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