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J. KIMS Technol > Volume 19(5); 2016 > Article
Journal of the Korea Institute of Military Science and Technology 2016;19(5):606-612.
DOI: https://doi.org/10.9766/KIMST.2016.19.5.606   
Captive Flight Test System Configuration and Verification for Multi-mode Guidance Missile System
Inchul Park, Wonyoung Heo, Yongho Lee, Seyoung Jeong
1PGM R&D Center, LIG Nex1 Co., Ltd.
2The 1st Guided Weapon System PEO, Agency for Defense Development
복합유도방식이 적용된 유도탄의 탑재비행시험(CFT) 시스템 구성 및 검증
박인철, 허원영, 이용호, 정세영
1LIG넥스원(주) 유도무기연구소
2국방과학연구소 제1유도무기체계개발단
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.
Key Words: Captive Flight Test, Multi-mode, Command Guidance, Distributed Weapon System


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