DocumentCode
1623559
Title
GPS Standard Positioning using Kalman filter
Author
Yamaguchi, Seiji ; Tanaka, Toshiyuki
Author_Institution
Dept. of Appl. Phys. & Physico-Infomatics, Keio Univ., Yokohama
fYear
2006
Firstpage
1351
Lastpage
1354
Abstract
At present GPS is applied to various situations because of its confidence and usefulness. Position calculated by GPS makes some errors caused from many different factors which GPS signals made. The greatest error factor which affects the accuracy and the precision of positioning by GPS is lack of the number of satellites you can see in the sky. To reduce this error factor and to improve the precision and accuracy of GPS positioning many projects are carried out research, such as QZSS, pseudolite system. These systems have potentiality to make the precision of GPS positioning under worse situation that you can see few GPS satellites because they increase the number of satellites which are available to use for position calculating. However, they require much time and expensive device for their infrastructure. We paid attention to GPS calculating method itself. We adapted Kalman filter to GPS positioning calculation. We improved the precision and accuracy of SPS positioning in stand-alone mode under worse situation adapted the Kalman filter parameter
Keywords
Global Positioning System; Kalman filters; GPS signals; GPS standard positioning; Kalman filter; error factor; Cities and towns; Clocks; Costs; Delay; Electronic mail; Global Positioning System; Nonlinear equations; Physics; Satellites; Tellurium; GPS; Kalman filter; SPS; least-squares method; stand-alone mode;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE-ICASE, 2006. International Joint Conference
Conference_Location
Busan
Print_ISBN
89-950038-4-7
Electronic_ISBN
89-950038-5-5
Type
conf
DOI
10.1109/SICE.2006.315572
Filename
4109175
Link To Document