GPS carrier signal parameters estimation under ionosphere scintillation

  • Xiaolei Mao*
  • , Yu T. Morton
  • , Lei Zhang
  • , Yanhong Kou
  • *Corresponding author for this work

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

Abstract

This paper presents a post-processing carrier tracking algorithm to track GPS carrier phases under scintillation conditions. The method utilizes GPS signal frequency estimation generated by a frequency lock loop and subsequent frequency correction and interpolation procedures to aid a carrier phase lock loop. The frequency estimation provides information on the signal dynamics. By removing the known dynamics from the input signal, the carrier phase lock loop can track the reduced dynamics signal with a smaller bandwidth to limit noise contributions. Simulated scintillation signals based on models and toolkit provided by Cornell University GPS Laboratory are used to evaluate the dynamic reduction-based PLL (DRP), a conventional PLL, and frequency-assisted PLL (FAP). The results show that the DRP method outperforms the conventional PLL and FAP in carrier phase error under all scintillation levels tested and is comparable or slight superior to the PLL and FAP in number of cycle slips for most test cases.

Original languageEnglish
Title of host publication23rd International Technical Meeting of the Satellite Division of the Institute of Navigation 2010, ION GNSS 2010
Pages3277-3283
Number of pages7
StatePublished - 2010
Event23rd International Technical Meeting of the Satellite Division of the Institute of Navigation 2010, ION GNSS 2010 - Portland, OR, United States
Duration: 21 Sep 201024 Sep 2010

Publication series

Name23rd International Technical Meeting of the Satellite Division of the Institute of Navigation 2010, ION GNSS 2010
Volume4

Conference

Conference23rd International Technical Meeting of the Satellite Division of the Institute of Navigation 2010, ION GNSS 2010
Country/TerritoryUnited States
CityPortland, OR
Period21/09/1024/09/10

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