Lyapunov Control Law for Slew Maneuver Using Time Finite Element Analysis

Author:

Suk Jinyoung1,Boo Sunwoong1,Kim Youdan2

Affiliation:

1. Korea Aerospace Industries, Ltd., Changwon 641-600, Republic of Korea

2. Seoul National University, Seoul 151-742, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A robust attitude control strategy with guaranteed transient performance via modified Lyapunov-based control and integral sliding mode control;Nonlinear Dynamics;2014-07-26

2. A comparative study for collocated and non-collocated sensor/actuator placement in vibration control of a maneuvering flexible satellite;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2014-07-21

3. Robust Attitude Control with Improved Transient Performance;IFAC Proceedings Volumes;2014

4. Gust Load Alleviation of an Aeroelastic System Using Nonlinear Control;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

5. Optimal active random vibration control for smart truss structures based on reliability;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2007-11-01

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