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Avionics Architecture Design for Military Unmanned Aerial Vehicles

군용 무인기의 항공전자 아키텍처 설계

  • Jae Ick, Shim (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development) ;
  • Jae Won, Choi (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development) ;
  • Yong Tae, Kim (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development) ;
  • Dong Wan, Yoo (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development) ;
  • Kook Bo, Yang (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development) ;
  • Hyun Seok, Ha (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development) ;
  • Sang Jin, Kim (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development) ;
  • Seung Yul, Lee (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development) ;
  • Sang Jun, Jung (The 1st Aero System PMO, Aerospace Technology Research Institute, Agency for Defense Development)
  • 심재익 (국방과학연구소 항공기술연구원 제1항공체계단) ;
  • 최재원 (국방과학연구소 항공기술연구원 제1항공체계단) ;
  • 김용태 (국방과학연구소 항공기술연구원 제1항공체계단) ;
  • 유동완 (국방과학연구소 항공기술연구원 제1항공체계단) ;
  • 양국보 (국방과학연구소 항공기술연구원 제1항공체계단) ;
  • 하현석 (국방과학연구소 항공기술연구원 제1항공체계단) ;
  • 김상진 (국방과학연구소 항공기술연구원 제1항공체계단) ;
  • 이승열 (국방과학연구소 항공기술연구원 제1항공체계단) ;
  • 정상준 (국방과학연구소 항공기술연구원 제1항공체계단)
  • Received : 2022.08.13
  • Accepted : 2022.11.30
  • Published : 2022.12.05

Abstract

This paper describes the design of the avionics architecture for military unmanned aerial vehicles considering the airworthiness requirements for the first time. This design considers the redundancy in the system data bus and the power system and the data link system to meet the system safety requirements of the airworthiness requirements of military UAVs. This avionics architecture design has been verified through the system integration test and the flight test after manufacturing the UAV.

Keywords

References

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