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
Online-Zugang:	Volltext
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