Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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Control Law Design Optimization for Helicopter Handling Qualities Using CONDUIT

CONDUIT을 이용한 헬리콥터 조종성에 대한 비행제어법칙 설계 및 최적화

  • 이장호 (한국항공우주연구원 항공제어전자팀) ;
  • 김응태 (한국항공우주연구원 항공제어전자팀) ;
  • 이석천 (한국항공우주연구원 항공제어전자팀) ;
  • 유혁 (한국항공우주연구원 항공제어전자팀)
  • Received : 2012.05.09
  • Accepted : 2012.06.15
  • Published : 2012.06.30
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Abstract

The evaluation of simulation models against ADS-33 quantitative rotorcraft handling qualities metrics has, in the past, been a time consuming effort, involving many individual analyses in both the time and frequency domains. Manual tuning of control system parameters to meet handling qualities and performance specifications has been cumbersome and complicated. Performing rigorous trade-off studies for numerous variations in the control system is too time consuming to be practicable. With the complex interaction of time- and frequency based specifications for the closed- and broken-loop responses, it is difficult to know if the design makes the most effective use of the available control power. The Control Designer's Unified Interface (CONDUIT) software makes possible rapid optimization and trade-offs of design configurations against handling qualities specifications.

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