User profiles for Youdan Kim
 | Youdan KimSeoul National University Verified email at snu.ac.kr Cited by 11352 |
A survey of fault detection, isolation, and reconfiguration methods
Fault detection, isolation, and reconfiguration (FDIR) is an important and challenging problem
in many engineering applications and continues to be an active area of research in the …
in many engineering applications and continues to be an active area of research in the …
[BOOK][B] Introduction to dynamics and control of flexible structures
JL Junkins, Y Kim - 1993 - books.google.com
… Junkins and Youdan Kim, 1993 Dynamics of Atmospheric Re-Entry Frank J. Regan and
Satya M. Anandakrishnan, 1993 Practical Intake Aerodynamic Design EL Goldsmith and J …
Satya M. Anandakrishnan, 1993 Practical Intake Aerodynamic Design EL Goldsmith and J …
Nonlinear adaptive flight control using backstepping and neural networks controller
FEEDBACK linearization is a theoretically established and widely used method in controlling
nonlinear systems. Exact input–output linearization is often used to control specific output …
nonlinear systems. Exact input–output linearization is often used to control specific output …
Robust backstepping control for slew maneuver using nonlinear tracking function
KS Kim, Y Kim - IEEE Transactions on control systems …, 2003 - ieeexplore.ieee.org
The backstepping control method provides useful control logic, especially for a cascaded
system. Because spacecraft dynamics and kinematics form a cascaded system, the spacecraft …
system. Because spacecraft dynamics and kinematics form a cascaded system, the spacecraft …
Design of missile guidance law via variable structure control
J Moon, K Kim, Y Kim - Journal of Guidance, Control, and Dynamics, 2001 - arc.aiaa.org
PROPORTIONAL navigation guidance (PNG) was fi rst developed during the 1950s, and
during the 1970s and 1980s various PNG laws such as pure proportional navigation (PPN), …
during the 1970s and 1980s various PNG laws such as pure proportional navigation (PPN), …
Modified pure proportional navigation guidance law for impact time control
The analytic solution for the time-to-go of the pure proportional navigation guidance law
against a stationary target is derived considering full nonlinear engagement kinematics without …
against a stationary target is derived considering full nonlinear engagement kinematics without …
Lyapunov-based impact time control guidance laws against stationary targets
M Kim, B Jung, B Han, S Lee… - IEEE Transactions on …, 2015 - ieeexplore.ieee.org
Nonlinear guidance laws that consider impact time constraints are proposed. Two-dimensional
and three-dimensional impact time control guidance laws are derived using Lyapunov …
and three-dimensional impact time control guidance laws are derived using Lyapunov …
Collision avoidance strategies for unmanned aerial vehicles in formation flight
Collision avoidance strategies for multiple unmanned aerial vehicles (UAVs) based on
geometry are investigated in this study. The proposed strategies allow a group of UAVs to avoid …
geometry are investigated in this study. The proposed strategies allow a group of UAVs to avoid …
Composite model reference adaptive control with parameter convergence under finite excitation
A new parameter estimation method is proposed in the framework of composite model reference
adaptive control for improved parameter convergence without persistent excitation. The …
adaptive control for improved parameter convergence without persistent excitation. The …
Reconfigurable flight control system design using adaptive neural networks
DH Shin, Y Kim - IEEE Transactions on control systems …, 2004 - ieeexplore.ieee.org
An adaptive controller design method based on neural network is proposed for reconfigurable
flight control systems in the presence of variations in aerodynamic coefficients or control …
flight control systems in the presence of variations in aerodynamic coefficients or control …