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J. KIMS Technol > Volume 15(4); 2012 > Article
Journal of the Korea Institute of Military Science and Technology 2012;15(4):374-380.
DOI: https://doi.org/10.9766/KIMST.2012.15.4.374   
A Study on Methods of Measuring and Compensating Misalignment between Inertial Sensor Body and Housing Frame
Hae-Sung Yu, Tae-Hoon Kim, Cheon-Joong Kim, Youn-Seon Lee, Heung-Won Park
관성항법장치의 관성 센서축과 하우징 축과의 비정렬 측정과 보상에 관한 연구
유해성, 김태훈, 김천중, 이윤선, 박흥원
국방과학연구소
Abstract
In guided missile systems, reducing terminal-position error is the primary objective of the inertial navigation system. As a seeker is used to sense and track a target, the critical function of the inertial navigation system is to provide the seeker with accurate missile attitude information and help the seeker to keep tracking a target continuously. As inertial sensor body and missile body alignment errors are taken into account, it is desirable to minimize the alignment errors between the missile seeker and the attitude of inertial navigation system. Among the alignment errors, this paper addresses the methods of measuring and compensating misalignment between inertial sensor body and housing frame and shows test results of several experiments.
Key Words: Inertial Sensor, Misalignment, Seeker, Inertial Navigation System


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