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SIMULINK를 이용한 헬리콥터 추진시스템의 성능해석에 관한 연구
공창덕(Chang-Duk Kong),기자영(Ja-Young Ki),고성희(Seong-Hee Kho),김재환(Jaehwan Kim) 한국추진공학회 2008 한국추진공학회지 Vol.12 No.1
In this study a turboshaft engine for a helicopter propulsion system was modeled using SIMULINK and the components maps were generated from the limited performance deck data provided by engine supplier using a hybrid method with the genetic algorithms and the system identification method. In order to verify the SIMULINK performance model and the component maps generated by the hybrid method, the steady-state performance analysis results were compared with the performance data provided by engine manufacturer. In this investigation, it was confirmed that the analysis results by the proposed model are closely met with those by engine manufacturers data.