Spacecraft Control Method for Fast Attitude Maneuver and Stabilization

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]. Chinese Space Science and Technology, 2010, 30(5): 48-53.

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https://journal26.magtechjournal.com/kjkxjs/EN/Y2010/V30/I5/48

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Spacecraft Control Method for Fast Attitude Maneuver and Stabilization

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