Title :
Research on initial alignment for large azimuth misalignment angle with Sage_Husa adaptive filtering
Author :
Cheng Zijian ; He Xiaofei ; Jiang Huan ; Li Dehui
Author_Institution :
Beijing Aerosp. Times Opt.-Electron. Technol. Co., Ltd., Beijing, China
Abstract :
The azimuth was often a large angle because navigation accuracy of fiber-optic inertial navigation system is not high, and the filtering equations of initial alignment are non-linear. In order to improve the initial alignment accuracy of nonlinear models, a improved Sage_Husa adaptive Kalman filtering method is put forward , and applied to initial alignment of fiber-optic inertial navigation system. This paper establishes initial alignment nonlinear model of large azimuth misalignment angle, contributes the system noise statistics estimators, and uses improved Sage_Husa adaptive Kalman filtering to simulate for nonlinear error equations. The simulation results show that the improved Sage_Husa adaptive Kalman filtering could deal with nonlinear problems, improve the accuracy of initial alignment. Azimuth misalignment angle error can converge 13.353´, better than 48.539´ of EKF.
Keywords :
adaptive Kalman filters; inertial navigation; noise; optical fibres; statistical analysis; fiber-optic inertial navigation system; filtering equation; improved Sage_Husa adaptive Kalman filtering method; initial alignment accuracy; large azimuth misalignment angle; nonlinear error equation; nonlinear model; nonlinear problem; system noise statistics estimator; Adaptive filters; Azimuth; Equations; Kalman filters; Mathematical model; Noise; Sage_Husa adaptive kalman filter; fiber-optic initial navigation system; initial alignment; nonlinear;
Conference_Titel :
Control and Decision Conference (CCDC), 2013 25th Chinese
Conference_Location :
Guiyang
Print_ISBN :
978-1-4673-5533-9
DOI :
10.1109/CCDC.2013.6561214