DocumentCode
1760722
Title
Pseudoranges Error Correction in Partial GPS Outages for a Nonlinear Tightly Coupled Integrated System
Author
Iqbal, Ummer ; Georgy, Jacques ; Abdelfatah, Walid F. ; Korenberg, M.J. ; Noureldin, Aboelmagd
Author_Institution
Trusted Positioning Inc., Calgary, AB, Canada
Volume
14
Issue
3
fYear
2013
fDate
Sept. 2013
Firstpage
1510
Lastpage
1525
Abstract
Integrated navigation systems based on a tightly coupled integration scheme utilize pseudoranges and pseudorange rates from Global Positioning System (GPS) satellites measured by the receiver. The positioning accuracy is highly dependent on the accuracy of the pseudoranges whose residual errors can deteriorate the overall positioning accuracy. The integrated system can be improved by the provision of more accurate pseudoranges through modeling the residual correlated errors. This paper utilizes parallel cascade identification (PCI), which is a nonlinear system identification technique, to model these correlated errors. To address the nonlinear error characteristics in the whole integrated navigation system, a nonlinear filter, i.e., mixture particle filter (M-PF), is employed to perform tightly coupled integration of a 3-D reduced inertial sensor system (RISS) with a GPS. The M-PF can accommodate the PCI models of the pseudorange errors in the measurement model. The results demonstrate the advantages of using M-PF-PCI for correcting the pseudoranges and enhancing the positioning solution as compared with M-PF-only, Kalman filter (KF)-PCI, and KF-only solutions.
Keywords
Global Positioning System; Kalman filters; error correction; nonlinear filters; particle filtering (numerical methods); radio receivers; GPS satellites; KF-PCI; Kalman filter; M-PF; M-PF-PCI; PCI models; global positioning system; integrated navigation systems; mixture particle filter; nonlinear filter; nonlinear system identification technique; nonlinear tightly coupled integrated system; parallel cascade identification; partial GPS outages; pseudoranges error correction; reduced inertial sensor system; residual correlated errors; Global Positioning System (GPS); inertial sensors; land vehicle navigation; parallel cascade identification (PCI); particle filter (PF); pseudoranges error modeling; tightly coupled integration;
fLanguage
English
Journal_Title
Intelligent Transportation Systems, IEEE Transactions on
Publisher
ieee
ISSN
1524-9050
Type
jour
DOI
10.1109/TITS.2013.2264474
Filename
6527938
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