基于虚拟测距的单星光学监测空间目标定轨方法

王秀红; 李俊峰; 高彦平; 高景丽; 安芳红

doi:10.3788/OPE.20162407.1541

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基于虚拟测距的单星光学监测空间目标定轨方法

现代应用光学 | 更新时间：2020-08-13

- 基于虚拟测距的单星光学监测空间目标定轨方法
- Orbit determination of space objects with single satellite optical observations and virtual range
- 光学精密工程 2016年24卷第7期页码：1541-1549
- 作者机构：
  
  1.清华大学航天航空学院, 北京 100084
  2.宇航动力学国家重点实验室, 陕西西安 710043
  3.63751部队, 陕西西安 710043
- 作者简介：
  
  [ "王秀红(1971-), 女, 陕西千阳县人, 博士, 研究员, 主要研究方向为航天器轨道确定及空间目标碰撞预警。E-mail:wangxiuhong1971@163.com" ]
  李俊峰(1964-), 男, 黑龙江人, 博士, 教授, 博士生导师, 1993年于莫斯科大学力学数学系获得博士学位, 主要研究方向为航天动力学与控制。E-mail:lijunf@mail.tsinghua.edu.cn E-mail:lijunf@mail.tsinghua.edu.cn
- 基金信息：
  
  国家自然科学基金资助项目(2015AA8083068)
- DOI：10.3788/OPE.20162407.1541
  中图分类号： V529
- 收稿日期：2016-01-21，
  
  录用日期：2016-3-22，
  
  纸质出版日期：2016-07
- 稿件说明：
移动端阅览
王秀红, 李俊峰, 高彦平, 等. 基于虚拟测距的单星光学监测空间目标定轨方法[J]. 光学精密工程, 2016,24(7):1541-1549.

Xiu-hong WANG, Jun-feng LI, Yan-ping GAO, et al. Orbit determination of space objects with single satellite optical observations and virtual range[J]. Optics and precision engineering, 2016, 24(7): 1541-1549.
王秀红, 李俊峰, 高彦平, 等. 基于虚拟测距的单星光学监测空间目标定轨方法[J]. 光学精密工程, 2016,24(7):1541-1549. DOI： 10.3788/OPE.20162407.1541.

Xiu-hong WANG, Jun-feng LI, Yan-ping GAO, et al. Orbit determination of space objects with single satellite optical observations and virtual range[J]. Optics and precision engineering, 2016, 24(7): 1541-1549. DOI： 10.3788/OPE.20162407.1541.

摘要

基于单颗天基卫星的光学监测数据在轨道改进时的可观测性差，迭代难以收敛，甚至法方程病态，造成大批量空间目标编目定轨失败。本文分析了仅利用单星光学监测确定空间目标轨道的特点和难点，针对基于天基监测的定轨亏秩问题和单星光学监测定轨的可观测度进行了研究。基于先验轨道信息建立了虚拟测距模型，提出了一种利用虚拟测距和天基测角数据联合的轨道改进方法，提高了利用单颗天基卫星的光学监测数据定轨系统的可观测性。采用我国首颗天基监测试验卫星2015年某40天内监测到的400多个目标的实测数据进行验证，添加虚拟测距后，定轨成功率由原来小于10%提高到90%以上，同时提高了轨道确定精度。

Abstract

Observability of optical monitoring data based on single space-based satellite is poor when the orbit is improved

iteration cannot be converged and even normal equation would be ill-conditioned

which would cause failure of cataloging and orbit determination of a large number of space targets. Features and difficulties of application of single-satellite optical monitoring to determine the orbit of space target were analyzed. Then the rank deficiency of orbit determination based on space-based monitoring and the observability of orbit determination of single-satellite optical monitoring were studied. On the basis of priori orbit information

a virtual ranging model was established. An orbit improvement method that combined virtual ranging and space-based angle measurement data was put forward

which improves the observability of optical monitoring data orbit determination system based on single space-based satellite. The verification was implemented on the basis of measured data of more than 400 targets monitored in 40 days in 2015 by the first space-based monitoring test satellite of China. After virtual ranging was added

success rate of orbit determination is increased from less than 10% to 90% above and the precision of orbit determination is improved as well.

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Keywords

references

PHILLIP A. Satellite box score[J]. Orbital Debris Quarterly News, 2015, 19(1):10.

LIOU J C. USA space debris environment, operations, and measurement updates[C]. 52nd Session of the Scientific and Technical Subcommittee Committee on the Peaceful Uses of Outer Space, United Nations:AIA, 2015. http://cn.bing.com/academic/profile?id=1586654578&encoded=0&v=paper_preview&mkt=zh-cn

SLANN P A. Space debris and the need for space traffic control[J]. Space Policy, 2014, 30:40-42.

ANDERSON P V, SCHAUB H. Local debris congestion in the geosynchronous environment with population augmentation[J].Acta Astronautica, 2014, 94(2):619-628.

JOSEPH A H, GREGORY P F. Space fence system overview[C]. Proceedings of the Advanced Maui Optical and Space Surveillance Technologies Conference, Maui, HI, 2015.

乔凯, 王治乐, 从明熠.空间目标天基与地基监视系统对比分析[J].光学技术, 2006, 32(5):744-749.

QIAO K, WANG ZH L, CONG M Y.Analysis on space based and ground based surveillance system to space target[J].Opt.Tech., 2006, 32(5):744-749.(in Chinese)

黄建余, 惠建江, 孙前贵, 等.地球同步带空间碎片天基观测初步效果分析[C].第八届全国空间碎片学术交流会, 北京, 2015:107-113.

HUANG J Y, HUI J J, SUN Q G, et al..Primary effect evaluation of space-based observation for geosynchronous debris[C].The Eighth Session of the National Space Debris Conference, Beijing, 2015:107-113.(in Chinese)

ANDREA M, FEDERICO G G, DE' MICHIELI V M, et al..Orbit determination with very short arcs.I.Admissible regions[J].Celestial Mechanics and Dynamical Astronomy, 2004, 90(12):59-87.

DAVID V, VLADIMIR A.Orbit determination results from optical measurements[C]. AIAA/AAS Astrodynamics Specialist Conference, Toronto:AIAA, 2010.

陈务深, 庆波, 常静, 等.利用天基测角资料进行定轨的方法初探[J].天文学报, 2008, 49(1):81-92.

CHEN W SH, QING B, CHANG J, et al..An orbit determination method angle measured using space-based data[J]. Acta Astronomica Sinica, 2008, 49(1):81-92.(in Chinese)

FRVH C, SCHILDKNECHT T. Orbit propagation and validation with angle-only observations[C]. AIAA/AAS Astrodynamics Specialist Conference, Toronto:AIAA, 2010.

潘晓刚, 周海银, 王炯琦.基于天基测控的同步卫星联合定轨方法研究[J].宇航学报, 2009, 30(5):1854-1859.

PAN X G, ZHOU H Y, WANG J Q.Research on the method of combine GEO satellite determination based on space-based tracking telemetry and command technology[J].Journal of Astronautics, 2009, 30(5):1854-1859.(in Chinese)

赵德勇, 潘晓刚, 王炯琦, 等.基于双星定位系统的近地卫星定轨精度仿真研究[J].系统仿真学报, 2006, 18(6):1437-1441.

ZHAO D Y, PAN X G, WANG J Q, et al.. Research on LEO orbit detemination precision simulation based on Bi-satellite positioning system[J].Journal of System Simlulation, 2006, 18(6):1437-1441.(in Chinese)

王秀红, 李俊峰, 王彦荣.天基照相机监测空间目标定轨方法及精度分析[J].光学精密工程, 2013, 21(6):1394-1403.

WANG X H, LI J F, WANG Y R.Orbit determination method and precision analysis of space object with space-based camera[J]. Opt. Precision Eng., 2013, 21(6):1394-1403.(in Chinese)

李冬, 易东云, 程洪玮.天基光学监视的GEO空问目标短弧段定轨方法[J].中国空间科学技术, 2011, 6(3):1-7.

LI D, YI D Y, CHEN H W. Orbit determination for GEO objects with short arcs of space-based optical observations[J].Chinese Space Science and Technology, 2011, 6(3):1-7.(in Chinese)

郭福成, 孙仲康, 安玮.利用方向角及其变化率对固定辐射源的三维单站无源定位[J].电子学报, 2002, 30(12):1885-1887.

GUO F CH, SUN ZH K, AN W. Single observer passive location of 3-D fixed emitter using direction and its rate of changing information[J].Acta Electronica Sinica, 2002, 30(12):1885-1887.(in Chinese)

周亚强, 曹延伟, 冯道旺, 等.基于视在加速度与角速度信息的单站无源定位原理与目标跟踪算法研究[J].电子学报, 2005, 33(12):2120-2124.

ZHOU Y Q, CAO Y W, FENG D W, et al.. Single observer passive location and tracking arithmetic using look acceleration and angle rate of changing information[J].Acta Electronica Sinica, 2005, 33(12):2120-2124.(in Chinese)

刘林, 王海红, 胡松杰.卫星定轨综述[J].飞行器测控学报, 2005, 24(2):28-33.

LIU L, WANG H H, HU S J. Summary on satellite orbit determination[J]. Journal of Spacecraft TT & C Technology, 2005, 24(2):28-33.(in Chinese)

赵德勇, 潘晓刚, 周海银, 等.基于联合定轨策略的星间相对测量自主定轨亏秩问题的改进[J].宇航学报, 2006, 27(2):181-186.

ZHAO D Y, PAN X G, ZHOU H Y, et al.. Improvement of satellite-to-satellite relative measurement autonomous orbit determination deficient-rank based on combined orbit determination strategy[J].Journal of Astronautic, 2006, 27(2):181-186.(in Chinese)

赵博, 周庆勇, 张旺, 等.基于天地基测控的空间目标联合定轨研究[J].光电工程, 2011, 38(11):57-62.

ZHAO B, ZHOU Q Y, ZHANG W, et al.. Combined space objects' orbit determination based on space/ground-based tracking telemetry and command technology[J].Opto-Electronic Engineering, 2011, 38(11):57-62.(in Chinese)

吴功友, 王家松, 赵长印, 等.天地基联合多星定轨及精度分析[J].中国空间科学技术, 2007, 27(3):58-63.

WU G Y, WANG J S, ZHAO CH Y, et al.. Multiple satellite joint orbit determination based on satellite-to-satellite and satellite to earth tracking[J]. Chinese Space and Technology, 2007, 27(3):58-63.(in Chinese)

GAPOSCHKIN E M, YON B C, SHARMA J.Space-based space surveillance with the spaced-based visible[J].Journal of Guidanee, Control and Dynamics, 2000, 23(1):148-152.

李强.单星对卫星目标的被动定轨与跟踪关键技术研究[D].长沙:国防科技大学电子科学与工程学院, 2007:14-64. http://cdmd.cnki.com.cn/article/cdmd-90002-2008098525.htm

LI Q.Research on Key Technologies of Single Satellite to Satellite Target Passive Orbit Determination and Tracking[D].Changsha:Graduate School of National University of Defense Technology, 2007:14-64.(in Chinese)

吴京, 王博, 李骏, 等.空间目标天基光学跟踪可观测性分析[J].湖南大学学报:自然科学版, 2009, 36(11):32-37.

WU J, WANG B, LI J, et al.. Observability analysis on space object tracking in space-based optical surveillance[J].Journal of Hunan University:Natural Sciences, 2009, 36(11):32-37.(in Chinese)

石章松, 刘忠.单站纯方位目标跟踪系统可观测性分析[J].火力与指挥控制制, 2007, 32(2):26-29.

SHI ZH S, LIU ZH.The analysis of the observability on the single platform bearings-only target tracking system[J].Fire Control and Command Control, 2007, 32(2):26-29.(in Chinese)

刘光明.基于天基测角信息的空间非合作目标跟踪算法及相关技术研究[D].长沙:国防科技大学电子科学与工程学院, 2011:30-72.

LIU G M.Research on Non-cooperative Target Tracking Algorithms and Related Technologies Using Space-based Bearings-only Measurements[D].Changsha:Graduate School of National University of Defense Technology, 2011:30-72.(in Chinese)

PORFILIO M, PIERGENTILI F, GRAZIANI F.Two-site orbit determination:The 2003 GEO observation campaign from Collepardo and Mallorca[J].Advances in Space Research, 2006, 38(9):2084-2092.

李济生.航天器轨道确定[M].北京:国防工业出版社, 2003.

LI J SH. Satellite Precise Orbit Determination[M]. Beijing:National Defence Industry Press, 2003.(in Chinese)

刘林.航天器轨道理论[M].北京:国防工业出版社, 2006:33-188.

LIU L. Orbit Theory of Spacecraft[M]. Beijing:National Defence Industry Press, 2006:33-188.(in Chinese)

胡小工, 黄勇, 廖新浩.状态转移矩阵的差分算法及其应用[J].天文学报, 2000, 41(2):113-122.

HU X G, HUANG Y, LIAO X H. The difference algorithm for state transition matrix and its applications[J].Acta Astronomica Sinica, 2000, 41(2):113-122.(in Chinese)

HOUSE K R. The shot term evolution of orbital debris clouds[J]. The Journal of the Astronautic Sciences, 1992, 40(2):203-213.

陈磊, 韩蕾, 白显宗, 等.空间目标轨道力学与误差分析[M].北京:国防工业出版社, 2010:30-61.

CHEN L, HAN L, BAI X Z, et al.. Orbital Dynamics and Error Analysis of Space Object[M]. Beijing:National Defence Industry Press, 2010:30-61.(in Chinese)

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