A hybrid control scheme for attitude and vibration suppression of a flexible spacecraft using energy-based actuators switching mechanism
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DOI: 10.1016/j.ast.2018.09.010
Abstract: Abstract A novel energy-based switching logic scenario to design a hybrid thruster/reaction wheel (RW) system is investigated for active vibration suppression of a flexible spacecraft embedded with collocated and Non-collocated configuration of Piezoelectric patches. The… read more here.
Keywords: flexible spacecraft; energy; vibration; control ... See more keywords