Inter-satellite link augmented BeiDou-3 orbit determination for precise point positioning

被引:0
|
作者
Liqian ZHAO [1 ,2 ]
Xiaogong HU [2 ]
Chengpan TANG [2 ]
Shanshi ZHOU [2 ]
Yueling CAO [2 ]
Qianxin WANG [3 ]
Ranran SU [4 ]
机构
[1] Space Star Technology Co., Ltd.
[2] Shanghai Astronomical Observatory, Chinese Academy of Sciences
[3] School of Environment Science and Spatial Informatics, China University of Mining and Technology
[4] Beijing Satellite Navigation Center
基金
中国国家自然科学基金;
关键词
D O I
暂无
中图分类号
V448 [制导与控制];
学科分类号
081105 ;
摘要
Precise Point Positioning(PPP) requires precise products, including high-accuracy satellite orbit and clock parameters. It is impossible to obtain an orbit solution that is sufficiently accurate for PPP services with a regional tracking network; therefore, satellite orbits are usually estimated by a global tracking network with a large number of ground stations. However, it is expensive to build globally distributed stations. Fortunately, BeiDou-3 satellites carry an InterSatellite Link(ISL) payload, which can track the whole arc of the BeiDou-3 satellites and enhance the orbit determination accuracy with regional ground stations. In this contribution, a novel orbit determination strategy for BeiDou-3 PPP is proposed, in which the BeiDou-3 satellite orbits are enhanced by the ISL. First, the generation of precise satellite products is demonstrated in detail.In addition, the products are assessed by Satellite Laser Ranging(SLR) residuals and overlap comparisons. Moreover, the products are used for receivers in mainland China to carry out the static and kinematic modes to research the PPP performance of Bei Dou-3’s 3IGSO/24MEO constellation.The SLR validations of the satellite orbits demonstrate an accuracy better than 0.1 m in the radial component, and the orbit overlap comparisons show accuracies of 0.016 m in the radial component,0.088 m in the along-track component and 0.087 m in the cross-track component. The Standard Deviation(STD) in the differences in overlapping arcs for the estimated satellite clocks is approximately 0.10 ns. The static PPP results demonstrate that the error in both the horizontal and vertical components is smaller than 10 cm after 30 minutes of convergence. After 24 hours of convergence,the errors are 0.70 cm, 0.63 cm and 1.99 cm for the north, east and up components, respectively.The kinematic PPP experiment illustrates that the Root Mean Square(RMS) position errors in the north, east and up components are approximately 3.23 cm, 5.27 cm and 8.64 cm, respectively,after convergence. The obtainable positioning and convergence performances are comparable to those using products generated by global tracking networks.
引用
收藏
页码:332 / 343
页数:12
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