한국지능시스템학회:학술대회논문집 (Proceedings of the Korean Institute of Intelligent Systems Conference)
- 한국퍼지및지능시스템학회 1998년도 The Third Asian Fuzzy Systems Symposium
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- Pages.438-442
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- 1998
Attitude Control of Helicopter using Fuzzy Inference Technique
- Lee, Joon-Tark (Dept. of Electrical Engineering, Dong-A University) ;
- Lee, Oh-Keol (Dept. of Electrical Engineering, Dongeui Technical Junior College) ;
- Shin, Song-Ho (Dept. of Electrical Engineering, Pusan Information College) ;
- Park, Doo-Hwan (Dept. of Electrical Engineering , Dong-A University) ;
- Gon, Ha-Hong (Dept. of Electronical Engineering, Dong-Eui University)
- 발행 : 1998.06.01
초록
The helicopter system is non-linear and complex. Futhermore, because of absence of an accurate mathematical model, it is difficult accurately to control its attitude. But we can control the non-modeled system with the uncertainty and unstructure using the fuzzy control algorithm. Therefore, we apply optimized fuzzy controllers for the control of its elevation angle and azimuth one using expert's intuitions and knowledges. The simulation and experimental results of the hellicopter simulator CE150 with MATLAB shall be introduced.