DocumentCode :
1311852
Title :
Characteristics of Kalman Filters for GNSS Signal Tracking Loop
Author :
Won, Jong-Hoon ; Pany, Thomas ; Eissfeller, Bernd
Author_Institution :
Inst. of Space Technol. & Space Applic., Univ. FAF Munich, Neubiberg, Germany
Volume :
48
Issue :
4
fYear :
2012
fDate :
10/1/2012 12:00:00 AM
Firstpage :
3671
Lastpage :
3681
Abstract :
Characteristics of signal tracking Kalman filter (KF) approaches for a Global Navigation Satellite System (GNSS) receiver are presented. In particular the direct-state KF is designed by using a state vector for signal parameters not for signal parameter errors, so as to directly utilize the discriminator output as a measurement residual. This enables the reuse of the existing signal tracking loop structure by simply adjusting the filter coefficients based on a time-varying optimal Kalman gain. The characteristics of the direct-state KF together with the error-state KF are analyzed by comparing their noise bandwidth and open- and closed-loop transfer functions with those of a traditional method. These KF approaches are mathematically equivalent to the traditional method except for the use of time-varying gains. This fact provides an insight how to tune the designed KFs based on their expected performances.
Keywords :
Kalman filters; satellite navigation; tracking filters; transfer functions; GNSS signal tracking loop; Global Navigation Satellite System; closed-loop transfer functions; direct state KF; error state KF; measurement residual; open-loop transfer functions; signal parameter errors; signal tracking Kalman filter; state vector; time varying optimal Kalman gain; Bandwidth; Global Navigation Satellite Systems; Kalman filters; Noise; Phase locked loops; Tracking loops; Transfer functions;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2012.6324756
Filename :
6324756
Link To Document :
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