Leader-Follower Consensus Control For Multi-Spacecraft With The Attitude Observers On SO(3)

Nanji Yang, Zhifu Wang, Dianyuan Huang
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Abstract

The issue of leader-follower consensus control for the multi-spacecraft structure on SO(3) has been studied in this article. An attitude observer has been utilized to reckon the attitude information of the reference spacecraft, which is not available for all followers. A new attitude error has been proposed. With the observer and the proposed attitude error, sliding mode control has been exploited to investigate a distributed control protocol for the leader-follower systems. Both the availability of the observer and the feasibility of the control approach are rigorously mathematically proven. Finally, a simulation outcomes confirm the superiority and validity of the protocols.
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基于SO(3)姿态观测器的多航天器领导-从者共识控制
本文研究了多航天器结构在SO(3)条件下的leader-follower共识控制问题。利用姿态观测器估计参考航天器的姿态信息,该信息并非对所有跟踪器都可用。提出了一种新的姿态误差。利用观测器和所提出的姿态误差,利用滑模控制方法研究了一种针对领导者-追随者系统的分布式控制协议。观测器的可用性和控制方法的可行性都得到了严格的数学证明。最后,仿真结果验证了协议的优越性和有效性。
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