Distributed optimal control allocation for 6-dof spacecraft with redundant thrusters
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DOI: 10.1016/j.ast.2021.106971
Abstract: Abstract Control allocation for 6-dof spacecraft maneuvers is considered. Retired spacecraft, whose own control system is inoperable, can be reused by installing multiple cellular thruster modules to provide thrusts for translational and rotational control. Such… read more here.
Keywords: allocation; allocation dof; dof spacecraft; thrust allocation ... See more keywords