Robust trajectory tracking control for soft landing on small bodies with input saturation

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

To deal with the uncertainties of asteroid gravitational field during landing on a small body, a fuzzy gain-scheduling output feedback control for robust trajectory tracking is proposed for soft landing on small body surface with actuator saturation via fuzzy Lyapunov function. For the saturation nonlinearity, the deadzone function of control input is introduced as a supplementary controller input. Then, a gain-scheduling output feedback controller is introduced to stabilize the saturated Takagi-Sugeno (T-S) fuzzy system with optimal L2 gain performance. The application of the fuzzy Lyapunov function tackles with the conservation problem in controller design. As a result, the synthesized system enjoys an enlarged stability region and enhanced robust performance, which are essential for the success of small body soft landing. The landing control algorithm proposed in this paper is demonstrated by a flight dynamics simulating the powered descent on the asteroid of Eros 433.

源语言英语
主期刊名Promote the Progress of the Pacific-Basin Region through Space Innovation
编辑Arun K. Misra, Li Ming, Yasuhiro Morita
出版商Univelt Inc.
291-304
页数14
ISBN(印刷版)9780877036555
出版状态已出版 - 2018
活动15th International Space Conference of Pacific-basin Societies, ISCOPS 2018 - Montreal, 加拿大
期限: 10 7月 201813 7月 2018

出版系列

姓名Advances in the Astronautical Sciences
166
ISSN(印刷版)0065-3438

会议

会议15th International Space Conference of Pacific-basin Societies, ISCOPS 2018
国家/地区加拿大
Montreal
时期10/07/1813/07/18

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