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NTIS 바로가기항공우주시스템공학회지 = Journal of aerospace system engineering, v.16 no.5, 2022년, pp.94 - 101
조경환 (LIG넥스원 PGM2연구소) , 문상찬 (LIG넥스원 PGM2연구소) , 윤석창 (LIG넥스원 PGM2연구소) , 권승복 (LIG넥스원 PGM2연구소) , 김도형 (마이크로인피니티) , 양일영 (한국산업기술시험원)
In this paper, we have obtained the acceleration coefficient of the IMU (Inertial Measurement Unit) to prove reliability by analyzing the characteristic of the MEMS IMU installed in guided weapon systems for overseas export and the operating environment of the guided weapon system. Additionally, bas...
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