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Cooperation attitude control of multiple spacecraft using sliding mode variable structure

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper focuses on the attitude control for multiple spacecraft. Two decentralized finite-time control laws are proposed when the communication topologies are directed and undirected, respectively. The proposed control schemes rely on the information of angular velocity errors and error quaternions of the neighboring spacecraft which determines the orientation of the torques and reduce the relative errors. Finite-time stabilization of the system is proved by using Lyapunov function and graph theory. Finally, simulation examples are illustrated to validate the approach by different case studies.

源语言英语
主期刊名Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014
出版商Institute of Electrical and Electronics Engineers Inc.
1828-1833
页数6
ISBN(电子版)9781479925384
DOI
出版状态已出版 - 31 8月 2015
活动International Conference on Mechatronics and Control, ICMC 2014 - Jinzhou, 中国
期限: 3 7月 20145 7月 2014

出版系列

姓名Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014

会议

会议International Conference on Mechatronics and Control, ICMC 2014
国家/地区中国
Jinzhou
时期3/07/145/07/14

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