Spacecraft Control Method for Fast Attitude Maneuver and Stabilization

中国科技核心期刊
中文核心期刊
CSCD、CSA核心源期刊
ESCI、SCOPUS、知网、万方、维普全文收录期刊

›› 2010, Vol. 30 ›› Issue (5): 48-53.

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Spacecraft Control Method for Fast Attitude Maneuver and Stabilization

LEI Yong-Jun^1,2, TAN Shu-Ping^1,2, LIU Yi-Wu^1,2

(1 Beijing Institute of Control Engineering, Beijing 100190)(2 National Laboratory of Space Intelligent Control, Beijing 100190)

Received:2009-10-09 Revised:2010-05-11 Published:2010-10-25 Online:2010-10-25

Abstract

Abstract: For the complex satellites with flexible appendages and input noises, the adaptive control method based on the characteristic model was used. A fast maneuver and stability controller was designed, which combined the multivariable track keeping control, logic integral control and logic differential control. A numerical simulation was presented. The simulation results show that the designed control method can insure the fast maneuver and stability performance.

Key words: Attitude control, Adaptive control, Fast maneuver, Characteristic model, Flexible satellite

LEI Yong-Jun, TAN Shu-Ping, LIU Yi-Wu. Spacecraft Control Method for Fast Attitude Maneuver and Stabilization[J]. , 2010, 30(5): 48-53.

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Spacecraft Control Method for Fast Attitude Maneuver and Stabilization

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