Proceedings of the KIEE Conference (대한전기학회:학술대회논문집)

The Korean Institute of Electrical Engineers (대한전기학회)
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Mathematical Analysis of Model Helicopter

모형헬리콥터의 수학적 해석

  • Kim, Y.O. (School of Electronics Eng. Ajou Univ.) ;
  • Lee, K.W. (School of Electronics Eng. Ajou Univ.) ;
  • Lee, J.S. (School of Electronics Eng. Ajou Univ.) ;
  • Hong, S.K. (School of Electronics Eng. Ajou Univ.)
  • 김양욱 (아주대학교 대학원 전자공학부) ;
  • 이광원 (아주대학교 전자공학부) ;
  • 이자성 (아주대학교 전자공학부) ;
  • 홍석교 (아주대학교 전자공학부)
  • Published : 1999.07.19
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Abstract

Helicopter system is regarded as a challenging example in multivariable robust control application since the dynamics of helicopter is highly coupled and nonlinear. In this paper, Dynamic equations for model helicopter at hover are derived. Various system properties are stated with respect to control of the attitude of the vehicle. A linearized model is used to analyse the system stability and to design the attitude controller. The simulation results of LQG controller are presented.

Keywords