3}^{t}-\alpha_{3}}=A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)-m_{1}^{i}\dfrac{A_{1}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}-m_{2}^{i}\dfrac{A_{2}^{i}(m_{3}^{i}-m_{3}^{r})}{\delta\mu_{-}}.

Since m1iA1i+m2iA2i=m3iA3im_{1}^{i}A_{1}^{i}+m_{2}^{i}A_{2}^{i}=-m_{3}^{i}A_{3}^{i}, this identity is equivalent to

(α3m1i(α1/δ)m2i(α2/δ))A3i(m3im3r)m3tα3=A3i(m3rm3i)+m3iA3im3im3rδμ.\left(\alpha_{3}-m_{1}^{i}(\alpha_{1}/\delta)-m_{2}^{i}(\alpha_{2}/\delta)\right)\dfrac{A_{3}^{i}\left(m_{3}^{i}-m_{3}^{r}\right)}{m_{3}^{t}-\alpha_{3}}=A_{3}^{i}\left(m_{3}^{r}-m_{3}^{i}\right)+m_{3}^{i}A_{3}^{i}\dfrac{m_{3}^{i}-m_{3}^{r}}{\delta\mu_{-}}.

Now notice that moving terms around and since m3im3r0m_{3}^{i}-m_{3}^{r}\neq 0, the last identity is equivalent to (6.3). Hence (6.4) follows.

Notice that given 𝐀i{\bf A}_{i}, the amplitude solution 𝐀t{\bf A}_{t}, and consequently 𝐀r{\bf A}_{r}, are unique since the null space of the matrix

[10α1/δ01α2/δ00α3m1i(α1/δ)m2i(α2/δ)00m3tα3]\begin{bmatrix}1&0&\alpha_{1}/\delta\\ 0&1&\alpha_{2}/\delta\\ 0&0&\alpha_{3}-m_{1}^{i}(\alpha_{1}/\delta)-m_{2}^{i}(\alpha_{2}/\delta)\\ 0&0&m_{3}^{t}-\alpha_{3}\end{bmatrix}

is zero since m3r<0m_{3}^{r}<0 and so m3tα3>0m_{3}^{t}-\alpha_{3}>0.

6.2. Analysis of the condition (6.3)

In case A3i=0A_{3}^{i}=0 (the incident wave is transverse electric (TE), that is, it is perpendicular to the normal to the interface), condition (6.3) obviously holds and from (6.4) the amplitudes are

(A1t,A2t,A3t)=μ+(m3im3r)μm3tμ+m3r(A1i,A2i,0),\left(A_{1}^{t},A_{2}^{t},A_{3}^{t}\right)=\dfrac{\mu_{+}\left(m_{3}^{i}-m_{3}^{r}\right)}{\mu_{-}m_{3}^{t}-\mu_{+}m_{3}^{r}}\left(A_{1}^{i},A_{2}^{i},0\right),

and hence from (6.1)

(A1r,A2r,A3r)=μ+(m3im3r)μm3tμ+m3r[10001000ϵ+/ϵ]𝐀i𝐀i=(μ+(m3im3r)μm3tμ+m3r1)(A1i,A2i,0).\left(A_{1}^{r},A_{2}^{r},A_{3}^{r}\right)=\dfrac{\mu_{+}\left(m_{3}^{i}-m_{3}^{r}\right)}{\mu_{-}m_{3}^{t}-\mu_{+}m_{3}^{r}}\begin{bmatrix}1&0&0\\ 0&1&0\\ 0&0&\epsilon_{+}/\epsilon_{-}\end{bmatrix}{\bf A}_{i}-{\bf A}_{i}=\left(\dfrac{\mu_{+}\left(m_{3}^{i}-m_{3}^{r}\right)}{\mu_{-}m_{3}^{t}-\mu_{+}m_{3}^{r}}-1\right)\left(A_{1}^{i},A_{2}^{i},0\right).

In case A3i0A_{3}^{i}\neq 0, if (6.3) holds, then some relationships between the wave vectors mm^{\ell}, =i,r,t\ell=i,r,t, must be satisfied. Indeed, cancelling A3iA_{3}^{i} in (6.3) for the solvability of the system we must have

m3iϵ+m3rϵm3tμ=m3iα3m3tμ\displaystyle m_{3}^{i}\dfrac{\frac{\epsilon_{+}m_{3}^{r}}{\epsilon_{-}}-m_{3}^{t}}{\mu_{-}}=m_{3}^{i}\dfrac{\alpha_{3}-m_{3}^{t}}{\mu_{-}} =δm3t+α1m1i+α2m2i\displaystyle=-\delta\,m_{3}^{t}+\alpha_{1}m_{1}^{i}+\alpha_{2}m_{2}^{i}
=(m3tμ+m3rμ)m3t+(ϵ+ϵμ1μ+)((m1i)2+(m2i)2).\displaystyle=-\left(\frac{m_{3}^{t}}{\mu_{+}}-\frac{m_{3}^{r}}{\mu_{-}}\right)\,m_{3}^{t}+\left(\frac{\epsilon_{+}}{\epsilon_{-}\mu_{-}}-\frac{1}{\mu_{+}}\right)\left(\left(m_{1}^{i}\right)^{2}+\left(m_{2}^{i}\right)^{2}\right).

Re writing this expression we get

(6.5) m3iϵ+m3rϵm3tμϵ=(m3tμ+m3rμ)m3t+(ϵ+μ+ϵμϵμμ+)((m1i)2+(m2i)2).m_{3}^{i}\dfrac{\epsilon_{+}m_{3}^{r}-\epsilon_{-}m_{3}^{t}}{\mu_{-}\epsilon_{-}}=-\left(\frac{m_{3}^{t}}{\mu_{+}}-\frac{m_{3}^{r}}{\mu_{-}}\right)\,m_{3}^{t}+\left(\frac{\epsilon_{+}\mu_{+}-\epsilon_{-}\mu_{-}}{\epsilon_{-}\mu_{-}\mu_{+}}\right)\left(\left(m_{1}^{i}\right)^{2}+\left(m_{2}^{i}\right)^{2}\right).

Since (m1i)2+(m2i)2+(m3i)2=ω2/v12=ω2ϵμ(m_{1}^{i})^{2}+(m_{2}^{i})^{2}+(m_{3}^{i})^{2}=\omega^{2}/v_{1}^{2}=\omega^{2}\,\epsilon_{-}\mu_{-}, we have (m1i)2+(m2i)2=ω2ϵμ(m3i)2(m_{1}^{i})^{2}+(m_{2}^{i})^{2}=\omega^{2}\,\epsilon_{-}\mu_{-}-(m_{3}^{i})^{2} which substituted in the last expression yields

m3iϵ+m3rϵm3tμϵ=(m3tμ+m3rμ)m3t+(ϵ+μ+ϵμϵμμ+)(ω2ϵμ(m3i)2).m_{3}^{i}\dfrac{\epsilon_{+}m_{3}^{r}-\epsilon_{-}m_{3}^{t}}{\mu_{-}\epsilon_{-}}=-\left(\frac{m_{3}^{t}}{\mu_{+}}-\frac{m_{3}^{r}}{\mu_{-}}\right)\,m_{3}^{t}+\left(\frac{\epsilon_{+}\mu_{+}-\epsilon_{-}\mu_{-}}{\epsilon_{-}\mu_{-}\mu_{+}}\right)\left(\omega^{2}\,\epsilon_{-}\mu_{-}-(m_{3}^{i})^{2}\right).

From (4.21), m3t=ω2(ϵ+μ+ϵμ)+(m3r)2m_{3}^{t}=\sqrt{\omega^{2}(\epsilon_{+}\mu_{+}-\epsilon_{-}\mu_{-})+(m_{3}^{r})^{2}}, which substituted in the last expression we get after simplification that the difference between the left-hand and right-hand sides becomes:

(m3i+m3r)(ϵ+μ+m3iϵμm3i+ϵμm3rϵμ+m3t)=0(m_{3}^{i}+m_{3}^{r})\left(\epsilon_{+}\mu_{+}m_{3}^{i}-\epsilon_{-}\mu_{-}m_{3}^{i}+\epsilon_{-}\mu_{-}m_{3}^{r}-\epsilon_{-}\mu_{+}m_{3}^{t}\right)=0

Thus, (6.5) holds if and only if:

(6.6) m3i+m3r=0m_{3}^{i}+m_{3}^{r}=0

or

(6.7) (ϵ+μ+ϵμ)m3i=ϵ(μ+m3tμm3r).\left(\epsilon_{+}\mu_{+}-\epsilon_{-}\mu_{-}\right)m_{3}^{i}=\epsilon_{-}\left(\mu_{+}m_{3}^{t}-\mu_{-}m_{3}^{r}\right).

From Equation (4.17) m3r=ω2μϵ(m1iωfx1)2(m2iωfx2)2m_{3}^{r}=-\sqrt{\omega^{2}\mu_{-}\epsilon_{-}-\left(m_{1}^{i}-\omega f_{x_{1}}\right)^{2}-\left(m_{2}^{i}-\omega f_{x_{2}}\right)^{2}}, and since m3i=ω2μϵ(m1i)2(m2i)2m_{3}^{i}=\sqrt{\omega^{2}\mu_{-}\epsilon_{-}-\left(m_{1}^{i}\right)^{2}-\left(m_{2}^{i}\right)^{2}}, (6.6) means

ω2μϵ(m1iωfx1)2(m2iωfx2)2=ω2μϵ(m1i)2(m2i)2\sqrt{\omega^{2}\mu_{-}\epsilon_{-}-\left(m_{1}^{i}-\omega f_{x_{1}}\right)^{2}-\left(m_{2}^{i}-\omega f_{x_{2}}\right)^{2}}=\sqrt{\omega^{2}\mu_{-}\epsilon_{-}-\left(m_{1}^{i}\right)^{2}-\left(m_{2}^{i}\right)^{2}}

which implies (m1iωfx1)2+(m2iωfx2)2=(m1i)2+(m2i)2\left(m_{1}^{i}-\omega f_{x_{1}}\right)^{2}+\left(m_{2}^{i}-\omega f_{x_{2}}\right)^{2}=\left(m_{1}^{i}\right)^{2}+\left(m_{2}^{i}\right)^{2}. So (6.6) holds if and only if the gradient of ff satisfies

ω((fx1)2+(fx2)2)=2(m1ifx1+m2ifx2).\omega\left((f_{x_{1}})^{2}+(f_{x_{2}})^{2}\right)=2\left(m_{1}^{i}f_{x_{1}}+m_{2}^{i}f_{x_{2}}\right).

This is clearly satisfied for the standard refraction case when f=0f=0.

Suppose m3i+m3r0m_{3}^{i}+m_{3}^{r}\neq 0. Notice that since m3i>0,m3r<0m_{3}^{i}>0,m_{3}^{r}<0, and m3t>0m_{3}^{t}>0, it follows that μ+m3tμm3r>0\mu_{+}m_{3}^{t}-\mu_{-}m_{3}^{r}>0 and so ϵ+μ+>ϵμ\epsilon_{+}\mu_{+}>\epsilon_{-}\mu_{-}. Therefore if ϵ+μ+ϵμ\epsilon_{+}\mu_{+}\leq\epsilon_{-}\mu_{-}, then from (6.7) for the system (6.2) to be solvable we must have (6.6) or A3i=0A_{3}^{i}=0.

7. Appendix

Here we prove Lemma 4.2 used in the proof of Theorem 4.3.

Proof.

Differentiating (4.6) with respect to x1x_{1} and dividing by i{\rm i} yields

(7.8) am1iei(𝐦iX)+b(m1r+ψx1)ei(𝐦rX+ψ(X))+c(m1t+ψx1)ei(𝐦tX+ψ(X))=0.a\,m_{1}^{i}\,e^{{\rm i}\,\left({\mathbf{m}}_{i}\cdot X\right)}+b\,\left(m_{1}^{r}+\psi_{x_{1}}\right)\,e^{{\rm i}\,\left({\mathbf{m}}_{r}\cdot X+\psi(X)\right)}+c\,\left(m_{1}^{t}+\psi_{x_{1}}\right)\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}=0.

Next differentiate (7.8) with respect to x1x_{1} to get

ia(m1i)2ei(𝐦iX)+b(ψx1x1+i(m1r+ψx1)2)ei(𝐦rX+ψ(X))\displaystyle{\rm i}\,a\,(m_{1}^{i})^{2}\,e^{{\rm i}\,\left({\mathbf{m}}_{i}\cdot X\right)}+b\,\left(\psi_{x_{1}x_{1}}+{\rm i}\,\left(m_{1}^{r}+\psi_{x_{1}}\right)^{2}\right)\,e^{{\rm i}\,\left({\mathbf{m}}_{r}\cdot X+\psi(X)\right)}
+c(ψx1x1+i(m1t+ψx1)2)ei(𝐦tX+ψ(X))=0.\displaystyle\qquad+c\,\left(\psi_{x_{1}x_{1}}+{\rm i}\,\left(m_{1}^{t}+\psi_{x_{1}}\right)^{2}\right)\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}=0.

Putting together (4.6), (7.8), and the last equation yields the following system

(111m1im1r+ψx1m1t+ψx1i(m1i)2ψx1x1+i(m1r+ψx1)2ψx1x1+i(m1t+ψx1)2)(aei(𝐦iX)bei(𝐦rX+ψ(X))cei(𝐦tX+ψ(X)))=0.\left(\begin{matrix}1&1&1\\ m_{1}^{i}&m_{1}^{r}+\psi_{x_{1}}&m_{1}^{t}+\psi_{x_{1}}\\ {\rm i}\,(m_{1}^{i})^{2}&\psi_{x_{1}x_{1}}+{\rm i}\,\left(m_{1}^{r}+\psi_{x_{1}}\right)^{2}&\psi_{x_{1}x_{1}}+{\rm i}\,\left(m_{1}^{t}+\psi_{x_{1}}\right)^{2}\\ \end{matrix}\right)\left(\begin{matrix}a\,e^{{\rm i}\,\left({\mathbf{m}}_{i}\cdot X\right)}\\ b\,e^{{\rm i}\,\left({\mathbf{m}}_{r}\cdot X+\psi(X)\right)}\\ c\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}\\ \end{matrix}\right)=0.

If a0a\neq 0, or b0b\neq 0, or c0c\neq 0, then the vector (aei(𝐦iX)bei(𝐦rX+ψ(X))cei(𝐦tX+ψ(X)))\left(\begin{matrix}a\,e^{{\rm i}\,\left({\mathbf{m}}_{i}\cdot X\right)}\\ b\,e^{{\rm i}\,\left({\mathbf{m}}_{r}\cdot X+\psi(X)\right)}\\ c\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}\\ \end{matrix}\right) is a non trivial solution to the system and therefore the matrix

M(x1,x2)=(111m1i(m1r+ψx1CLOSEm1t+ψx1i(m1i)2ψx1x1+i(m1r+ψx1)2ψx1x1+i(m1t+ψx1)2)\displaystyle M(x_{1},x_{2})=\left(\begin{matrix}1&1&1\\ m_{1}^{i}&(m_{1}^{r}+\psi_{x_{1}}&m_{1}^{t}+\psi_{x_{1}}\\ {\rm i}\,(m_{1}^{i})^{2}&\psi_{x_{1}x_{1}}+{\rm i}\,\left(m_{1}^{r}+\psi_{x_{1}}\right)^{2}&\psi_{x_{1}x_{1}}+{\rm i}\,\left(m_{1}^{t}+\psi_{x_{1}}\right)^{2}\\ \end{matrix}\right)

has determinant equals zero. Multiplying the first row of MM by m1i-m_{1}^{i} and adding it to the second row, and multiplying the first row by i(m1i)2-{\rm i}\,(m_{1}^{i})^{2} and adding it to the third row yields

(1110m1i+m1r+ψx1m1i+m1t+ψx10ψx1x1+i((m1r+ψx1)2(m1i)2)ψx1x1+i((m1t+ψx1)2(m1i)2)).\left(\begin{matrix}1&1&1\\ 0&-m_{1}^{i}+m_{1}^{r}+\psi_{x_{1}}&-m_{1}^{i}+m_{1}^{t}+\psi_{x_{1}}\\ 0&\psi_{x_{1}x_{1}}+{\rm i}\,\left(\left(m_{1}^{r}+\psi_{x_{1}}\right)^{2}-(m_{1}^{i})^{2}\right)&\psi_{x_{1}x_{1}}+{\rm i}\,\left(\left(m_{1}^{t}+\psi_{x_{1}}\right)^{2}-(m_{1}^{i})^{2}\right)\\ \end{matrix}\right).

So the determinant of the last matrix is zero and factoring the difference of squares yields

(m1i+m1r+ψx1)(ψx1x1+i(m1t+ψx1m1i)(m1t+ψx1+m1i))\displaystyle\left(-m_{1}^{i}+m_{1}^{r}+\psi_{x_{1}}\right)\left(\psi_{x_{1}x_{1}}+{\rm i}\,\left(m_{1}^{t}+\psi_{x_{1}}-m_{1}^{i}\right)\left(m_{1}^{t}+\psi_{x_{1}}+m_{1}^{i}\right)\right)
(m1i+m1t+ψx1)(ψx1x1+i(m1r+ψx1m1i)(m1i+m1r+ψx1))=0\displaystyle\qquad-\left(-m_{1}^{i}+m_{1}^{t}+\psi_{x_{1}}\right)\left(\psi_{x_{1}x_{1}}+{\rm i}\,\left(m_{1}^{r}+\psi_{x_{1}}-m_{1}^{i}\right)\left(m_{1}^{i}+m_{1}^{r}+\psi_{x_{1}}\right)\right)=0

that is,

(7.9) (m1rm1t)(ψx1x1i(m1i+m1r+ψx1)(m1t+ψx1m1i))=0.\left(m_{1}^{r}-m_{1}^{t}\right)\,\left(\psi_{x_{1}x_{1}}-{\rm i}\,\left(-m_{1}^{i}+m_{1}^{r}+\psi_{x_{1}}\right)\,\left(m_{1}^{t}+\psi_{x_{1}}-m_{1}^{i}\right)\right)=0.

Proceeding in the same way differentiating (4.6) with respect to x2x_{2} we obtain for the second components the equation

(7.10) (m2rm2t)(ψx2x2i(m2i+m2r+ψx2)(m2t+ψx2m2i))=0.\left(m_{2}^{r}-m_{2}^{t}\right)\,\left(\psi_{x_{2}x_{2}}-{\rm i}\,\left(-m_{2}^{i}+m_{2}^{r}+\psi_{x_{2}}\right)\,\left(m_{2}^{t}+\psi_{x_{2}}-m_{2}^{i}\right)\right)=0.

Proof of (i). We shall prove first that m1t=m1rm_{1}^{t}=m_{1}^{r}, and a similar argument proves that m2t=m2rm_{2}^{t}=m_{2}^{r}. Suppose by contradiction that m1tm1rm_{1}^{t}\neq m_{1}^{r}, then from (7.9) we must have

ψx1x1i(m1i+m1r+ψx1)(m1t+ψx1m1i)=0\psi_{x_{1}x_{1}}-{\rm i}\,\left(-m_{1}^{i}+m_{1}^{r}+\psi_{x_{1}}\right)\,\left(m_{1}^{t}+\psi_{x_{1}}-m_{1}^{i}\right)=0

and since the wave vectors mm^{\ell} have real components for =i,r,t\ell=i,r,t and the function ψ\psi is real valued we obtain that

ψx1x1(x1,x2)=0 and (m1i+m1r+ψx1)(m1t+ψx1m1i)=0.\psi_{x_{1}x_{1}}(x_{1},x_{2})=0\text{ and }\left(-m_{1}^{i}+m_{1}^{r}+\psi_{x_{1}}\right)\,\left(m_{1}^{t}+\psi_{x_{1}}-m_{1}^{i}\right)=0.

which implies that ψx1(x1,x2)=g(x2)\psi_{x_{1}}(x_{1},x_{2})=g(x_{2}), and

(7.11) m1im1r=ψx1(x1,x2), or m1im1t=ψx1(x1,x2)m_{1}^{i}-m_{1}^{r}=\psi_{x_{1}}(x_{1},x_{2}),\text{ or }m_{1}^{i}-m_{1}^{t}=\psi_{x_{1}}(x_{1},x_{2})

for all x1,x2x_{1},x_{2}. Since ψx1\psi_{x_{1}} is continuous we get that ψx1\psi_{x_{1}} is constant. Then ψ(x1,x2)=c0x1+h(x2)\psi(x_{1},x_{2})=c_{0}\,x_{1}+h(x_{2}) with c0c_{0} constant. Also at least one of the equations in (7.11) holds, so m1im1r=c0m_{1}^{i}-m_{1}^{r}=c_{0} or m1im1t=c0m_{1}^{i}-m_{1}^{t}=c_{0}. Suppose first that m1im1r=c0m_{1}^{i}-m_{1}^{r}=c_{0}. Substituting the value of m1rm_{1}^{r} into (4.6) and letting x2=0x_{2}=0 yields

aei(m1ix1)+bei(m1rx1+ψ(x1,0))+cei(m1tx1+ψ(x1,0))\displaystyle a\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}\right)}+b\,e^{{\rm i}\,\left(m_{1}^{r}\,x_{1}+\psi(x_{1},0)\right)}+c\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+\psi(x_{1},0)\right)}
=aei(m1ix1)+bei(m1rx1+c0x1+h(0))+cei(m1tx1+c0x1+h(0))\displaystyle=a\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}\right)}+b\,e^{{\rm i}\,\left(m_{1}^{r}\,x_{1}+c_{0}\,x_{1}+h(0)\right)}+c\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+c_{0}\,x_{1}+h(0)\right)}
=aei(m1ix1)+bei(m1ix1+h(0))+cei(m1tx1+c0x1+h(0))\displaystyle=a\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}\right)}+b\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}+h(0)\right)}+c\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+c_{0}\,x_{1}+h(0)\right)}
=(a+beih(0))ei(m1ix1)+cei(m1tx1+c0x1+h(0))=0.\displaystyle=\left(a\,+b\,e^{{\rm i}\,h(0)}\right)\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}\right)}+c\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+c_{0}\,x_{1}+h(0)\right)}=0.

Letting A=a+beih(0)A=a\,+b\,e^{{\rm i}\,h(0)} and B=ceih(0)B=c\,e^{{\rm i}\,h(0)} we obtain that

Aei(m1ix1)+Bei(m1tx1+c0x1)=0A\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}\right)}+B\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+c_{0}\,x_{1}\right)}=0

for all x1x_{1}. Differentiating the last expression with respect to x1x_{1} and dividing by i{\rm i} yields

Am1iei(m1ix1)+B(m1t+c0)ei(m1tx1+c0x1)=0A\,m_{1}^{i}\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}\right)}+B\left(m_{1}^{t}+c_{0}\right)\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+c_{0}\,x_{1}\right)}=0

which written in matrix form is

(11m1im1t+c0)(Aei(m1ix1)Bei(m1tx1+c0x1))=0.\left(\begin{matrix}1&1\\ m_{1}^{i}&m_{1}^{t}+c_{0}\end{matrix}\right)\left(\begin{matrix}A\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}\right)}\\ B\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+c_{0}\,x_{1}\right)}\end{matrix}\right)=0.

Since c0c\neq 0, the vector (Aei(m1ix1)Bei(m1tx1+c0x1))0\left(\begin{matrix}A\,e^{{\rm i}\,\left(m_{1}^{i}\,x_{1}\right)}\\ B\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+c_{0}\,x_{1}\right)}\end{matrix}\right)\neq 0, then we obtain c0=m1im1tc_{0}=m_{1}^{i}-m_{1}^{t}. Since we assumed c0=m1im1rc_{0}=m_{1}^{i}-m_{1}^{r}, we get that m1r=m1tm_{1}^{r}=m_{1}^{t} contradicting the assumption that m1rm1tm_{1}^{r}\neq m_{1}^{t}. If on the other hand, m1im1t=c0m_{1}^{i}-m_{1}^{t}=c_{0} proceeding in the same way and now using that b0b\neq 0 we get as before m1r=m1tm_{1}^{r}=m_{1}^{t} contradicting the initial assumption.

To prove that m2r=m2tm_{2}^{r}=m_{2}^{t}, we proceed in the same way but using (7.10).

To complete the proof of (i), since m1t=m1rm_{1}^{t}=m_{1}^{r} and m2t=m2rm_{2}^{t}=m_{2}^{r}, substituting these into (4.6) yields

(7.12) aei(m1ix1+m2ix2)+(b+c)ei(m1rx1+m2rx2+ψ(x1,x2))=0.a\,e^{{\rm i}\,\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}\right)}+(b+c)\,e^{{\rm i}\,\left(m_{1}^{r}x_{1}+m_{2}^{r}x_{2}+\psi(x_{1},x_{2})\right)}=0.

Differentiating this identity with respect to x1x_{1} and dividing by i{\rm i} yields

am1iei(m1ix1+m2ix2)+(b+c)(m1r+ψx1)ei(m1rx1+m2rx2+ψ(x1,x2))=0.a\,m_{1}^{i}\,e^{{\rm i}\,\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}\right)}+(b+c)\,\left(m_{1}^{r}+\psi_{x_{1}}\right)\,e^{{\rm i}\,\left(m_{1}^{r}x_{1}+m_{2}^{r}x_{2}+\psi(x_{1},x_{2})\right)}=0.

That is, we obtain the system of equations

(11m1im1r+ψx1)(aei(m1ix1+m2ix2)(b+c)ei(m1rx1+m2rx2+ψ(x1,x2)))=0.\left(\begin{matrix}1&1\\ m_{1}^{i}&m_{1}^{r}+\psi_{x_{1}}\end{matrix}\right)\left(\begin{matrix}a\,e^{{\rm i}\,\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}\right)}\\ (b+c)\,e^{{\rm i}\,\left(m_{1}^{r}x_{1}+m_{2}^{r}x_{2}+\psi(x_{1},x_{2})\right)}\end{matrix}\right)=0.

Since a0a\neq 0, the vector (aei(m1ix1+m2ix2)(b+c)ei(m1rx1+m2rx2+ψ(x1,x2)))\left(\begin{matrix}a\,e^{{\rm i}\,\left(m_{1}^{i}x_{1}+m_{2}^{i}x_{2}\right)}\\ (b+c)\,e^{{\rm i}\,\left(m_{1}^{r}x_{1}+m_{2}^{r}x_{2}+\psi(x_{1},x_{2})\right)}\end{matrix}\right) is a non trivial solution to the system and so det(11m1im1r+ψx1)=m1r+ψx1m1i=0\det\left(\begin{matrix}1&1\\ m_{1}^{i}&m_{1}^{r}+\psi_{x_{1}}\end{matrix}\right)=m_{1}^{r}+\psi_{x_{1}}-m_{1}^{i}=0 for all x1,x2x_{1},x_{2} as desired.

Differentiating (7.12) with respect to x2x_{2} in the same way we obtain that m2r+ψx2m2i=0m_{2}^{r}+\psi_{x_{2}}-m_{2}^{i}=0 completing the proof of (i).

Proof of (ii). Since a=0a=0, we have simplifying the exponential eiψ(X)e^{{\rm i}\,\psi(X)} in (4.6) that

bei𝐦rX+cei𝐦tX=0.b\,e^{{\rm i}\,{\mathbf{m}}_{r}\cdot X}+c\,e^{{\rm i}\,{\mathbf{m}}_{t}\cdot X}=0.

Differentiating the last equation with respect to x1x_{1} and letting x2=0x_{2}=0 yields

bm1reim1rx1+cm1teim1tx1=0.b\,m_{1}^{r}\,e^{{\rm i}\,m_{1}^{r}\,x_{1}}+c\,m_{1}^{t}\,e^{{\rm i}\,m_{1}^{t}\,x_{1}}=0.

So we get the system

(11m1rm1t)(beim1rx1ceim1tx1)=0,\left(\begin{matrix}1&1\\ m_{1}^{r}&m_{1}^{t}\end{matrix}\right)\left(\begin{matrix}b\,e^{{\rm i}\,m_{1}^{r}\,x_{1}}\\ c\,e^{{\rm i}\,m_{1}^{t}\,x_{1}}\end{matrix}\right)=0,

and since c0c\neq 0 the determinant of the last matrix must be zero and so m1r=m1tm_{1}^{r}=m_{1}^{t}. Similarly, differentiating with respect to x2x_{2} and letting x1=0x_{1}=0 we obtain that m2r=m2tm_{2}^{r}=m_{2}^{t}.

Proof of (iii). We have

aei𝐦iX+cei(𝐦tX+ψ(X))=0,a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}+c\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}=0,

and differentiating with respect to x1x_{1} and dividing by i{\rm i} yields

m1iaei𝐦iX+(m1t+ψx1)cei(𝐦tX+ψ(X))=0,m_{1}^{i}\,a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}+\left(m_{1}^{t}+\psi_{x_{1}}\right)c\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}=0,

and so

(11m1im1t+ψx1)(aei𝐦iXcei(𝐦tX+ψ(X)))=0.\left(\begin{matrix}1&1\\ m_{1}^{i}&m_{1}^{t}+\psi_{x_{1}}\end{matrix}\right)\left(\begin{matrix}a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}\\ c\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}\end{matrix}\right)=0.

Since the vector (aei𝐦iXcei(𝐦tX+ψ(X)))0\left(\begin{matrix}a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}\\ c\,e^{{\rm i}\,\left({\mathbf{m}}_{t}\cdot X+\psi(X)\right)}\end{matrix}\right)\neq 0, the determinant of the matrix equals zero, i.e., m1t+ψx1(x1,x2)=m1im_{1}^{t}+\psi_{x_{1}}(x_{1},x_{2})=m_{1}^{i} for all XX and therefore ψx1\psi_{x_{1}} is constant, that is, ψ(x1,x2)=c0x1+g(x2)\psi(x_{1},x_{2})=c_{0}\,x_{1}+g(x_{2}). Substituting the value of ψ\psi in the original equation yields

aei𝐦iX+cei(m1tx1+m2tx2+c0x1+g(x2))=0,a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}+c\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+m_{2}^{t}\,x_{2}+c_{0}\,x_{1}+g(x_{2})\right)}=0,

which differentiated with respect to x2x_{2} gives

m2iaei𝐦iX+(m2t+g(x2))cei(m1tx1+m2tx2+c0x1+g(x2))=0.m_{2}^{i}\,a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}+\left(m_{2}^{t}+g^{\prime}(x_{2})\right)\,c\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+m_{2}^{t}\,x_{2}+c_{0}\,x_{1}+g(x_{2})\right)}=0.

Therefore

(11m2im2t+g(x2))(aei𝐦iXcei(m1tx1+m2tx2+c0x1+g(x2)))=0.\left(\begin{matrix}1&1\\ m_{2}^{i}&m_{2}^{t}+g^{\prime}(x_{2})\end{matrix}\right)\left(\begin{matrix}a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}\\ c\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+m_{2}^{t}\,x_{2}+c_{0}\,x_{1}+g(x_{2})\right)}\end{matrix}\right)=0.

Again, since the vector (aei𝐦iXcei(m1tx1+m2tx2+c0x1+g(x2)))0\left(\begin{matrix}a\,e^{{\rm i}\,{\mathbf{m}}_{i}\cdot X}\\ c\,e^{{\rm i}\,\left(m_{1}^{t}\,x_{1}+m_{2}^{t}\,x_{2}+c_{0}\,x_{1}+g(x_{2})\right)}\end{matrix}\right)\neq 0, we obtain m2t+g(x2)=m2im_{2}^{t}+g^{\prime}(x_{2})=m_{2}^{i}, implying that g(x2)g^{\prime}(x_{2}) is constant and so g(x2)=c1x2+c2g(x_{2})=c_{1}\,x_{2}+c_{2} and we are done.

This proof of (iv) is the same as the proof of (iii). ∎

8. Conclusion

An analysis of the Maxwell system of electrodynamics in the context of distributions is carried out, leading to the derivation of boundary conditions for the electromagnetic field when the current and charge densities are localized at the interface. Consequently, by representing the electric field as a nonlinear perturbation of a plane wave characterized by a phase discontinuity function, the generalized Snell law is obtained. Furthermore, we derive formulas for the amplitudes of the reflected and transmitted waves in terms of the amplitude of the incident wave.

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