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• W4210372912 abstract "This chapter investigates the robust state feedback nonfragile attitude control problem for uncertain spacecraft, and the problem explored here is subject to H∞ performance constraint, quadratic stability, external disturbances, controller perturbation, and control input saturation. The model of spacecraft attitude control system is introduced and transformed into a state-space form with parameter uncertainty. Based on Lyapunov theory, sufficient conditions for the existence of a robust state feedback nonfragile controller are given based on linear matrix inequalities (LMIs) in terms of additive perturbation and multiplicative perturbation. Then, the design of a nonfragile controller subject to required constraints is regarded as a convex optimization problem based on LMIs. By solving LMIs to obtain an optimal feasible solution that satisfies all the constraints of the problem and optimizes the objective function, the controller gain matrix can be precisely obtained. Based on the obtained controller, the spacecraft attitude control problem can be solved. The simulation results also demonstrate the effectiveness of the proposed control method." @default.
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• W4210372912 date "2022-01-01" @default.
• W4210372912 modified "2023-09-28" @default.
• W4210372912 title "State feedback nonfragile control" @default.
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• W4210372912 doi "https://doi.org/10.1016/b978-0-323-99005-9.00002-x" @default.
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