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A Software Update Technique for Aircraft Missiles based on MIL-STD-1760

MIL-STD-1760 기반 항공기용 유도탄 소프트웨어 업데이트 기법

  • Lee, Seungyoun (The 1st Research and Development Institute, Agency for Defense Development) ;
  • Kim, Sungkwon (The 1st Research and Development Institute, Agency for Defense Development) ;
  • Lee, Hyunah (The 1st Research and Development Institute, Agency for Defense Development) ;
  • Cho, Dongsik (The 1st Research and Development Institute, Agency for Defense Development)
  • 이승연 (국방과학연구소 제1기술연구본부) ;
  • 김성권 (국방과학연구소 제1기술연구본부) ;
  • 이현아 (국방과학연구소 제1기술연구본부) ;
  • 조동식 (국방과학연구소 제1기술연구본부)
  • Received : 2018.03.08
  • Accepted : 2018.08.24
  • Published : 2018.10.05

Abstract

It is essential that weapons which are mounted on aircraft need to prove its reliability and safety during its developments. A guided missile should have high reliability and safety throughout various tests which are including ground tests, captive flight tests, detailed technical tests and operational tests. In these various tests, it is vital that software of each component in the guided missile should be easily updated in order to correct algorithms or errors. In this paper, we propose a software update technique based on MDTP(mass data transfer protocol) which are defined in MIL-STD-1760. The proposed techniques have the following advantages: First, software of each unit in a weapon can be updated through a test equipment without disassemble a guided missile. Second, development periods for a software update can be reduced by reusing MDTP. Third, we can easily maintenance of the software because it is based on standard. We proved its efficiency and validity through experiments. Therefore, the proposed technique should be effectively utilized for software update of a weapon mounted on an aircraft during development processes.

Keywords

References

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