Multi-GNSS Combined Orbit and Clock Solutions at iGMAS

• DOI: 10.3390/s22020457
• Publication Date: 2022-01-10T04:08:26Z
• Authors: Wei Zhou; Hongliang Cai; Guo Chen; Wenhai Jiao; Qianqian He; Yuguo Yang
• Keywords: multi-GNSS; Chemical technology; SLR residual; TP1-1185; iGMAS; multi-GNSS; orbit combination; clock combination; SLR residual; precise point positioning; 01 natural sciences; clock combination; Article; iGMAS; orbit combination; precise point positioning; 0105 earth and related environmental sciences

Global navigation services from the quad-constellation of GPS, GLONASS, BDS, and Galileo are now available. The international GNSS monitoring and assessment system (iGMAS) aims to evaluate the navigation performance of the current quad systems under a unified framework. In order to assess impact of orbit and clock errors on the positioning accuracy, the user range error (URE) is always taken as a metric by comparison with the precise products. Compared with the solutions from a single analysis center, the combined solutions derived from multiple analysis centers are characterized with robustness and reliability and preferred to be used as references to assess the performance of broadcast ephemerides. In this paper, the combination method of iGMAS orbit and clock products is described, and the performance of the combined solutions is evaluated by various means. There are different internal precisions of the combined orbit and clock for different constellations, which indicates that consistent weights should be assigned for individual constellations and analysis centers included in the combination. For BDS-3, Galileo, and GLONASS combined orbits of iGMAS, the root-mean-square error (RMSE) of 5 cm is achieved by satellite laser ranging (SLR) observations. Meanwhile, the SLR residuals are characterized with a linear pattern with respect to the position of the sun, which indicates that the solar radiation pressure (SRP) model adopted in precise orbit determination needs further improvement. The consistency between combined orbit and clock of quad-constellation is validated by precise point positioning (PPP), and the accuracies of simulated kinematic tests are 1.4, 1.2, and 2.9 cm for east, north, and up components, respectively.