TY - GEN
T1 - Near real time precise orbit and clock determination for GLONASS
AU - Weiss, Jan P.
AU - Bar-Sever, Yoaz
AU - Bertiger, Willy
AU - Romans, Larry J.
PY - 2010
Y1 - 2010
N2 - 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.
AB - 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.
UR - https://www.scopus.com/pages/publications/79960009774
M3 - Conference contribution
AN - SCOPUS:79960009774
SN - 9781617827358
T3 - 23rd International Technical Meeting of the Satellite Division of the Institute of Navigation 2010, ION GNSS 2010
SP - 2771
EP - 2777
BT - 23rd International Technical Meeting of the Satellite Division of the Institute of Navigation 2010, ION GNSS 2010
T2 - 23rd International Technical Meeting of the Satellite Division of the Institute of Navigation 2010, ION GNSS 2010
Y2 - 21 September 2010 through 24 September 2010
ER -