Backstepping attitude coordination control for spacecraft formation with multiple delays

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 addresses attitude coordination control for spacecraft formation with multiple delays. A distributed angular velocity input law is firstly constructed for attitude synchronization and tracking under multiple communication delays. Introducing virtual auxiliary systems makes it possible to integrate the angular velocity input law with the true control torque, and asymptotic stability of the system is guaranteed by Lyapunov theory. Moreover, by modifying the angular velocity input law, attitude coordination among spacecrafts can be guaranteed even under control input saturation constraints. Finally, effectiveness of the proposed methodology is illustrated by concrete simulations.

源语言英语
主期刊名2nd IAA Conference on Dynamics and Control of Space Systems, 2014
编辑Filippo Graziani, Anna D. Guerman, Jean-Michel Contant
出版商Univelt Inc.
1043-1054
页数12
ISBN(印刷版)9780877036173
出版状态已出版 - 2015
活动2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014 - Rome, 意大利
期限: 24 3月 201426 3月 2014

出版系列

姓名Advances in the Astronautical Sciences
153
ISSN(印刷版)0065-3438

会议

会议2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014
国家/地区意大利
Rome
时期24/03/1426/03/14

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