Orbit and clock analysis of Compass GEO and IGSO satellites

被引:185
|
作者
Steigenberger, P. [1 ]
Hugentobler, U. [1 ]
Hauschild, A. [2 ]
Montenbruck, O. [2 ]
机构
[1] Tech Univ Munich, Inst Astron & Phys Geodasie, D-80290 Munich, Germany
[2] Deutsch Zentrum Luft & Raumfahrt, German Space Operat Ctr, D-82230 Wessling, Germany
关键词
GNSS; BeiDou-2; Satellite orbits; Allan deviation; GPS;
D O I
10.1007/s00190-013-0625-4
中图分类号
P3 [地球物理学]; P59 [地球化学];
学科分类号
0708 ; 070902 ;
摘要
China is currently focussing on the establishment of its own global navigation satellite system called Compass or BeiDou. At present, the Compass constellation provides four usable satellites in geostationary Earth orbit (GEO) and five satellites in inclined geosynchronous orbit (IGSO). Based on a network of six Compass-capable receivers, orbit and clock parameters of these satellites were determined. The orbit consistency is on the 1-2 dm level for the IGSO satellites and on the several decimeter level for the GEO satellites. These values could be confirmed by an independent validation with satellite laser ranging. All Compass clocks show a similar performance but have a slightly lower stability compared to Galileo and the latest generation of GPS satellites. A Compass-only precise point positioning based on the products derived from the six-receiver network provides an accuracy of several centimeters compared to the GPS-only results.
引用
收藏
页码:515 / 525
页数:11
相关论文
共 50 条
  • [1] Orbit and clock analysis of Compass GEO and IGSO satellites
    P. Steigenberger
    U. Hugentobler
    A. Hauschild
    O. Montenbruck
    Journal of Geodesy, 2013, 87 : 515 - 525
  • [2] Precise Orbit Determination for COMPASS IGSO Satellites During Yaw Maneuvers
    Guo, Jing
    Zhao, Qile
    Geng, Tao
    Su, Xing
    Liu, Jingnan
    CHINA SATELLITE NAVIGATION CONFERENCE (CSNC) 2013 PROCEEDINGS: PRECISE ORBIT DETERMINATION & POSITIONING, ATOMIC CLOCK TECHNIQUE & TIME-FREQUENCY SYSTEM, INTEGRATED NAVIGATION & NEW METHODS, 2013, 245 : 41 - 53
  • [3] Analysis on navigation accuracy of high orbit spacecraft based on BDS GEO and IGSO satellites
    Ma, Xiangtai
    Dong, Xurong
    Hu, Yanfeng
    ADVANCES IN SPACE RESEARCH, 2023, 71 (05) : 2481 - 2492
  • [4] Precise relative positioning using real tracking data from COMPASS GEO and IGSO satellites
    Shi, Chuang
    Zhao, Qile
    Hu, Zhigang
    Liu, Jingnan
    GPS SOLUTIONS, 2013, 17 (01) : 103 - 119
  • [5] An orbit maneuver detection method based on orbital elements for BeiDou GEO and IGSO satellites
    Fan, Lihong
    Tu, Rui
    Zhang, Rui
    Han, Junqiang
    Zhang, Pengfei
    Wang, Siyao
    Hong, Ju
    Lu, Xiaochun
    ADVANCES IN SPACE RESEARCH, 2022, 69 (10) : 3644 - 3654
  • [6] Combined Autonomous Orbit Determination of GEO/IGSO Satellites on the Space-Based Probe
    Liu, Peng
    Hou, Xi-Yun
    CHINA SATELLITE NAVIGATION CONFERENCE (CSNC) 2014 PROCEEDINGS, VOL III, 2014, 305 : 241 - 250
  • [7] Precise relative positioning using real tracking data from COMPASS GEO and IGSO satellites
    Chuang Shi
    Qile Zhao
    Zhigang Hu
    Jingnan Liu
    GPS Solutions, 2013, 17 : 103 - 119
  • [8] Precise Orbit Determination for BeiDou GEO/IGSO Satellites during Orbit Maneuvering with Pseudo-Stochastic Pulses
    Qin, Zhiwei
    Huang, Guanwen
    Zhang, Qin
    Wang, Le
    Yan, Xingyuan
    Xie, Shichao
    Cao, Yu
    Wang, Xiaolei
    REMOTE SENSING, 2019, 11 (21)
  • [9] GEO and IGSO joint precise orbit determination
    Yue Mao
    Yu Du
    XiaoYong Song
    XiaoLin Jia
    XianBing Wu
    Science China Physics, Mechanics and Astronomy, 2011, 54 : 1009 - 1013
  • [10] GEO and IGSO joint precise orbit determination
    MAO Yue 1
    2 China Aerospace Science and Technology Corporation
    ScienceChina(Physics,Mechanics&Astronomy), 2011, (06) : 1009 - 1013