Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint

Binglong Cong*, Xiangdong Liu, Zhen Chen, Xianren Ren

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

9 引用 (Scopus)

摘要

In this paper, the attitude control problem for uncertain spacecraft under angular velocity constraint is addressed. Both parametric uncertainty and external disturbance are considered in the spacecraft's dynamics. The spacecraft's attitude is represented by modified Rodrigues parameter (MRP) for its non-redundancy. A time-varying sliding mode control (TVSMC) algorithm is derived for attitude control system. The proposed control algorithm eliminates the reaching phase of the conventional time-invariant sliding mode control (SMC) and guarantees the sliding mode occurrence all the time. Moreover, the control parameter is adjusted to avoid the angular velocity constraint during the maneuver. Finally, a numerical simulation is employed to verify the proposed control algorithm.

源语言英语
主期刊名Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011
670-674
页数5
DOI
出版状态已出版 - 2011
活动2011 Chinese Control and Decision Conference, CCDC 2011 - Mianyang, 中国
期限: 23 5月 201125 5月 2011

出版系列

姓名Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011

会议

会议2011 Chinese Control and Decision Conference, CCDC 2011
国家/地区中国
Mianyang
时期23/05/1125/05/11

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