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• W2773960757 abstract "For the missile system with external disturbances and parametric uncertainties, the problem of composite anti-disturbance autopilot design is considered with angle constraint. First, a nonlinear disturbance observer is designed for missile system. Second, using dynamic surface control technique, a composite anti-disturbance autopilot is developed for missile systems. Third, the stability analysis is given by Lyapunov function theory and the uniform ultimate boundedness is obtained for the closed-loop system signals. Finally, a simulation result is presented to demonstrate the effectiveness of the proposed method." @default.
• W2773960757 created "2017-12-22" @default.
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• W2773960757 date "2017-10-01" @default.
• W2773960757 modified "2023-10-14" @default.
• W2773960757 title "Composite anti-disturbance autopilot design for missile system with angle constraint" @default.
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• W2773960757 doi "https://doi.org/10.1109/iecon.2017.8217053" @default.
• W2773960757 hasPublicationYear "2017" @default.
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