Pointing control of spacecraft using two SGCMGs via LPV control theory

Author:

Kwon Sangwon,Shimomura Takashi,Okubo Hiroshi

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference14 articles.

1. Singularity escape/avoidance steering logic for control moment gyro systems;Wie;Journal of Guidance, Control, and Dynamics,2005

2. Steering law design for redundant single gimbal control moment gyroscopes;Bedrossian;Journal of Guidance, Control, and Dynamics,1990

3. Singular direction avoidance steering for control moment gyros;Ford;Journal of Guidance, Control, and Dynamics,2000

4. H. Okubo, Y. Tani, Singularity robust steering of redundant single gimbal control moment gyros for small satellites, in: Proceedings of the 8th International Symposium on Artificial Intelligence, Robotics and Automation in Space, Munich, Germany, 2005, pp. 1–8.

5. Attitude stabilization of a rigid spacecraft using two momentum wheel actuators;Krishnan;Journal of Guidance, Control, and Dynamics,1995

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