留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于虚拟观测值的X射线单脉冲星星光组合导航

杨博 胡声曼 孙晖 徐帆

杨博, 胡声曼, 孙晖, 等 . 基于虚拟观测值的X射线单脉冲星星光组合导航[J]. 北京航空航天大学学报, 2016, 42(6): 1107-1115. doi: 10.13700/j.bh.1001-5965.2015.0422
引用本文: 杨博, 胡声曼, 孙晖, 等 . 基于虚拟观测值的X射线单脉冲星星光组合导航[J]. 北京航空航天大学学报, 2016, 42(6): 1107-1115. doi: 10.13700/j.bh.1001-5965.2015.0422
YANG Bo, HU Shengman, SUN Hui, et al. Integrated single X-ray pulsar and starlight navigation based on virtual observation value[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1107-1115. doi: 10.13700/j.bh.1001-5965.2015.0422(in Chinese)
Citation: YANG Bo, HU Shengman, SUN Hui, et al. Integrated single X-ray pulsar and starlight navigation based on virtual observation value[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1107-1115. doi: 10.13700/j.bh.1001-5965.2015.0422(in Chinese)

基于虚拟观测值的X射线单脉冲星星光组合导航

doi: 10.13700/j.bh.1001-5965.2015.0422
基金项目: 国家自然科学基金(51275027)
详细信息
    作者简介:

    杨博 女,博士,副教授。主要研究方向:航天器自主导航制导、深空探测导航制导和可重复运载器GNC关键技术。Tel.:15901355288 E-mail:yangbo@buaa.edu.cn;胡声曼 女,硕士研究生。主要研究方向:X射线脉冲星自主导航。Tel.:13269830856 E-mail:228737949@qq.com

    通讯作者:

    杨博,Tel.:15901355288 E-mail:yangbo@buaa.edu.cn

  • 中图分类号: P128.4;P145.6;V476.4

Integrated single X-ray pulsar and starlight navigation based on virtual observation value

  • 摘要: 传统的X射线脉冲星导航系统需要同时观测3~4颗脉冲星,有效载荷的质量和功耗极大。因此,单探测器脉冲星导航技术是实现航天器利用X射线脉冲星导航的关键举措。针对单探测器脉冲星导航的可观测性弱和精度低等问题提出了基于虚拟观测值的X射线单脉冲星与星光集中式组合滤波的高精度导航方法,即在X射线脉冲星的长周期内增加与星光同时刻观测的虚拟观测值,以实现高精度的集中式组合滤波算法。同时提出了利用神经网络预测虚拟观测值方法,并与利用动力学递推的方法进行比较,精度可以达到10-7量级。仿真结果表明,该方法可大大提高单探测器的导航的可靠性,补偿由于探测器误差造成的导航误差,导航位置误差为259.79 m,同时有效地减小了导航系统的重量,为X射线脉冲星导航的工程实现提供了参考依据。

     

  • [1] 乔黎.X射线脉冲星高轨道卫星自主导航及其应用技术研究[D].南京:南京航空航天大学,2010:35-47. QIAO L.X-ray pulsar-based autonomous navigation and its application to high earth orbits satellites[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2010:35-47(in Chinese).
    [2] SHEIKH S I,PINES D J,RAY P S,et al.Spacecraft navigation using X-ray pulsars[J].Journal of Guidance,Control,and Dynamics,2006,29(1):50-63.
    [3] 帅平,李明,陈绍龙,等.X射线脉冲星导航系统原理与方法[J].北京:中国宇航出版社,2009:23-27. SHUAI P,LI M,CHEN S L,et al.Principle and method of X-ray pulsars navigation system[J].Beijing:China Astronautic Publishing House,2009:23-27(in Chinese).
    [4] 杨博,张睿,孙晖,等.分时段实时观测脉冲星的单探测器导航方法[J].北京航空航天大学学报,2014,40(9):1183-1188. YANG B,ZHANG R,SUN H,et al.Navigation method using a single detector based on the observation of X-ray pulsar in different time interval[J].Journal of Beijing University of Aeronautics and Astronautics,2014,40(9):1183-1188(in Chinese).
    [5] EMADZADEH A A,SPEYER J L.X射线脉冲星导航[M].侯建文,阳光,贺亮,等,译.北京:国防工业出版社,2013:5-15. EMADZADEH A A,SPEYER J L.X-ray pulsar-based navigation[M].HOU J W,YANG G,HE L,et al,translated.Beijing:National Defence of Industry Press,2013:5-15(in Chinese).
    [6] 杨廷高.X射线脉冲星脉冲到达航天器时间测量[J].空间科学学报,2008,28(4):330-334. YANG T G.Spacecraft X-ray pulsar pulse time measurement[J].Journal of Space Science,2008,28(4):330-334(in Chinese).
    [7] ANDERSON K D,PINES D J.Experimental validation of pulse phase tracking for X-ray pulsar based spacecraft navigation:AIAA-2013-5202[R].Reston:AIAA,2013.
    [8] SHEIKH S I,HELLINGS R W,MATZNER R A.High-order pulsar timing for navigation[C]//Proceedings of the 63rd Annual Meeting of the Institute of Navigation.Fairfax,VA:ION,2007:432-443.
    [9] GOLSHAN A R,SHEIKH S I.On pulse phase estimation and tracking of variable celestial X-ray sources[C]//Proceedings of the 63rd Annual Meeting of the Institute of Navigation.Fairfax,VA:ION,2007:413-422.
    [10] 刘林,胡松杰,王歆.航天动力学引论[M].南京:南京大学出版社,2006:125-156. LIU L,HU S J,WANG X.Introduction of aerospace dynamics[M].Nanjing:Nanjing University Press,2006:125-156(in Chinese).
    [11] SUNEEL I S.The use of variable celestial X-ray sources for spacecraft navigation[D].Maryland:University of Maryland,2005:26-37.
    [12] JASON W M, MUNTHER A H,LUKE M B W,et al.SEXTANT-Station explorer for X-ray timing and navigation technology:AIAA-2015-0865[R].Reston:AIAA,2015.
    [13] 房建成,宁晓琳,田玉龙.航天器自主天文导航原理与方法[M].北京:国防工业出版社,2010:77-80. FANG J C,NING X L,TIAN Y L.Principle and method of the spacecraft autonomous celestial navigation[M].Beijing:National Defence of Industry Press,2010:77-80(in Chinese).
    [14] 刘劲,马杰,田金文.利用X射线脉冲星和多普勒频移的组合导航[J].宇航学报,2010,31(6):1552-1556. LIU J,MA J,TIAN J W.Integrated X-ray and doppler shift navigation[J].Journal of Astronautics,2010,31(6):1552-1556(in Chinese).
    [15] 毛悦,宋小勇,冯来平.X射线脉冲星导航可见性分析[J].武汉大学学报,2009,34(2):222-225. MAO Y,SONG X Y,FENG L P.Visibility analysis of X-ray pulsar navigation[J].Journal of Wuhan University,2009,34(2):222-225(in Chinese).
    [16] 卞鸿巍,李安,覃方军,等.现代信息融合技术在组合导航中的应用[M].北京:国防工业出版社,2010:123-126. BIAN H W,LI A,QIN F J,et al.Modern information fusion technology in the application of the integrated navigation[M].Beijing:National Defence of Industry Press,2010:123-126(in Chinese).
  • 加载中
计量
  • 文章访问数:  843
  • HTML全文浏览量:  86
  • PDF下载量:  483
  • 被引次数: 0
出版历程
  • 收稿日期:  2015-06-24
  • 网络出版日期:  2016-06-20

目录

    /

    返回文章
    返回
    常见问答