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• W2384366249 abstract "This paper deals with the problem of attitude regulation control of rigid satellite subject to control input saturation,external disturbance and parametric uncertainty.In the proposed controller,a single parameter is adjusted dynamically in such a fashion that it is possible to prove that both attitude and angular velocity will tend to zero asymptotically.Lyapunov theory is employed to prove the global asymptotic stability of zero equilibrium points of the closed loop system.The controller is derived independent of satellite inertia matrix and thus robust to parametric uncertainty.Simulation results demonstrate that the control scheme realizes the attitude control under control saturation and implements the effective rejection problem for disturbances." @default.
• W2384366249 created "2016-06-24" @default.
• W2384366249 creator A5075312748 @default.
• W2384366249 date "2008-01-01" @default.
• W2384366249 modified "2023-09-23" @default.
• W2384366249 title "Satellite attitude regulation control subject to control Input saturation" @default.
• W2384366249 hasPublicationYear "2008" @default.
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