모형 헬리콥터의 자세 제어

Attitude Control of Simulated Helicopter

  • Kim, H.B. (Dept. of Electrical Eng., Dong-A Univ.) ;
  • Park, D.H. (Dept. of Electrical Eng., Dong-A Univ.) ;
  • Kim, T.W. (Dept. of Electrical Eng., Dong-A Univ.) ;
  • Ha, H.G. (Dept. of Electronical Eng., Dong-Eui Univ.) ;
  • Lee, J.T. (Dept. of Electrical Eng., Dong-A Univ.)
  • 발행 : 1997.11.29

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 therefore, we propose a fuzzy control technique to control efficiently its elevation angle and azimuth one. This controller is on the basis of expert's knowledges and his experiences. The simulation results using MATLAB are introduced.

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