Abstract

For Global Positioning System (GPS) precise orbit determination (POD), the solar radiation pressure (SRP) is the dominant nongravitational perturbation force. Among the current SRP models, the ECOM and box-wing models are widely used in the International GNSS Service (IGS) community. However, the performance of different models varies over different GPS satellites. In this study, we investigate the performances of different SRP models, including the box-wing and adjustable box-wing as a priori models, and ECOM1 and ECOM2 as parameterization models, in the GPS POD solution from 2017 to 2019. Moreover, we pay special attention to the handling of the shadow factor in the SRP modeling for eclipsing satellites, which is critical to achieve high-precision POD solutions but has not yet been fully investigated. We demonstrate that, as an a priori SRP model, the adjustable box-wing has better performance than the box-wing model by up to 5 mm in the orbit day boundary discontinuity (DBD) statistics, with the largest improvement observed on the BLOCK IIR satellites using the ECOM1 as a parameterization SRP model. The box-wing model shows an insignificant orbit improvement serving as the a priori SRP model. For the eclipsing satellites, the three-dimensional (3D) root mean square (RMS) values of orbit DBD are improved when the shadow factor is applied only in the D direction (pointing toward to Sun) than that in the three directions (D, Y, and B) in the satellite frame. Different SRP models have comparable performance in terms of the Earth rotation parameter (ERP) agreement with the IERS EOP 14C04 product, whereas the magnitude of the length of day (LoD) annual signal is reduced when the shadow factor is applied in the D direction than in the three directions. This study clarifies how the shadow factor should be applied in the GPS POD solution and demonstrates that the a priori adjustable box-wing model combined with ECOM1 is more suitable for high-precision GPS POD solutions, which is useful for the further GNSS data analysis.

Highlights

  • This study clarifies how the shadow factor should be applied in the Global Positioning System (GPS) precise orbit determination (POD) solution and demonstrates that the a priori adjustable box-wing model combined with ECOM1 is more suitable for high-precision GPS POD solutions, which is useful for the further GNSS data analysis

  • We investigated the performance of different solar radiation pressure (SRP) models, including the box-wing and adjustable box-wing as the a priori model, and the ECOM1 and ECOM2 as the parameterization model in GPS POD solutions

  • For the GPS BLOCK IIR satellite, the performance of the SRP coefficient Y0 between in and out of eclipse seasons is consistent with the shadow factor that is applied in the

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Summary

Introduction

The Global Positioning System (GPS) serves as a critical role in the positioning, navigation, and timing (PNT) services and is a powerful tool in monitoring and understanding the geophysical processes of the Earth system [1,2], crust movement [3,4], and meteorological studies [5,6]. The International GNSS Service (IGS) community has been making continuous efforts in understanding the errors and further improving satellite orbit dynamic modeling. The GPS orbit products from IGS and other analysis lefts (ACs) have a one-dimensional (1D) mean error of around 1 cm in terms of inter-AC agreement [7]. 2.5 cm root mean square (RMS) in terms of the satellite laser ranging (SLR) validation [http://www.igs.org (accessed on 9 January 2021)].

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