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- W1566561983 abstract "In this paper, we demonstrate that, in fact, two momentum wheel actuators can be used to control the attitude of a rigid spacecraft and that arbitrary reorientation maneuvers of the spacecraft can be accomplished in a specific sense. The complete spacecraft dynamics cannot be stabilized to an equilibrium attitude. However, the spacecraft equations are small time locally controllable in a reduced nonlinear sense. The reduced spacecraft dynamics cannot be asymptotically stabilized to an equilibrium attitude using a time-invariant continuous feedback control law, but a discontinuous feedback control strategy is constructed which asymptotically stabilizes an equilibrium attitude of the spacecraft. Consequently, arbitrary reorientation of the spacecraft can be accomplished using this discontinuous feedback control strategy." @default.
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- W1566561983 date "1992-08-01" @default.
- W1566561983 modified "2023-09-24" @default.
- W1566561983 title "Attitude stabilization of a rigid spacecraft using momentum wheel actuators operating in a failure mode" @default.
- W1566561983 hasPublicationYear "1992" @default.
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