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Published in 2021 at "Science China Information Sciences"
DOI: 10.1007/s11432-020-3109-x
Abstract: In this paper, we address simultaneous control of a flexible spacecraft’s attitude and vibrations in a three-dimensional space under input disturbances and unknown actuator failures. Using Hamilton’s principle, the system dynamics is modeled as an…
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Keywords:
adaptive control;
flexible spacecraft;
control;
unknown actuator ... See more keywords