Comparison of shadow models and their impact on precise orbit determination of BeiDou satellites during eclipsing phases

被引:1
|
作者
Zhang, Yan [1 ,2 ,4 ]
Wang, Xiaoya [1 ,2 ,3 ]
Xi, Kewei [1 ,2 ]
Li, Zhen [5 ]
机构
[1] Chinese Acad Sci, Shanghai Astron Observ, Astrogeodynam Res Ctr, Shanghai 200030, Peoples R China
[2] Univ Chinese Acad Sci, Beijing 100049, Peoples R China
[3] Shanghai Key Lab Space Nav & Positioning Tech, Shanghai 200030, Peoples R China
[4] Univ Calgary, Dept Geomat Engn, 2500 Univ Dr NW, Calgary, AB T2N 1N4, Canada
[5] Beihang Univ, Res Inst Frontier Sci, Key Lab Satellite Nav & Mobile Commun, Beijing 100191, Peoples R China
来源
EARTH PLANETS AND SPACE | 2022年 / 74卷 / 01期
基金
中国国家自然科学基金;
关键词
Shadow model; Earth's oblateness; Atmospheric effect; SLR; Inter-satellite link; SOLAR-RADIATION PRESSURE; EARTH SATELLITES; INTERSATELLITE LINKS; PERTURBATIONS; MOTION;
D O I
10.1186/s40623-022-01684-5
中图分类号
P [天文学、地球科学];
学科分类号
07 ;
摘要
Solar radiation pressure (SRP) is an extremely critical perturbative force that affects the GNSS satellites' precise orbit determination (POD). Its imperfect modelling is one of the main error sources of POD, whose magnitude is even to10(-9) m/s(2). The shadow factor (i.e., eclipse factor) is one crucial parameter of SRP, generally estimated by the cylindrical model, the conical model, or shadow models considering the Earth's oblateness and the atmospheric effect, such as the Perspective Projection Method atmosphere (PPMatm) model and Solar radiation pressure with Oblateness and Lower Atmospheric Absorption, Refraction, and Scattering Curve Fit (SOLAARS-CF) model. This paper applies the former four shadow models to determine the corresponding precise orbit using BeiDou satellites' ground-based observation, and then compared and assessed the orbit accuracy through Satellite Laser Ranging (SLR) validation and Inter-Satellite Link (ISL) check. The results show that the PPMatm model's accuracy is equivalent to the SOLAARS-CF model. Compared with the conical shadow model, SLR validations show the orbit accuracy from the PPMatm and SOLAARS-CF model can be generally improved by 2-10 mm; ISL range check shows that the Root Mean Square (RMS) can be decreased by 2-7 mm. These results show that the shadow model in GNSS POD should fully consider the Earth's oblateness and the atmospheric effect, especially for the perturbative acceleration higher than 10(-10) m/s(2).
引用
收藏
页数:14
相关论文
共 50 条
  • [41] Beidou satellite maneuver thrust force estimation for precise orbit determination
    Jing Qiao
    Wu Chen
    GPS Solutions, 2018, 22
  • [42] Precise orbit determination of BeiDou constellation based on BETS and MGEX network
    Lou, Yidong
    Liu, Yang
    Shi, Chuang
    Yao, Xiuguang
    Zheng, Fu
    SCIENTIFIC REPORTS, 2014, 4
  • [43] Beidou satellite maneuver thrust force estimation for precise orbit determination
    Qiao, Jing
    Chen, Wu
    GPS SOLUTIONS, 2018, 22 (02)
  • [44] Precise orbit determination of BeiDou constellation based on BETS and MGEX network
    Yidong Lou
    Yang Liu
    Chuang Shi
    Xiuguang Yao
    Fu Zheng
    Scientific Reports, 4
  • [45] Precise orbit determination method for BeiDou mixed constellations with layered constraints
    北斗混合星座分层约束下的精密定轨方法
    Zhu, Jun (zhujun9306@126.com), 1600, SinoMaps Press (50):
  • [46] Centralized Autonomous Orbit Determination of Beidou Satellites Under the Constraint of Anchor Station
    Wen, Xufeng
    Hao, Jinming
    Hu, Xiaogong
    Tang, Chengpan
    Wang, Dongxia
    Xin, Jie
    Jiao, Bo
    Wang, Jing
    CHINA SATELLITE NAVIGATION CONFERENCE (CSNC) 2018 PROCEEDINGS, VOL II, 2018, 498 : 409 - 421
  • [47] Orbit determination and prediction for Beidou GEO satellites at the time of the spring/autumn equinox
    LI XiaoJie
    ZHOU JianHua
    HU XiaoGong
    LIU Li
    GUO Rui
    ZHOU ShanShi
    Science China(Physics,Mechanics & Astronomy), 2015, (08) : 92 - 100
  • [48] Orbit determination and prediction for Beidou GEO satellites at the time of the spring/autumn equinox
    Li XiaoJie
    Zhou JianHua
    Hu XiaoGong
    Liu Li
    Guo Rui
    Zhou ShanShi
    SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 58 (08)
  • [49] Orbit determination and prediction for Beidou GEO satellites at the time of the spring/autumn equinox
    XiaoJie Li
    JianHua Zhou
    XiaoGong Hu
    Li Liu
    Rui Guo
    ShanShi Zhou
    Science China Physics, Mechanics & Astronomy, 2015, 58
  • [50] Precise orbit determination for geostationary satellites with multiple tracking techniques
    GUO Rui 1
    2 Graduate University of Chinese Academy of Sciences
    3 Beijing Global Information Application and Development Center
    Science Bulletin, 2010, (08) : 687 - 692