Optimal attitude consensus control for rigid spacecraft formation based on control Lyapunov functions

Abstract In this article, the optimal attitude consensus control problem of distributed spacecraft formation through local information exchange is solved in the presence of parameter uncertainty and disturbance. The attitude dynamics model of rigid spacecraft formation is established based on unit q...

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Bibliographic Details
Main Authors: Hui Wang, Jinxiu Zhang, Qingrui Zhou, Hui‐Jie Sun, Yu‐Yao Wu
Format: Article
Language:English
Published: Wiley 2023-08-01
Series:IET Control Theory & Applications
Subjects:
Online Access:https://doi.org/10.1049/cth2.12513