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

The Korea Institute of Military Science and Technology (한국군사과학기술학회)
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Captive Flight Test System Configuration and Verification for Multi-mode Guidance Missile System

복합유도방식이 적용된 유도탄의 탑재비행시험(CFT) 시스템 구성 및 검증

  • 박인철 (LIG넥스원(주) 유도무기연구소) ;
  • 허원영 (국방과학연구소 제1유도무기체계개발단) ;
  • 이용호 (LIG넥스원(주) 유도무기연구소) ;
  • 정세영 (LIG넥스원(주) 유도무기연구소)
  • Received : 2015.11.26
  • Accepted : 2016.09.23
  • Published : 2016.10.05
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Abstract

A Captive Flight Test(CFT) is used to verify the performance of missile component such as seeker and guiding algorithm of missile. Recently most of surface to air missile adapts multi-mode guidance method which include command guidance and active/passive guidance. A CFT system for missile system adapting multi-mode guidance method consists of pod equipment, command transmitting system and measuring system. In this paper, we proposed CFT system and testing method for missile which adapt multi-mode guidance, and system integration procedure by using distributed missile system integration method and procedure. The proposed CFT system and system integration method was applied to CFT of surface to air missile, and brought successful result.

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References

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