Title :
Stable Fuzzy Controller Design for a Nonlinear Helicopter Model
Author :
Tahersima, Hanif ; Kaveh, Mahdi ; Fatehi, Alireza
Author_Institution :
K.N.Toosi of Tech Univ., Tehran
Abstract :
In this paper, a method for designing a stable fuzzy controller for nonlinear systems with the ability of reference tracking is introduced. First, the nonlinear equations of model helicopter is presented which is modeled by Humusoft Inc. based on linearization around system operating points, a T-S fuzzy model is represented. Then, based on state feedback a T-S fuzzy controller is developed, which its stability is guaranteed by nonlinear matrix Inequalities (LMI). These inequalities are solved using convex optimization methods by means of Matlab and LMI toolbox. In the following, tracking problem, control signal constraints are discussed.
Keywords :
aircraft control; control system synthesis; convex programming; fuzzy control; helicopters; linear matrix inequalities; mathematics computing; nonlinear control systems; stability; state feedback; tracking; LMI toolbox; Matlab; Takagi-Sugeno fuzzy controller; control signal constraints; convex optimization methods; nonlinear helicopter model; nonlinear matrix Inequalities; reference tracking; stable fuzzy controller design; state feedback; Control systems; Design methodology; Fuzzy control; Fuzzy systems; Helicopters; Mathematical model; Nonlinear control systems; Nonlinear equations; Nonlinear systems; State feedback;
Conference_Titel :
Innovative Computing, Information and Control, 2007. ICICIC '07. Second International Conference on
Conference_Location :
Kumamoto
Print_ISBN :
0-7695-2882-1
DOI :
10.1109/ICICIC.2007.536