Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode

Chao Gan, Pingli Lu, Xiangdong Liu, Dapeng Yang

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

In this paper, the distributed cooperative attitude tracking control law based on a new modified fast terminal sliding mode is presented for multiple spacecraft formation flying in the presence of model uncertainty and external disturbance. Firstly, to speed the convergence rate and avoid the singularity problem, a new modified fast terminal sliding mode manifold is proposed. Then, based on the proposed terminal sliding mode manifold, the distributed cooperative attitude tracking controller is designed for the spacecraft formation flying(SFF) in the presence of model uncertainty and external disturbance, Meanwhile, the finite time stability of SFF system can be also guaranteed. Finally, numerical simulation is given to verify the validity of the proposed control algorithm.

源语言英语
主期刊名Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014
出版商Institute of Electrical and Electronics Engineers Inc.
2687-2692
页数6
版本March
ISBN(电子版)9781479958252
DOI
出版状态已出版 - 2 3月 2015
活动2014 11th World Congress on Intelligent Control and Automation, WCICA 2014 - Shenyang, 中国
期限: 29 6月 20144 7月 2014

出版系列

姓名Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
编号March
2015-March

会议

会议2014 11th World Congress on Intelligent Control and Automation, WCICA 2014
国家/地区中国
Shenyang
时期29/06/144/07/14

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