한국항행학회논문지 (Journal of Advanced Navigation Technology)

  • 제28권5호
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  • Pages.664-669
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  • 2024
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  • 1226-9026(pISSN)
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  • 2288-842X(eISSN)
한국항행학회 (The Korean Navigation Institute)
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항공기 무장/장착물 연동성 검증을 위한 실시간 통합점검시스템 설계 및 구현

Design and Implementation of a Real-time Integrated Inspection System to Verify Aircraft Armament/Equipment Interoperability

  • 김효중 (LIG넥스원 연구개발본부) ;
  • 김지민 (LIG넥스원 연구개발본부) ;
  • 박찬영 (LIG넥스원 연구개발본부) ;
  • 권병기 (LIG넥스원 연구개발본부)
  • Hyo-Joung Kim (R&D Center of LIGNex1Co, Ltd) ;
  • Ji-Min Kim (R&D Center of LIGNex1Co, Ltd) ;
  • Chan-Young Park (R&D Center of LIGNex1Co, Ltd) ;
  • Byung-Gi Kwon (R&D Center of LIGNex1Co, Ltd)
  • 투고 : 2024.09.27
  • 심사 : 2024.10.29
  • 발행 : 2024.10.31
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초록

국내에서 한국형 전투기 개발이 진행되고 있다. 이로 인해서 다양한 임무를 수행할 수 있는 무장/장착물이 장착되어 운용될 예정이다. 항공기와 무장/장착물이 성공적으로 장착되고, 운용되기 위해서는 연동 표준을 기반으로 설계 및 개발되어야 하며, 절차에 따라 동작해야 한다. 그리고 많은 반복 시험을 통해서 안전성과 신뢰성을 검증해야 한다. 본 논문에서는 반복 시험을 수행함에 따라 소모되는 자원(시간, 비용, 인력)을 최적화하기 위해서 항공기 표준 인터페이스(MIL-STD-1760)에 따라 점검시스템을 제작하고, 항공기 연동 절차를 실시간으로 수행할 수 있는 소프트웨어를 개발해서 무장/장착물의 연동성을 사전에 검증할 수 있는 통합점검시스템을 확보하였다.

Recently, the development of a Korean fighter jet is underway in Korea. As a result, various armament/equipment that can perform various missions will be installed and linked. In order for the aircraft and armament/equipment to be successfully installed and linked, they must be designed and developed based on linkage standards and must operate according to the operating procedures. In addition, safety and reliability must be verified through many repeated tests. In this paper, in order to optimize the resources (time, cost, manpower) consumed by performing repeated tests, an inspection system was developed according to the MIL-STD-1760, an airborne standard interface, and software that can perform aircraft linkage procedures in real time was installed to secure an integrated inspection system that can verify the linkage of armament/equipment in advance.

키워드

참고문헌

  1. U.S. Department of Defense, Aircraft/store electrical interconnection system(MIL-STD-1760E), 24 Oct 2007. Retrieved from https://quicksearch.dla.mil/qsDocDetails.aspx?ident_number=37120.
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  3. T. Kim, K. Park, J. Kim, J. Jung, and B. Kwon, "A case study on MIL-STD-1760E based test bench implementation for aircraft-weapon interface testing," Journal of Advanced Navigation Technology, Vol. 22, No. 2, pp. 57-63, Apr. 2018. DOI: https://doi.org/10.12673/jant.20 18.22.2.57
  4. H. Kim, Y. Kim, and B. Kwon, "Design and implementation of test system for safety separation and performance verification of aircraft weapons/equipment," Journal of Advanced Navigation Technology, Vol. 26, No. 2, pp. 47-53, Apr. 2022. DOI: https://doi.org/10.12673/jant.2022.26.2 47
  5. S. Choi, J. Lee, J. Kim, S. Lee, and J. Jung, "Analysis of the correlation between armament/store integration criteria and aircraft launch missile development process," Journal of Advanced Navigation Technology, Vol. 22, No. 2, pp. 84-89, Apr. 2018. DOI: https://doi.org/10.12673/jant.2018.22.2.57.
  6. S. Lee, S. Kim, H. Lee, and D. Cho, "A software update technique for aircraft missiles based on MIL-STD-1760," Journal of the KIMST, Vol. 21, No. 5, pp. 649-657, Aug. 2018. DOI: https://doi.org/10.9766/KIMST.2018.21.5.649
  7. U.S. Department of Defense, Digital time division command/response multiplex data bus(MIL-STD-1553B), 5 Jan 1996. Retrieved from https://quicksearch.dla.mil/qsDocDetails.aspx?ident_number=36973