DocumentCode
1722763
Title
An optimization method for self-calibration method of dual-axis rotational inertial navigation system
Author
Liu Tong ; Ren Qian ; Wang Bo ; Xiao Xuan ; Fu Meng-Yin
Author_Institution
Sch. of Autom., Beijing Inst. of Technol., Beijing, China
fYear
2013
Firstpage
5198
Lastpage
5203
Abstract
According to the error model of strapdown inertial navigation system, an eight-location system-level self-calibration method is designed with special feature that the annular shelf of dual-axis Ins is rotatable. The analytical method of eight-location layout scheme is provided, and the optimal location layout method is found among all the schemes that are satisfying the observability condition with D-optimal principle. The system velocity error of each location is estimated with Kalman filter and the calibration result of parameter error is obtained. Simulation results show that this method is reduced 20% of the calibration time with no loss of accuracy, compared to the traditional method.
Keywords
Kalman filters; calibration; inertial navigation; inertial systems; optimisation; D-optimal principle; Kalman filter; dual-axis rotational inertial navigation system; eight-location system-level self-calibration method; error model; optimization method; parameter error; strapdown inertial navigation system; system velocity error; Automation; Calibration; Electronic mail; Inertial navigation; Kalman filters; Layout; Optimization methods; Kalman filter; inertial navigation system; rotation modulation; self-calibration;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2013 32nd Chinese
Conference_Location
Xi´an
Type
conf
Filename
6640343
Link To Document