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J. KIMS Technol > Volume 17(1); 2014 > Article
Journal of the Korea Institute of Military Science and Technology 2014;17(1):135-141.
DOI: https://doi.org/10.9766/KIMST.2014.17.1.135   
A Study on Measuring the Misaligned Angle between Seeker and Inertial Navigation System
Taehoon Kim, Hojun Lee, Jinseob Jeong, Hongseok Choi
Anti-ship Missile PEO, Agency for Defense Development
탐색기와 관성항법장치 간 비정렬각 측정 기법 연구
김태훈, 이호준, 정진섭, 최홍석
국방과학연구소 대함유도무기체계단
In order to guide a flying object which uses a seeker(SKR) and an inertial navigation system(INS) properly, we should confirm that axes of both equipments are aligned in the scope expected. In this paper we have proposed a method to measure the misaligned angle between a SKR and an INS during the system integration procedure. And we expanded this method to measure misalignments between several SKRs and an INS in case of captive flight test.
Key Words: Seeker, Inertial Navigation System, Misaligned Angle, Captive Flight Test


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