Singular perturbation analysis of discrete-time output feedback sliding mode control with disturbance attenuation

We address the output feedback sliding mode control problem for a sampled data linear system with disturbances. By taking into account the disturbance compensation, a deadbeat high gain output feedback control strategy with additional dynamics is able to attenuate the disturbances. It is shown that...

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Veröffentlicht in:2009 American Control Conference S. 757 - 762
Hauptverfasser: Nguyen, T., Wu-Chung Su, Gajic, Z.
Format: Tagungsbericht
Sprache:Englisch
Veröffentlicht: IEEE 01.06.2009
Schlagworte:
Aerospace control
Aircraft manufacture
Attenuation
Attitude control
Closed loop systems
Control systems
Linear feedback control systems
Linear systems
Output feedback
Sliding mode control
ISBN:142444523X, 9781424445233
ISSN:0743-1619
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Zusammenfassung:We address the output feedback sliding mode control problem for a sampled data linear system with disturbances. By taking into account the disturbance compensation, a deadbeat high gain output feedback control strategy with additional dynamics is able to attenuate the disturbances. It is shown that the closed loop system exhibits both singularly perturbed and weakly coupled characteristics. A numerical example of an aircraft attitude output feedback control is provided to demonstrate the effectiveness of the proposed approach.
ISBN:142444523X
9781424445233
ISSN:0743-1619
DOI:10.1109/ACC.2009.5160654