Impact of ECOM Solar Radiation Pressure Models on Multi-GNSS Ultra-Rapid Orbit Determination

被引:6
作者
Liu, Yang [1 ]
Liu, Yanxiong [1 ]
Tian, Ziwen [1 ]
Dai, Xiaolei [2 ]
Qing, Yun [3 ]
Li, Menghao [1 ]
机构
[1] Minist Nat Resources, Inst Oceanog 1, Qingdao 266061, Peoples R China
[2] Wuhan Univ, GNSS Res Ctr, Wuhan 430079, Peoples R China
[3] China Earthquake Adm, Inst Seismol, Key Lab Earthquake Geodesy, Wuhan 430071, Peoples R China
基金
中国博士后科学基金;
关键词
solar radiation pressure; multi-GNSS; ultra-rapid orbit; ambiguity resolution; ECOM; AMBIGUITY RESOLUTION; YAW-ATTITUDE; IGS; PRECISION; QUALITY; SERVICE;
D O I
10.3390/rs11243024
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
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.
引用
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页数:16
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