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http://dx.doi.org/10.6109/jkiice.2008.12.10.1822

Calibration of a Low Grade MEMS IMU Using a High Performance Reference Sensor  

Chang, Keun-Hyung (건국대학교)
Chun, Se-Bum (마이크로 인피니티)
Sung, Sang-Kyung (건국대학교)
Lee, Eun-Sung (한국항공우주연구원)
Jun, Hyang-Sig (한국항공우주연구원)
Lee, Young-Jae (건국대학교)
Abstract
Calibration of an MEMS inertial measurement unit is very important process for obtaining precise navigation performance. In this paper, one method is proposed to overcome a limitations on cost and efficiency using a relatively higher grade sensor and a rate table. The same dynamic input is applied to both the reference and the target sensors during and after calibration process, then the results are analyzed. The experimental results show that the proposed method is very effective and useful in practice.
Keywords
MEMS Inertial Sensor; Calibration; Reference Sensor;
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  • Reference
1 U.Krogmann, Identification Procedures for Strapd own-Sensor-Parameters by Laboratory Testing, DGON-Symposium, Sept.1978
2 Schmidt, G. T., Strapdown Inertial Systems Theory and Applications. Introduction and Overview, AGARD Lecture Series, No.95, 1978
3 D.H.Titterton and J.L.Weston, Strapdown inertial navigation technology, IEEE, 1997
4 D.K.Joos, Comparison of Typical gyro errors for Strapdown Applications, DGON-Symposium, Sept. 1977
5 Savage, P. G., Strapdown Inertial Navigation Integration Algorithm Design Part 1: Attitude Algorithms, Journal of Guidance, Control, and Dynamics, Vol 21, No 1, 1998
6 Stephen J.Huffman, IEEE Standard for Inertial Sensor Terminology , IEEE Std 528, 1994
7 박찬국, 진용, 원종석, "관성항법시스템을 위한 센서오차의 최적추정 기법", 한국항공우주학회지 26권 5호, pp.116-240, 1998
8 Savage, P. G., Strapdown Inertial Navigation Integration Algorithm Design Part 2: Velocity and Position Algorithms, Journal of Guidance, Control, and Dynamics, Vol 21, No 2, 1998
9 한국항공우주연구소, Technology Developmen t of the Inertial Navigation and Global Navigation Sarellite System, 과학기술부, 2000