DocumentCode :
761121
Title :
Direct Kalman filtering approach for GPS/INS integration
Author :
Qi, Honghui ; Moore, John B.
Volume :
38
Issue :
2
fYear :
2002
fDate :
4/1/2002 12:00:00 AM
Firstpage :
687
Lastpage :
693
Abstract :
We present a novel Kalman filtering approach for GPS/INS integration. In the approach, GPS and INS nonlinearities are preprocessed prior to a Kalman filter. The GPS preprocessed data are taken as measurement input, while the INS preprocessed data are taken as additional information for the state prediction of the Kalman filter. The advantage of this approach, over the well-studied (extended) Kalman filtering approaches is that a simple and linear Kalman filter can be implemented to achieve significant computation saving with very competitive performance figures
Keywords :
Global Positioning System; Kalman filters; aircraft navigation; inertial navigation; sensor fusion; GPS/INS integration; computation saving; data fusion; dead reckoning; direct Kalman filtering approach; inertial measurement unit; linear stochastic model; nonlinearities; receiver clock error; state prediction; strapdown navigator; transition matrix; Acceleration; Aircraft navigation; Data preprocessing; Earth; Filtering; Global Positioning System; Kalman filters; Measurement units; Nonlinear equations; Radio navigation;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2002.1008998
Filename :
1008998
Link To Document :
بازگشت