Improve satellite radio navigation system performances using linear kalman filtering

C. Hajiyev*

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

A recursive Kalman filter which estimates the user coordinates has been designed, when satellite radio navigation system is used. This filter also makes finding the distance measuring errors, resulted from the time differences between user and satellite (clock bias), possible. Results of performed simulation revealed that the designed filter has worked with high accuracy and has considered both user coordinates and clock bias in real time.

Original languageEnglish
Title of host publicationRAST 2003 - Proceedings of International Conference on Recent Advances in Space Technologies
EditorsS. Kurnaz, Fuat Ince, S. Onbasioglu
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages547-552
Number of pages6
ISBN (Electronic)0780381424, 9780780381421
DOIs
Publication statusPublished - 2003
EventInternational Conference on Recent Advances in Space Technologies, RAST 2003 - Istanbul, Turkey
Duration: 20 Nov 200322 Nov 2003

Publication series

NameRAST 2003 - Proceedings of International Conference on Recent Advances in Space Technologies

Conference

ConferenceInternational Conference on Recent Advances in Space Technologies, RAST 2003
Country/TerritoryTurkey
CityIstanbul
Period20/11/0322/11/03

Bibliographical note

Publisher Copyright:
© 2003 IEEE.

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