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- W4289883912 abstract "A study of finite-time control is made for rigid–flexible coupling satellite in large-angle rapid maneuver. A first-order approximation rigid–flexible coupling dynamic model is set up, with the consideration of serious coupling effect between the deformation of flexible appendages and large scope spatial movement of the central body. Given that all states including flexible vibration measurements of the satellite system can be measured, a nonsingular fast terminal sliding mode (NFTSM) state feedback controller is designed in the presence of model uncertainties and disturbances. The finite-time stability of the system is proved by the Lyapunov theory. Then a modified NFTSM output feedback controller is proposed in the condition that the flexible vibration measurements are not available, and the finite-time output feedback control is based on measurements of angle and angular velocity only. At last, numerical simulations of the proposed controllers and comparisons with the controller in present literature together demonstrate the finite-time stability of the control method proposed." @default.
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- W4289883912 date "2022-01-01" @default.
- W4289883912 modified "2023-09-26" @default.
- W4289883912 title "Finite-time output feedback attitude control" @default.
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- W4289883912 doi "https://doi.org/10.1016/b978-0-323-95455-6.00005-6" @default.
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