DocumentCode :
381333
Title :
Maneuver simulation of a non-linear system using membership function optimization of a fuzzy logic controller
Author :
Zadeh, Hossein S.
Author_Institution :
Sch. of Bus. Inf. Technol., R. Melbourne Inst. of Technol., Vic., Australia
Volume :
5
fYear :
2002
fDate :
2002
Firstpage :
146584
Abstract :
This work is an ongoing investigation of attitude control (π/2 rad rotation) as well as vibration suppression of a very flexible structure. A nominal fuzzy logic controller had been designed and used as a basis for design of an optimized fuzzy controller. The optimization algorithm and procedure have been explained in an earlier paper. This paper presents simulation results of both the nominal and optimized systems. Clear improvement in the performance of the optimized controller in comparison to that of the nominal system is evident. A computer program is developed to animate results of the simulation in a three dimensional space. The program runs under GNU/Linux and uses GTK and OpenGL for visualization.
Keywords :
aerospace computing; artificial satellites; attitude control; control system synthesis; digital simulation; flexible structures; fuzzy control; nonlinear control systems; optimisation; vibration control; GNU/Linux; GTK; OpenGL; attitude control; computer program; flexible structure; fuzzy logic controller design; membership function optimization; nonlinear system; satellite maneuver simulation; simulation; solar panel deployment; spacecraft; vibration suppression; visualization; Animation; Computational modeling; Computer simulation; Control systems; Design optimization; Flexible structures; Fuzzy control; Fuzzy logic; Nonlinear control systems; Vibration control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1035399
Filename :
1035399
Link To Document :
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