DocumentCode :
2956804
Title :
Controller design using fuzzy logic for a twin rotor MIMO system
Author :
Islam, Badar Ul ; Ahmed, Nisar ; Bhatti, Daud Latif ; Khan, Shahid
Author_Institution :
Fac. of Electron. Eng., Ghulam Ishaq Khan Inst. of Eng. Sci. & Technol., Swabi, Pakistan
fYear :
2003
fDate :
8-9 Dec. 2003
Firstpage :
264
Lastpage :
268
Abstract :
The paper discusses the design of a fuzzy logic controller for a twin rotor MIMO system. The system has three degrees of freedom, but we have designed the controller for two degrees of freedom (DOF) only, i.e., travel and elevation. The controller is designed such that a change in one degree should have minimum effect on the other and overall the system should remain stable. We have designed two fuzzy logic controllers: one for travel control and one for elevation: both are designed in MATLAB and have Sugeno inference. For the twin rotor MIMO system, commonly known as the helicopter problem, many conventional controllers exist. Our controller´s performance had to be better than, or at least equal to, their´s. To test the controller on a practical system was not possible, therefore we used simulations to benchmark the performance of the fuzzy logic controller. The simulation results show that the system performance with a fuzzy logic controller is superior to the system performance with a conventional PID or LQR controller, over the whole range of operating conditions.
Keywords :
MIMO systems; control system CAD; fuzzy control; fuzzy logic; inference mechanisms; PID controller; Sugeno inference; degrees of freedom; elevation control; fuzzy control; fuzzy logic controller design; helicopter problem; travel control; twin rotor MIMO system; Benchmark testing; Control systems; Fuzzy logic; Helicopters; Logic testing; MATLAB; MIMO; System performance; System testing; Three-term control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Multi Topic Conference, 2003. INMIC 2003. 7th International
Print_ISBN :
0-7803-8183-1
Type :
conf
DOI :
10.1109/INMIC.2003.1416722
Filename :
1416722
Link To Document :
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