DocumentCode :
1873452
Title :
Optimal tuning of sliding mode controller parameters using LQR input trend
Author :
Azad, Reza Khoshrooz ; Banazadeh, Afshin ; Ahadi, Amirhosein
Author_Institution :
Dept. of Aerosp. Eng., Sharif Univ. of Technol., Tehran, Iran
fYear :
2012
fDate :
6-8 Sept. 2012
Firstpage :
297
Lastpage :
303
Abstract :
This paper presents a novel method fortuning the parameters of an sliding mode (SM) controller to obtain near-optimal performance. In order to do so the Linear Quadratic Regulator (LQR) was implemented on a linearized system. The input history of the LQR was used as a reference to obtain an optimal space for sliding mode controller parameters. Afterwards, the optimal space boundaries were dedicated to Genetic Algorithm (GA) to search for the optimal parameter for the nonlinear model. Also, the center of the obtained optimal space was used as an initial guess to the Particle Swarm Optimization (PSO) Algorithm. The proposed algorithm was implemented to regulate SM controller for the attitude control of a virtual satellite with uncertainly on inertia matrix. The proposed method also eliminates the heavy burden of trial and error and promises to deliver near-optimal performance that is considered as an important merit of the present study.
Keywords :
genetic algorithms; linear quadratic control; linear systems; particle swarm optimisation; variable structure systems; LQR input trend; genetic algorithm; linear quadratic regulator; linearized system; near optimal performance; nonlinear model; optimal space boundaries; optimal tuning; particle swarm optimization; sliding mode controller; Aerospace electronics; Birds; Equations; History; Mathematical model; Satellites; Tuning; Genetic Algorithm; Particle swarm optimization; Sliding mode controller; attitude control; optimal parameter tuning;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Systems (IS), 2012 6th IEEE International Conference
Conference_Location :
Sofia
Print_ISBN :
978-1-4673-2276-8
Type :
conf
DOI :
10.1109/IS.2012.6335151
Filename :
6335151
Link To Document :
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