Formation Control of Spacecraft Based on <italic>SE</italic>(3) With Asymmetric Saturated Input
In this paper, a set of integrated control problems for distributed spacecraft formation with input asymmetric constraints under external disturbances are studied. First, a new configuration error function is designed based on the compact nonlinear manifold <inline-formula> <tex-math notati...
Główni autorzy: | , , , , |
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Format: | Artykuł |
Język: | English |
Wydane: |
IEEE
2023-01-01
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Seria: | IEEE Access |
Hasła przedmiotowe: | |
Dostęp online: | https://ieeexplore.ieee.org/document/10322723/ |