DocumentCode :
2544181
Title :
Discrete-time fuzzy modeling and control & its application
Author :
Zhigang Yang ; Jinxiang Chen
Author_Institution :
Coll. of Electr. Eng., Hebei United Univ., Tangshan, China
fYear :
2012
fDate :
29-31 May 2012
Firstpage :
57
Lastpage :
61
Abstract :
Discrete-time fuzzy modeling and state feedback control are investigated for nonlinear systems. The considered nonlinear system is firstly estimated by a discrete-time T-S fuzzy model. A fuzzy state feedback controller is designed. The sufficient conditions for the existence of controller are derived via a linear matrix inequality (LMI) approach. The designed controller not only can guarantee that the closed-loop system is asymptotically stable and but also can get good control performances. The gains of controller are obtained by solving a set of LMIs. The presented approach is applied to control helicopter systems. In contrast to the existing results, the proposed method has several advantages: i). Transient time is short; ii). There is no overshoot; iii). External disturbances can be effectively reduced. A CE150 helicopter system example is given to show the effectiveness of our scheme.
Keywords :
aircraft control; asymptotic stability; closed loop systems; control system synthesis; discrete time systems; fuzzy control; helicopters; linear matrix inequalities; nonlinear control systems; state feedback; CE150 helicopter system; LMI; asymptotic stability; closed-loop system; discrete-time T-S fuzzy model; linear matrix inequality approach; nonlinear systems; state feedback control; transient time; Attitude control; Fuzzy systems; Helicopters; Mathematical model; Nonlinear systems; Stability analysis; State feedback; Fuzzy modeling; LMI; attitude control; fuzzy control; helicopter;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Fuzzy Systems and Knowledge Discovery (FSKD), 2012 9th International Conference on
Conference_Location :
Sichuan
Print_ISBN :
978-1-4673-0025-4
Type :
conf
DOI :
10.1109/FSKD.2012.6233892
Filename :
6233892
Link To Document :
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