Abstract

The Global Navigation Satellite System (GNSS) ultra-rapid precise orbits are crucial for global and wide-area real-time high-precision applications. The solar radiation pressure (SRP) model is an important factor in precise orbit determination. The real-time orbit determination is generally less accurate than the post-processed one and may amplify the instability and mismodeling of SRP models. Also, the impact of different SRP models on multi-GNSS real-time predicted orbits demands investigations. We analyzed the impact of the ECOM 1 and ECOM 2 models on multi-GNSS ultra-rapid orbit determination in terms of ambiguity resolution performance, real-time predicted orbit overlap precision, and satellite laser ranging (SLR) validation. The multi-GNSS observed orbital arc and predicted orbital arcs of 1, 3, 6, and 24 h are compared. The simulated real-time experiment shows that for GLONASS and Galileo ultra-rapid orbits, compared to ECOM 1, ECOM 2 increased the ambiguity fixing rate to 89.3% and 83.1%, respectively, and improves the predicted orbit accuracy by 9.2% and 27.7%, respectively. For GPS ultra-rapid orbits, ECOM 2 obtains a similar ambiguity fixing rate as ECOM 1 but slightly better orbit overlap precision. For BDS GEO ultra-rapid orbits, ECOM 2 obtains better overlap precision and SLR residuals, while for BDS IGSO and MEO ultra-rapid orbits, ECOM 1 obtains better orbit overlap precision and SLR residuals.

Highlights

  • The International GNSS (Global Navigation Satellite System) Service (IGS) officially began providing services in 1994

  • For BDS IGSO and MEO ultra-rapid orbits, ECOM 1 obtained a similar fixing rate as ECOM 2, and improved orbit overlap precision and satellite laser ranging (SLR) residuals, which suggests that ECOM 1 better fits BDS IGSO and MEO satellites with bodies of a nearly cube shape

  • Multi-GNSS ultra-rapid orbits are crucial for real-time high-precision GNSS applications, and the solar radiation pressure model is one of the main factors influencing predicted orbit accuracy

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Summary

Introduction

The International GNSS (Global Navigation Satellite System) Service (IGS) officially began providing services in 1994. The GLONASS system is integrated into the IGS daily processing operation to provide precise orbit, atmosphere, earth rotation parameters like those of GPS [1]. To meet the different needs of timeliness, IGS provides the final, rapid, and ultra-rapid orbit products. The real-time precise orbit is a prerequisite for global and wide-area precise positioning of decimeter to centimeter level. For real-time users, IGS has provided the ultra-rapid (IGU) orbits since 2000 [3,4]. The GPS orbital accuracy of the observed part is about 3 cm, and that of prediction (real-time) is about 5 cm. The IGS real-time service (RTS) orbits have a 3D RMS of 5 cm for GPS and 13 cm for GLONASS compared with the IGS final products [5]

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