23rd Congress of International Council of the Aeronautical Sciences, 8-13 September, 2002, Toronto, Canada
Paper ICAS 2002-7.4.2


FAST CALIBRATION TECHNIQUE FOR A GIMBALLED INERTIAL NAVIGATION SYSTEM

Y. J. Shin (1), J. H. Park (1), C. J. Kim (2)
(1) Agency for Defence Development, Republic of Korea; (2) Korea Aerospace Research Institute, Yuseong, Daejeon, Korea

Keywords: calibration, gimballed ins, kalman filtering, schuler factor

In this paper, we propose the fast calibration technique by Kalman filtering with the modified level axis Schuler error loop in which the Schuler factor is introduced in order to be able to change the Schuler period. This technique has led to enhanced estimation accuracy as well as reduced calibration test time.


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