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• W2171142890 abstract "The problem of attitude tracking for a flexible spacecraft is studied in this paper. A finite -time sliding mode controller is applied to quaternion-based attitude control for tracking maneuvers with external disturbances. The proposed sliding mode control law is developed by using a terminal sliding mode control algorithm which is able to guarantee finite time reachability of given desired attitude motion of a flexible spacecraft. By using the second method of Lyapunov and terminal sliding mode control concepts, stability of the closed-loop system can be achieved in finite time. An example of multiaxial attitude maneuvers is presented. Simulation results are included to demonstrate and verify the usef ulness of the developed controller." @default.
• W2171142890 created "2016-06-24" @default.
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• W2171142890 creator A5031531588 @default.
• W2171142890 date "2014-12-24" @default.
• W2171142890 modified "2023-09-24" @default.
• W2171142890 title "Robust Control with Finite Time Convergence for Flexible Spacecraft Attitude Tracking" @default.
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• W2171142890 hasPublicationYear "2014" @default.
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