摘要
This paper investigates the coordinated control for multiple spacecraft system with state constraints. The proposed control scheme is with application to a novel multiple spacecraft system called tethered space net robot. The coordinated control strategies are proposed based on the artificial potential field method. Simulations show that the system can track the desired trajectory with the predetermined pattern and simultaneously avoid violating the constraints.
源语言 | 英语 |
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文章编号 | 8760549 |
页(从-至) | 1189-1201 |
页数 | 13 |
期刊 | IEEE Transactions on Aerospace and Electronic Systems |
卷 | 56 |
期 | 2 |
DOI | |
出版状态 | 已出版 - 4月 2020 |