The scientist’s investigation covers issues in Control theory, Control engineering, Control system, Control theory and Control reconfiguration. His Actuator, Lyapunov function, Sliding mode control, Nonlinear system and Variable structure control investigations are all subjects of Control theory research. Youdan Kim has researched Control engineering in several fields, including Fault tolerance, Artificial neural network, Differential GPS and Fault detection and isolation.
His Control system research is multidisciplinary, incorporating elements of Mobile robot, Machine vision, Pursuit guidance, Ground control station and Robustness. Youdan Kim usually deals with Control theory and limits it to topics linked to Flight control surfaces and Angle of attack, Aerodynamic force, Rudder and Yaw. Youdan Kim works mostly in the field of Control reconfiguration, limiting it down to topics relating to Nonlinear control and, in certain cases, Stuck-at fault, as a part of the same area of interest.
Youdan Kim focuses on Control theory, Control engineering, Control theory, Computer simulation and Nonlinear system. His studies in Control theory integrate themes in fields like Missile and Fault detection and isolation. His Fault detection and isolation research incorporates themes from Fault tolerance, Kalman filter and Inertial frame of reference.
His work carried out in the field of Control engineering brings together such families of science as Control reconfiguration and Actuator. Youdan Kim combines subjects such as Artificial neural network, Control, Lyapunov function and Linearization with his study of Control theory. His research integrates issues of Stability and Proportional navigation in his study of Computer simulation.
His primary scientific interests are in Control theory, Computer simulation, Nonlinear system, Missile and Trajectory. Youdan Kim studies Control theory, namely Control theory. The study incorporates disciplines such as Spacecraft, Proportional navigation, Missile guidance and Hamiltonian in addition to Computer simulation.
His Nonlinear system research is multidisciplinary, relying on both Fault tolerance, Autopilot and Reference model. His Missile research includes elements of Full state feedback, Tracking error, Acceleration and Riccati equation. Youdan Kim has included themes like Ballistic missile, Control system, Position and Waypoint in his Trajectory study.
The scientist’s investigation covers issues in Control theory, Computer simulation, Field of view, Nonlinear system and Interception. His work in the fields of Control theory, such as Nonlinear stability, overlaps with other areas such as Halo orbit. In his study, Orbit, Libration, Control theory, Celestial mechanics and Point is strongly linked to Spacecraft, which falls under the umbrella field of Computer simulation.
His Field of view study incorporates themes from Control, Pursuit guidance and Limit. His research investigates the connection between Pursuit guidance and topics such as Acceleration that intersect with problems in Trajectory and Missile. His work on Feedback linearization as part of his general Nonlinear system study is frequently connected to Inversion of control, thereby bridging the divide between different branches of science.
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A Survey of Fault Detection, Isolation, and Reconfiguration Methods
Inseok Hwang;Sungwan Kim;Youdan Kim;Chze Eng Seah.
IEEE Transactions on Control Systems and Technology (2010)
Introduction to Dynamics and Control of Flexible Structures
John L. Junkins;Youdan Kim.
Nonlinear Adaptive Flight Control Using Backstepping and Neural Networks Controller
Taeyoung Lee;Youdan Kim.
Journal of Guidance Control and Dynamics (2001)
Design of Missile Guidance Law via Variable Structure Control
Jongki Moon;Kiseok Kim;Youdan Kim.
Journal of Guidance Control and Dynamics (2001)
Robust backstepping control for slew maneuver using nonlinear tracking function
Ki-Seok Kim;Youdan Kim.
IEEE Transactions on Control Systems and Technology (2003)
Reconfigurable flight control system design using adaptive neural networks
Dong-Ho Shin;Youdan Kim.
IEEE Transactions on Control Systems and Technology (2004)
Reconfigurable Flight Control System Design Using Direct Adaptive Method
Ki-Seok Kim;Keum-Jin Lee;Youdan Kim.
Journal of Guidance Control and Dynamics (2003)
Modified Pure Proportional Navigation Guidance Law for Impact Time Control
Namhoon Cho;Youdan Kim.
Journal of Guidance Control and Dynamics (2016)
Time-Domain Finite Element Method for Inverse Problem of Aircraft Maneuvers
Suchang Lee;Youdan Kim.
Journal of Guidance Control and Dynamics (1997)
Lyapunov-based impact time control guidance laws against stationary targets
Mingu Kim;Bokyung Jung;Bumku Han;Sangchul Lee.
IEEE Transactions on Aerospace and Electronic Systems (2015)
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