항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제9권4호
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  • Pages.1-7
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  • 2015
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  • 1976-6300(pISSN)
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  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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FMI 표준을 활용한 관절형 로터/공력 연계시뮬레이션

Articulated Rotor/Aerodynamics Co-Simulation Using FMI Standard

  • 백승길 (한국항공우주연구원 회전익기연구팀) ;
  • 박중용 (한국항공우주연구원 회전익기연구팀)
  • Paek, Seung-Kil (Rotorcraft Research Team, Korea Aerospace Research Institute) ;
  • Park, Joongyong (Rotorcraft Research Team, Korea Aerospace Research Institute)
  • 투고 : 2015.10.15
  • 심사 : 2015.12.04
  • 발행 : 2015.12.31
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초록

The purpose of this research is to develop co-simulation methodology of codes developed in different modeling and simulation environment. We develop aerodynamic FMU(Functional Mock-up Unit) meeting FMI(Functional Mock-up Interface) specification version2 utilizing Legacy FORTRAN aerodynamic code based on unsteady vortex lattice method. It is concluded that making FMU is possible utilizing Legacy code made in any language which can be compiled and linked with object in FMI API coded in C language. This paper explains QTronic's method of using FMU SDK(Software Development Kit) and suggestion for using FORTRAN properly. Finally, we make articulated rotor/aerodynamics co-simulation by integrating aerodynamics FMU and rotor FMU developed by Modelica.

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참고문헌

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