Adaptive Modified Sliding-Mode-Based Attitude Control of a Satellite under Reaction Wheel Fault
In this paper, passive adaptive modified sliding-mode-based fault tolerant control is designed to track the desired attitude of a satellite with four reaction wheels in the presence of external disturbances, system uncertainties, and actuator fault. In order to achieve this goal, the adaptive modifi...
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| Главные авторы: | , , , , |
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| Формат: | Artigo |
| Язык: | Persa |
| Опубликовано: |
Aerospace Research Institute (ARI)
2024-09-01
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| Серии: | فناوری در مهندسی هوافضا |
| Предметы: | |
| Online-ссылка: | https://jtae.ari.ac.ir/article_180798_c96b5a720b38c5c75742a4cb696ceba1.pdf |
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