Proceedings of the IEEK Conference (대한전자공학회:학술대회논문집)

The Institute of Electronics and Information Engineers (대한전자공학회)
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Turbojet Engine Control using Fuzzy Inference Method

퍼지추론 기법에 의한 터보제트 엔진제어

  • 지민석 (한국항공대학교 항공전자공학과) ;
  • 이영찬 (한국항공대학교 항공전자공학과) ;
  • 이강웅 (한국항공대학교 항공전자공학과) ;
  • 기자영 (조선대학교 우주항공공학과) ;
  • 공창덕 (조선대학교 우주항공공학과)
  • Published : 2003.07.01
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Abstract

In this paper we propose a turbojet engine controller based on fuzzy inference method. Fuel flow control input is designed by fuzzy inference in order to avoid surge and flame-out during acceleration and deceleration. Acceleration and deceleration demands are used as control commands, which can achieve effective performance without surge and flame-out.

Keywords