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Volume 38 Issue 6
Jun.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  38(6): 755-759,765.
Li Taohu, Liu Jiansheng, Qin Honglei, et al. Preliminary orbit determination method of HEO satellite using a single navigation GPS satellite measurements[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(6): 755-759,765. (in Chinese)
Citation: Li Taohu, Liu Jiansheng, Qin Honglei, et al. Preliminary orbit determination method of HEO satellite using a single navigation GPS satellite measurements[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(6): 755-759,765. (in Chinese)
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Preliminary orbit determination method of HEO satellite using a single navigation GPS satellite measurements

  • School of Electronics and Information Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 02 Apr 2011
  • Publish Date: 30 Jun 2012
    Abstract
  • The autonomous navigation of highly elliptical orbit (HEO) satellites using GPS needed to solve a key problem of the preliminary orbit determination under the condition of only one navigation satellite. The feasibility by using the pseudo-range received from a single navigation satellite was demonstrated, and the limitation of the F.G method for preliminary orbit determination was figured out. An iterative batch method using orbit elements as constrains was proposed to determine the preliminary orbit. This algorithm did not have complex mathematic operation and could avoid the influence of ill-conditioned equation with short arc data by using F.G method. The simulation results show that its positioning bias is about 104 m and velocity bias is approximate 100 m/s with an acceptable orbit injection errors, and the proposed method using a single navigation satellite measurements could determine the HEO initial orbit credibly.

     

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    • References(12)
  • [1]
    Balbach O,Eissfeller B,HEIN G W,et al.Tracking GPS above GPS satellite altitude:first results of the GPS experiment on the HEO mission equator-S [C]// Proceedings of the 11th International Technical Meeting of the Satellite Division of the Institute of Navigation (ION GPS 1998).Nashville,TN:[s.n.],1998:1555-1564
    [2]
    Davis G,Moreau M,Bauer F,et al.GPS-based navigation and orbit determination for AMSAT AO-40 satellite [C]//AIAA Guidance,Navigation,and Control Conference and Exhibit.Monterey,California:AIAA,2002:5-8
    [3]
    Long A,Kelbel D,Lee T,et al.Autonomous navigation improvements for high-earth orbiters using GPS[C]//Proceedings of the 15th International Symposium on Spaceceflight Dynamics.Biarritz:CNES,2000
    [4]
    赵春梅,瞿锋.无准确初轨信息时星载GPS低轨卫星定轨方法研究[J].测绘科学,2006,31(3):23-27
    Zhao Chunmei,Qu Feng.Research on methods of low-earth satellites orbit determination based on GPS without accurate preliminary orbit position[J].Science of Surveying and Mapping,2006,31(3):23-27(in Chinese)
    [5]
    刘林,张巍.关于各种类型数据的初轨计算方法[J].飞行器测控学报,2009,28(3):70-76 Liu Lin,Zhang Wei.Initial orbit determination for different data types[J].Journal of Spacecraft TT&C Technology,2009,28(3):70-76(in Chinese)
    [6]
    刘艳芳,巨涛.用两颗GPS卫星确定低轨卫星轨道的初值方法[J].中国空间科学技术,1999,4(2):47-52 Liu Yanfang,Ju Tao.Initial value method of orbit determination using two GPS satellites[J].Chinese Space Science and Technology,1999,4(2):47-52(in Chinese)
    [7]
    刘林.人造地球卫星轨道力学[M].北京:高等教育出版社,1992:49-54 Liu Lin.Orbital dynamics of manned satellite [M].Beijing:Higher Education Press,1992:49-54 (in Chinese)
    [8]
    刘小河.非线性系统分析与控制引论[M].北京:清华大学出版社,2008:235-240 Liu Xiaohe.Analysis and control of nonlinear systems[M].Beijing:Tsinghua University Publishing House,2008:235-240 (in Chinese)
    [9]
    Yim Jo R,Crassidis John L,Junkins John L.Autonomous orbit navigation of interplanetary spacecraft[R].AIAA-2000-3936,2000
    [10]
    Alfriend K T,Dasenbrock R R,Kaufman B,et al.Autonomous interplanetary orbit determination using satellite-to-satellite tracking[J].Journal of Guidance,Control,and Dynamics,2007,30(3):679-686
    [11]
    Lee Deok-Jin,Alfriend Kyle T,OZA D H,et al.Landsat-4 (TDRSS-user) orbit determination using batch least-squaresand sequential methods[C]//AIAA/AAS Astrodynamics Conference.South Carolina:AIAA,1992:10-12
    [12]
    Teixeira B O S,Bernstein D S,Santillo M A,et al.Spacecraft tracking using sampled-data Kalman filters[J].IEEE Control Systems Magazine,2008,28(4):78-94
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