한국군사과학기술학회지 (Journal of the Korea Institute of Military Science and Technology)

  • 제25권6호
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  • Pages.628-636
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  • 2022
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  • 1598-9127(pISSN)
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  • 2636-0640(eISSN)
한국군사과학기술학회 (The Korea Institute of Military Science and Technology)
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군용 무인기의 항공전자 아키텍처 설계

Avionics Architecture Design for Military Unmanned Aerial Vehicles

  • 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)
  • 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)
  • 투고 : 2022.08.13
  • 심사 : 2022.11.30
  • 발행 : 2022.12.05
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초록

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.

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참고문헌

  1. Sung Woo Kim, Jae Ick Shim, Wang Guk Lee, Woo Jin Lee, Dae Yeon Won, "A Study on the Trend an Avionics System Architecture Development for UAV," Journal of the Korea Institute of Military Science and Technology, Vol. 17, No. 4, pp. 436~447, 2014. https://doi.org/10.9766/KIMST.2014.17.4.436
  2. G. Loegering, D. Evans, "The Evolution of the Global Hawk and MALD Avionics Systems," Digital Avionics System Conference, 24-29, Oct., 1999.
  3. NATO Standardization Agency, "STANAG 4671 (Edition 1) - Unmanned Aerial Vehicles Systems Airworthiness Requirements(USAR)," 2009.
  4. NATO Standardization Agency, "STANAG 4586 Standard Interfaces of UAV Control System(UCS) for NATO UA Interoperability-Interface Control Document," Edition 4, pp. 3~7, April 2017.
  5. John M. Borky, "Payload Technologies and Applications for Uninhabited Air Vehicles(UAVs)," IEEE Aerospace Conference, Vol. 3, pp. 267-283, Feb. 1997.
  6. Schaefer, R., "Unmanned Aerial Vehicle Reliability Study," Office of the Secretary of Defense, February 2003.
  7. Jae Ick Shim, Byung Wook Choi, Sang Soon Park, Dong Wan Yoo, Seon Mi Cho, Jin ku Byun, Jae Geun Lim, Jae Hwa Lee, "A System Level HILS Platform Design for the Integrated Verification of the Operational Logic and the Flight Performance of UAS," 2015 SASE Spring Conference, 79-84, May 2015.
  8. Jae Ick Shim, "UAV SIL Development for the Verification of the Integrated Operability of the UAV System," KIMST Annual Conference Proceedings pp. 1737-1738, June 2022.