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基于自适应滤波的编队卫星实时相对定轨

秦显平 任夏 杨元喜

秦显平, 任夏, 杨元喜等 . 基于自适应滤波的编队卫星实时相对定轨[J]. 北京航空航天大学学报, 2014, 40(9): 1195-1199. doi: 10.13700/j.bh.1001-5965.2013.0589
引用本文: 秦显平, 任夏, 杨元喜等 . 基于自适应滤波的编队卫星实时相对定轨[J]. 北京航空航天大学学报, 2014, 40(9): 1195-1199. doi: 10.13700/j.bh.1001-5965.2013.0589
Qin Xianping, Ren Xia, Yang Yuanxet al. Real-time relative orbit determination for formation flying satellites using adaptive filtering[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(9): 1195-1199. doi: 10.13700/j.bh.1001-5965.2013.0589(in Chinese)
Citation: Qin Xianping, Ren Xia, Yang Yuanxet al. Real-time relative orbit determination for formation flying satellites using adaptive filtering[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(9): 1195-1199. doi: 10.13700/j.bh.1001-5965.2013.0589(in Chinese)

基于自适应滤波的编队卫星实时相对定轨

doi: 10.13700/j.bh.1001-5965.2013.0589
基金项目: 国家自然科学基金资助项目(41274040,41020144004,41304024)
详细信息
    作者简介:

    秦显平(1974-),男,河南荥阳人,副研究员,qxianping92@163.com.

  • 中图分类号: V557.1

Real-time relative orbit determination for formation flying satellites using adaptive filtering

  • 摘要: 提出基于自适应滤波的编队卫星实时相对定轨算法,利用2005-12-09—10两颗GRACE(Gravity Recovery and Climate Experiment)卫星的GPS(Global Positioning System)实测数据进行实时相对定轨试验计算,采用JPL(Jet Propulsion Laboratory)轨道对试验结果外部检核,结果表明:①自适应滤波相对定轨通过自适应因子,可以较好地平衡编队卫星的观测信息和相对动力学信息,其相对定轨结果精度优于Kalman滤波相对定轨结果;②自适应滤波相对定轨结果随着星间基线缩短而精度提高;③两颗GRACE卫星采用单频伪距和广播星历进行自适应滤波相对定轨,可以得到精度优于6cm的星间基线。

     

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出版历程
  • 收稿日期:  2013-10-15
  • 网络出版日期:  2014-09-20

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