Sliding mode control attitude tracking of rigid spacecraft using adaptive back-stepping method

Chunmei Yu, Kunfeng Lu, Yuanqing Xia, Hailiang Liu

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

The attitude tracking control problem for a rigid spacecraft system is investigated in this paper. A novel adaptive approach is proposed with the utilization of sliding mode control (SMC) and backstepping technique (BT) to achieve accurate attitude tracking control for spacecraft system in the presence of inertia uncertainties and external disturbances. Finally, simulation results are presented to illustrate effectiveness of the control strategies.

源语言英语
主期刊名Proceedings of the 34th Chinese Control Conference, CCC 2015
编辑Qianchuan Zhao, Shirong Liu
出版商IEEE Computer Society
3281-3286
页数6
ISBN(电子版)9789881563897
DOI
出版状态已出版 - 11 9月 2015
活动34th Chinese Control Conference, CCC 2015 - Hangzhou, 中国
期限: 28 7月 201530 7月 2015

出版系列

姓名Chinese Control Conference, CCC
2015-September
ISSN(印刷版)1934-1768
ISSN(电子版)2161-2927

会议

会议34th Chinese Control Conference, CCC 2015
国家/地区中国
Hangzhou
时期28/07/1530/07/15

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