Adaptive predefined-time precise anti-unwinding attitude control for a spacecraft with inertia uncertainty
This paper proposes an adaptive predefined-time accurate anti-unwinding attitude controller for a spacecraft with uncertain inertia. The novelty of the proposed algorithm lies in that the spacecraft attitude error is regulated to exact zero after a predefined settling time, which is an explicit para...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2025-07-01
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| Series: | Measurement + Control |
| Online Access: | https://doi.org/10.1177/00202940241281217 |
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