DocumentCode :
3394759
Title :
Study on a method of rapid transfer alignment
Author :
Luan Hongzhong ; Mao Yuliang
Author_Institution :
Sch. of Autom., Beijing Inst. of Technol., Beijing, China
fYear :
2011
fDate :
19-22 Aug. 2011
Firstpage :
1423
Lastpage :
1426
Abstract :
For the rapidity and accuracy which airborne INS transfer alignment requires, the paper analyzed different transfer alignment matching method, chose velocity plus attitude matching method, deduced system error model and measurement equation in detail. Finally, the paper designed a new Kalman filter for simulation with a classic trajectory. Simulation shows that, the estimation of the misalignment angles can reach the accuracy requirement in a short time, the design of simulation is accurate, and the velocity plus attitude matching method is efficient.
Keywords :
Kalman filters; inertial navigation; measurement theory; Kalman filter; airborne INS transfer alignment; deduced system error model; measurement equation; misalignment angle estimation; rapid transfer alignment; transfer alignment matching method; velocity plus attitude matching method; Accuracy; Equations; Estimation; Kalman filters; Mathematical model; Navigation; Velocity measurement; Kalman filtering; matching method; transfer alignment;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronic Science, Electric Engineering and Computer (MEC), 2011 International Conference on
Conference_Location :
Jilin
Print_ISBN :
978-1-61284-719-1
Type :
conf
DOI :
10.1109/MEC.2011.6025738
Filename :
6025738
Link To Document :
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