DocumentCode
3612944
Title
Dynamic calibration method for SINS lever-arm effect for HCVs
Author
Zhi Xiong ; Hui Peng ; Jie Wang ; Rong Wang ; Jian-Ye Liu
Author_Institution
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
Volume
51
Issue
4
fYear
2015
Firstpage
2760
Lastpage
2771
Abstract
A dynamic calibration method for the lever-arm effect of the Strap-Down Inertial Navigation System (SINS) on hypersonic cruise vehicles is proposed. The lever-arm length is extended as the state variables of the Kalman filter; the model of the lever-arm effect is built, and observability is analyzed. Simulation results show that the proposed method can effectively calibrate the lever-arm length. The calibration results are utilized to compensate the lever-arm effect, and the accuracy of SINS is improved.
Keywords
Kalman filters; aircraft navigation; calibration; inertial navigation; length measurement; missiles; observability; HCV; Kalman filter; SINS lever-arm effect; compensation; dynamic calibration method; hypersonic cruise vehicle; observability analysis; strapdown inertial navigation system; Accelerometers; Aerodynamics; Antenna measurements; Calibration; Inertial navigation systems; Navigation; Vehicle dynamics;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.2015.140048
Filename
7376215
Link To Document