Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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Realization of Flight Modes for Light General Aviation Flight Director using Stateflow

Stateflow를 이용한 소형제트기 Flight Director의 비행모드 구현

  • 이장호 (한국항공우주연구원 첨단비행제어팀) ;
  • 김성필 (한국항공우주연구원 첨단비행제어팀) ;
  • 성기정 (한국항공우주연구원 첨단비행제어팀) ;
  • 김웅태 (한국항공우주연구원 항공미래기술연구실)
  • Published : 2007.09.30
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Abstract

Flight modes of automatic flight control system for light general aviation flight deck. Garmin G1000, were realized using Stateflow. In developing aircraft, it is difficult to verify the operational flight program in particular branch statement because developer can not see any visual logical steam. So, Stateflow has been used to visualize logical stream, transition from one flight mode to another flight mode. The performance was approved by applying flight mode transition conditions of G1000 to proposed transition system that is composed of states, switches, events, data and transition conditions. DURMI-II was used as 6-DOF simulation model.

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