GNSS World of China

Volume 43 Issue 4
Aug.  2018
Turn off MathJax
Article Contents
Article Navigation >  GNSS World of China  > 2018  >  43(4): 59-66
WANG Youcun, GUO Jinyun, XIA Yaowei, KONG Qiaoli. Accuracy Analysis of LEO Satellite Orbit Prediction Based on Dynamic Fitting Method[J]. GNSS World of China, 2018, 43(4): 59-66. doi: 10.13442/j.gnss.1008-9268.2018.04.011
Citation: WANG Youcun, GUO Jinyun, XIA Yaowei, KONG Qiaoli. Accuracy Analysis of LEO Satellite Orbit Prediction Based on Dynamic Fitting Method[J]. GNSS World of China, 2018, 43(4): 59-66. doi: 10.13442/j.gnss.1008-9268.2018.04.011
shu

Accuracy Analysis of LEO Satellite Orbit Prediction Based on Dynamic Fitting Method

doi: 10.13442/j.gnss.1008-9268.2018.04.011

  • College of Geodesy and Geomatics,Shandong University of Science and Technology,Qingdao 266590, China

  • Publish Date: 2018-09-21
    Abstract
  • The orbit prediction plays a significant role in the scientific mission of remote sensing satellite. To obtain the longperiod and highprecision orbit prediction, the orbit forecast is performed by a dynamic fitting method. To analyze the effect of orbital height and different fitting arc lengths on the accuracy of orbit forecast, the data of the GRACEA satellite,HYA satellite, Jason2 satellite are used as examples. From the results, it is concluded that the prediction orbit of 3D RMS of 4 h and 8 h arc length of GRACEA satellites,the results are better than 3 m and 10 m respectively; for HY2A and Jason2 the 4 h arc length prediction results are less than 2 dm and 1 dm separately, 24 h arc length prediction results are better than 2.5 m and 2 m respectively.

     

    • FullText(HTML)
  • loading
    • References(25)
  • [1]
    王文彬,刘荣芳.基于经验加速度的低轨卫星轨道预报新方［J］.空间科学学报，2015,35(6):715-720.
    [2]
    柳青松,刘峰,巨涛.基于GPS的低轨卫星简化解析法轨道预报［J］.全球定位系统,2010,35(2):1-4.
    [3]
    冯来平,毛悦,宋小勇,等.低轨卫星与星间链路增强的北斗卫星联合定轨精度分析［J］.测绘学报,2016,45(S2):109-115.
    [4]
    田世伟.从“传统”到“协同:卫星导航增强理论与方法研究［D］.南京:中国人民解放军理工大学,2015.
    [5]
    马开锋,彭碧波,洪樱.基于卫星轨道特征的低轨卫星星历参数拟合法［J］.大地测量与地球动力学,2007,27(1):85-90.
    [6]
    张如伟,刘根友.低轨卫星轨道拟合及预报方法研究［J］.大地测量与地球动力学,2008,28(4):115-120.
    [7]
    张守建,李建成,邢乐林,等.两种IGS精密星历插值方法的比较分析［J］.大地测量与地球动力学,2007,27(2):80-83.
    [8]
    高鹏,乔学军,范城城.HY2 卫星精密轨道拟合与外推的两种方法比较［J］.海洋测绘,2013,33(4):58-61.
    [9]
    钟世明,王亚菲,王海涛,等.基于Collocation 积分法的LEO 卫星轨道预报研究 ［J］.地球物理学进展，2016,31(3):1045-1051.
    [10]
    王亚菲,钟世明,王海涛,等.LEO卫星轨道预报精度分析［J］.测绘学报,2016,45(9):1035-1041.
    [11]
    LOUPIAN E A,MAZUROV A,FLITMAN E V,et al. Satellite monitoring of forest fires in Russia at federal and regional levels［J］.Mitigation and Adaptation Strategies for Global Change,2006,11(1):113-145.
    [12]
    刘林,王彦荣.卫星轨道预报的一种分析方法［J］.天文学报,2005,46(3):307-313.
    [13]
    龚晓颖,蔡诗响,李征航.小步长低阶Collocation方法轨道积分性能研究［J］.宇航学报,2013,34(5):642648.
    [14]
    周建华,杨龙,徐波,等.一种导航卫星中长期轨道预报方法［J］.测绘学报,2011,40(S1):39-45.
    [15]
    SVEHLA D., ROTHACHER M. Kinematic and reducedynamic precise orbit determination of low earth orbiters［J］.Advances in Geosicence,2003（1）:47-56.
    [16]
    PAVLIS N K, HOLMES S A, KENYON S C, et al. The development and evaluation of earth gravitational model (EGM2008)［J］. Journal of Geophysical Research Solid Earth,2013,118(5):2633-2633.
    [17]
    李济生.人造卫星精密轨道确定［M］.北京:解放军出版社,1995.
    [18]
    宋小勇,毛悦,贾小林.BERNESE光压模型参数的统计分析［J］.测绘科学,2009,34(3):25-27.
    [19]
    WATSON C,TREGONING P,COLEMAN R. Impact of solid earth tide models on GPS coordinate and tropospheric time series［J］. Geophysical Research Letters,2006, 33(8):153-172.
    [20]
    CAPITAINE N,WALLACE P T,CHAPRONT J. Expressions for IAU 2000 precession quantities［J］.Astronomy ＆ Astrophysics,2003,412(2):567-586.
    [21]
    ALTAMIMI Z, REBISCHUNG P, METIVIER L, COLLILIEUX X. ITRF2014: A new release of the International Terrestrial Reference Frame modeling nonlinear station motions［J］. Journal of Geophysical Research: Solid Earth,2016,121(8):6109-6131.
    [22]
    LI J C, ZHANG S J, ZOU X C, JIANG W P. Precise orbit determination for GRACE with zerodifference kinematic method. Chinese Science Bulletin,2009,54(16),2355-2362.
    [23]
    ZHAO G, ZHOU X, WU B. Precise orbit determination of Haiyang2 using satellite laser ranging［J］.Chinese Science Bulletin,2013,58(6):589-597.
    [24]
    GUO J Y, QIN J, KONG QL, LI GW. On simulation of precise orbit determination of HY2 with centimeter precision based on satelliteborne GPS technique［J］. Applied Geophysics, 2012, 9(1):95-107.
    [25]
    LAMBIN J, MORROW R, FU L L, et al. The OSTM／Jason2 mission［J］.Marine Geodesy,2010,33(S1):4-25.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views (413) PDF downloads(138) Cited by()
    Proportional views
    Related

    Copyright © 2009《 GNSS World of China 》 Editorial Office

    Address：84 Jianshe Dong Lu, Muye District, Xinxiang City, Henan Province, ChinaChina Pos：453000Tel：0373-3712411Fax：0373-3052232Email：qqdwxt@126.com

    Supported by: Beijing Renhe Information Technology Co. Ltd    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return