Modeling and adaptive control for a spatial flexible spacecraft with unknown actuator failures
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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… read more here.
Keywords: adaptive control; flexible spacecraft; control; unknown actuator ... See more keywords