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• W2022344546 startingPage "442" @default.
• W2022344546 abstract "The problem of robust control of spacecraft circular orbit rendezvous system subject to input saturation is studied in this paper. The relative model with parameter uncertainties caused by linearization error and saturation nonlinearity is established based on C–W equation. By combining the parametric Riccati equation and the existing gain scheduling technique, a new robust gain scheduling controller is proposed to solve the robust control problem. By scheduling the design parameters online, the convergence rate of the state can be improved. With the designed controller, the spacecraft orbit rendezvous is accomplished successfully. Numerical simulations show the effectiveness of the proposed approach." @default.
• W2022344546 created "2016-06-24" @default.
• W2022344546 creator A5043623971 @default.
• W2022344546 creator A5046225712 @default.
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• W2022344546 date "2015-04-01" @default.
• W2022344546 modified "2023-09-26" @default.
• W2022344546 title "Robust gain scheduled control of spacecraft rendezvous system subject to input saturation" @default.
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• W2022344546 doi "https://doi.org/10.1016/j.ast.2015.02.002" @default.
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