Precise orbit determination of BDS-3 satellites using B1C and B2a dual-frequency measurements

• Published in: GPS solutions 2021-07, Vol.25 (3), Article 95
• Main Authors: Li, Ran, Wang, Ningbo, Li, Zishen, Zhang, Yang, Wang, Zhiyu, Ma, Hongyang
• Format: Article
• Language: English
• Subjects: Atmospheric Sciences; Automotive Engineering; BeiDou Navigation Satellite System; Earth and Environmental Science; Earth orbits; Earth Sciences; Electrical Engineering; Elevation angle; Frequency measurement; Geophysics/Geodesy; Global navigation satellite system; Global positioning systems; GPS; Orbit determination; Orbits; Original Article; Radiation pressure; Satellite constellations; Satellite laser ranging; Satellite navigation systems; Satellite Orbit Determination; Satellites; Solar radiation; Space Exploration and Astronautics; Space Sciences (including Extraterrestrial Physics; Steering; Yaw
• ISSN: 1080-5370; 1521-1886
• DOI: 10.1007/s10291-021-01126-x

Compared to the BeiDou regional navigation satellite system (BDS-2), the BeiDou global navigation satellite system (BDS-3) includes the newly designed B1C and B2a signals, which are compatible with the L1 and L5 frequencies of the global positioning system (GPS). Considering that the precise orbit determination (POD) of the BDS-3 constellation is currently restricted to the legacy B1I and B3I signals, we reported the POD performance of BDS-3 satellites using B1C and B2a dual-frequency measurements. Nine globally distributed Multi-GNSS Experiment (MGEX) stations were selected to determine the orbits of BDS-3 satellites during the period of July 2019. The results show that B1C/B2a-based POD enables an average three-dimensional root-mean-square error (3D RMS) of 24.2 cm, and the precision is better than 6 cm in the radial component in a comparison of two-day overlapping arcs. Satellite laser ranging (SLR) validation achieves an overall precision of 6.8 cm in RMS differences. Compared to the B1I/B3I-based POD results, the quality of B1C/B2a-based orbits is improved by approximately 9% across the whole BDS-3 constellation, indicating that the new B1C/B2a signals can be employed for the superior POD performance of BDS-3 satellites. Moreover, we investigated the behavior of the solar radiation pressure (SRP), which is generally considered one of the primary error sources in BDS-3 medium earth orbit (MEO) dynamic orbit determination. The ECOM7 SRP model has a better POD performance in continuous yaw steering (CYS) mode than the ECOM5 and ECOM9 SRP models. The results also show that there is no degradation in the orbit precision of BDS-3 MEO satellites when the elevation angle of the sun above the orbital plane (β angle) varies within the range of − 4° to + 4°.