Near real time precise orbit and clock determination for GLONASS

Jan P. Weiss, Yoaz Bar-Sever, Willy Bertiger, Larry J. Romans

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

Abstract

We present a near real-time precise orbit and clock determination system for the GLONASS constellation. The system utilizes tracking data from a global network of GPS+GLONASS receivers and a hybrid GPS/GLONASS estimation strategy to produce GLONASS spacecraft orbit and clock estimates with a latency of about 1.5 hours. This paper provides a detailed overview of our processing system and estimation strategy, and describes challenges unique to the GLONASS system. We assess orbit and clock solution accuracy via internal and external metrics. The near real-time orbit solutions are shown to be accurate to better than 15 cm (1D) in the RMS sense, while the clock solutions are shown to be accurate at the 30-40 cm level (RMS). We further assess the near real-time products by performing GLONASS-only static and kinematic precise point positioning for 20 globally distributed sites over a period of 4 weeks. The 3D median position estimate accuracy is 4.7 cm and 7.4 cm for the static and kinematic test, respectively.

Original languageEnglish
Title of host publication23rd International Technical Meeting of the Satellite Division of the Institute of Navigation 2010, ION GNSS 2010
Pages2771-2777
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: Sep 21 2010Sep 24 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
Period09/21/1009/24/10

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