An implementation of INS calibration technique using the velocity initialization

속도오차 초기화를 이용한 관성항법장치 교정기법의 구현

In this paper a linear Kalman filter for calibration of gimballed inertial navigation system(GINS) is designed and its performace is analyzed through the simulation with a real navigation data. Simulation results show that the proposed Kalman filter gives a good performance to calibrate the sensor errors.