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- W3080921657 abstract "A minimal actuator design is proposed for orbit-attitude control of a spacecraft. The actuator design includes a single thruster, fixed in the body frame, and a variable-speed control moment gyroscope (VSCMG) used for thrust vectoring. It is known that the full attitude cannot be controlled using a single VSCMG, but that a single axis is controllable. This paper develops a nonlinear control that is able to vector the thruster at discrete intervals or continuously. The closed-loop stability of the system is proved using Lyapunov stability theory for each control law. These control laws could enable high maneuverability of CubeSats, using either a single chemical (impulsive) or electric thruster (continuous). The controls are demonstrated, in simulation, with an application to a 12U CubeSat rendezvous using a single throttable electric thruster." @default.
- W3080921657 created "2020-09-01" @default.
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- W3080921657 date "2020-10-01" @default.
- W3080921657 modified "2023-09-25" @default.
- W3080921657 title "Control of a Thrust-Vectoring CubeSat Using a Single Variable-Speed Control Moment Gyroscope" @default.
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- W3080921657 doi "https://doi.org/10.2514/1.g005181" @default.
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