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- W2100076805 abstract "This study deals with the problem of integrated translation and rotation finite-time maneuver of a rigid spacecraft with actuator misalignment. In view of the system natural couplings, the coupled translational and rotational dynamics of the spacecraft is derived, where a thruster configuration with installation misalignment is taken into account. An integrated finite-time control strategy is proposed by using terminal sliding mode technique to enable the spacecraft to track command position and attitude in a pre-determined time. Within the Lyapunov framework, the finite-time stability of the closed-loop system is guaranteed in the presence of the thruster misalignment and bounded disturbances. A scenario numerical simulation demonstrates the effect of the designed control strategy." @default.
- W2100076805 created "2016-06-24" @default.
- W2100076805 creator A5026612109 @default.
- W2100076805 creator A5043623971 @default.
- W2100076805 date "2012-01-01" @default.
- W2100076805 modified "2023-10-16" @default.
- W2100076805 title "Integrated translational and rotational finite-time maneuver of a rigid spacecraft with actuator misalignment" @default.
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- W2100076805 doi "https://doi.org/10.1049/iet-cta.2011.0413" @default.
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