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Published in 2019 at "IEEE/ASME Transactions on Mechatronics"
DOI: 10.1109/tmech.2019.2928703
Abstract: The spacecraft attitude tracking problem with exponential convergence and resilient control capability ensured is investigated. The system uncertainties induced by uncertain inertia and external disturbance, and the actuator uncertainties consisting of misalignment and faults, are…
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Keywords:
actuator uncertainties;
exponential resilient;
attitude tracking;
resilient control ... See more keywords