Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description

Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description

For the obstacle avoidance and formation maintenance issues of spacecraft formation, a control method with prescribed performance is proposed. Firstly, an error description system based on SE (3) is established. Secondly, to simplify the control system, collision avoidance, formation control of lead...

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Bibliographic Details
Main Authors:	Lijun Li, Yuanda Wang, Qin Yang, Erhan Wang
Format:	Article
Language:	English
Published:	Wiley 2025-01-01
Series:	International Journal of Aerospace Engineering
Online Access:	http://dx.doi.org/10.1155/ijae/8765666
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