DocumentCode :
558777
Title :
Robust control design based-on integral sliding-mode for systems with norm-bounded uncertainties
Author :
Feng, Chieh-Chuan ; Lin, Yung-Yeh
Author_Institution :
Dept. of Electr. Eng., I-Shou Univ., Kaohsiung, Taiwan
fYear :
2011
fDate :
26-29 Oct. 2011
Firstpage :
1178
Lastpage :
1183
Abstract :
Based on the integral sliding-mode control that copes with norm-bounded matched uncertainties, a robust control of L2-gain performance measure subsequently applied to the system is proposed to handle both nonlinearities and unmatched uncertainties. The similar issue through the use of higher order multi-mode model has been relaxed. Instead of using exact known multi-mode to express the uncertain system, the norm-bound convex set is a concise way of expressing the model and hence, higher order models needed in the computation can be avoided. In this paper integral sliding-mode control robustly nullifies the matched uncertainties from the first beginning of the process and then, once in the sliding mode, the nonlinearities and unmatched uncertainties are further compensated by the quadratic stability with L2-gain performance measure to not only stabilize the system but also ensure the satisfaction of performance. The effectiveness is shown in a numerical example.
Keywords :
control nonlinearities; control system synthesis; robust control; stability; uncertain systems; variable structure systems; L2-gain performance; higher order multimode model; integral sliding mode control; nonlinearities; norm-bounded uncertainty; quadratic stability; robust control design; Linear matrix inequalities; Measurement uncertainty; Robust control; Robustness; Sliding mode control; Uncertain systems; Uncertainty; L2-gain; Sliding-mode control; integral sliding-mode control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation and Systems (ICCAS), 2011 11th International Conference on
Conference_Location :
Gyeonggi-do
ISSN :
2093-7121
Print_ISBN :
978-1-4577-0835-0
Type :
conf
Filename :
6106106
Link To Document :
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