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
相关论文
共 50 条
  • [31] Precise Point Positioning with the BeiDou Navigation Satellite System
    Li, Min
    Qu, Lizhong
    Zhao, Qile
    Guo, Jing
    Su, Xing
    Li, Xiaotao
    SENSORS, 2014, 14 (01) : 927 - 943
  • [32] Performance Analysis of Beidou-2/Beidou-3e Combined Solution with Emphasis on Precise Orbit Determination and Precise Point Positioning
    Xu, Xiaolong
    Li, Min
    Li, Wenwen
    Liu, Jingnan
    SENSORS, 2018, 18 (01)
  • [33] Research on the Enhancement of BDS-3 Constellation Orbit Determination and ERP by Inter-satellite Link
    Zhao, Xinglong
    Liu, Jinhuo
    Zhou, Shanshi
    Li, Xiaojie
    Chen, Qiuli
    Zhang, Gong
    Wang, Haihong
    CHINA SATELLITE NAVIGATION CONFERENCE PROCEEDINGS, CSNC 2022, VOL III, 2022, 910 : 334 - 342
  • [34] Precise orbit determination for BeiDou-3 satellite with solar panel non-nominal orientation operations using telemetry information
    Xia, Fengyu
    Zhou, Shanshi
    Lin, Xia
    Hu, Xiaogong
    Liu, Xiao
    Jiang, Nana
    You, Yunzhi
    GPS SOLUTIONS, 2024, 28 (04)
  • [35] Orbit determination of a cislunar space probe using Inter-Satellite Link data
    Huang, Yong
    Yang, Peng
    Chen, Yanling
    Li, Peijia
    Zhou, Shanshi
    Tang, Chengpan
    Hu, Xiaogon
    SCIENTIA SINICA-PHYSICA MECHANICA & ASTRONOMICA, 2023, 53 (02)
  • [36] Early analysis of precise orbit and clock offset determination for the satellites of the global BeiDou-3 system
    Yan, Xingyuan
    Huang, Guanwen
    Zhang, Qin
    Liu, Chenchen
    Wang, Le
    Qin, Zhiwei
    ADVANCES IN SPACE RESEARCH, 2019, 63 (03) : 1270 - 1279
  • [37] Initial Results of the Precise Orbit Determination for the New-Generation BeiDou Satellites (BeiDou-3) Based on the iGMAS Network
    Tan, Bingfeng
    Yuan, Yunbin
    Wen, Mingyue
    Ning, Yafei
    Liu, Xifeng
    ISPRS INTERNATIONAL JOURNAL OF GEO-INFORMATION, 2016, 5 (11)
  • [38] Inter-frequency code bias handling and estimation for multi-frequency BeiDou-3/Galileo uncombined precise point positioning
    Cao, Xinyun
    Shen, Fei
    Ge, Yulong
    Liu, Chao
    Zhang, Shoujian
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2022, 33 (01)
  • [39] Research on satellite positioning technology based on BeiDou-3 navigation satellite system
    Zhao, Pengfei
    Chen, Gaofeng
    Li, Xiaojuan
    Wang, Dabao
    Liu, Ning
    Wang, Huicong
    CHINESE SPACE SCIENCE AND TECHNOLOGY, 2022, 42 (02) : 64 - 70
  • [40] Comparing satellite orbit determination by batch processing and extended Kalman filtering using inter-satellite link measurements of the next-generation BeiDou satellites
    Ren, Xia
    Yang, Yuanxi
    Zhu, Jun
    Xu, Tianhe
    GPS SOLUTIONS, 2019, 23 (01)