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 :
بازگشت