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...
Main Authors: | , , , , |
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Format: | Article |
Language: | English |
Published: |
Wiley
2023-08-01
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Series: | IET Control Theory & Applications |
Subjects: | |
Online Access: | https://doi.org/10.1049/cth2.12513 |