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地月平动点导航星座的概要设计与性能分析

孟云鹤 陈琪锋

地月平动点导航星座的概要设计与性能分析

孟云鹤, 陈琪锋
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  • 研究应用地月平动点轨道的深空导航星座的概要设计问题. 首先, 建立三体平动点动力学模型, 给出计算平动点周期轨道族的微分校正算法, 并介绍周期轨道的稳定性因子概念; 然后, 定义有效覆盖概念, 分析实现有效覆盖的平动点导航星座的相关要素, 给出设计步骤; 在此基础上, 分别从轨道选择、空间覆盖率、几何精度衰减因子、导航信号传输、导航精度等角度, 对平动点导航星座进行设计、分析与估算, 以全球定位系统为参照, 通过综合对比分析, 全面论证平动点导航星座的可行性, 并给出技术指标与性能. 研究表明: 采用所设计的地月L3 平动点Vertical轨道的5星星座可为地月空间各种飞行器提供有效覆盖的导航服务, 在不考虑星座卫星等误差因素情况下, 导航精度可优于10 m, 并可随导航卫星数目增加而进一步提高.
    • 基金项目: 国家自然科学基金(批准号: 10702078)和国防科技大学基础科学预研计划(批准号: JC13-01-08)资助的课题.
    [1]

    Zhang S X 1996 GPS Satellite Positioning and Measurement: Theory and Application (Changsha: National University of Defense Technology Press) pp1-5 (in Chinese) [张守信 1996 GPS卫星测量定位理论与应用 (长沙: 国防科技大学出版社) 第1–5页]

    [2]

    Yuan J P, Luo J J, Yue X K, Fang Q 2003 Satellite Navigation System: Principle and Application (Beijing: China Astronautic Publishing House) p40, 193 (in Chinese) [袁建平, 罗建军, 岳晓奎, 方群 2003 卫星导航原理与应用(北京: 中国宇航出版社) 第40, 193页]

    [3]

    Bhasin K, Hayden J L 2004 AIAA International Communications Satellite Systems Conference and Exhibit Monterey, United State, May 9-12, 2004 p1180

    [4]

    Kulkarni T R, Dharne A, Mortari D 2005 Space Exploration Conference: Continuing the Voyage of Discovery Orlando, United State, Jan. 30-Feb. 1, 2005 p382

    [5]

    Lee S, Kim J H, Lee S P 2003 J. Astronanfical Space Sci. 20 4

    [6]

    Xu S J, Xu M 2006 International Astronautical Congress Spain, Oct. 2-6, 2006 IAC-06-A3.4.03

    [7]

    Space Communication Architecture Working Group (SCAWG) 2006 NASA Space Communication and Navigation Architecture Recommendations for 2005-2030 May, 2006 p100

    [8]

    Grebow D, Ozimek M, Howell K, Folta D 2006 AAS 06-179, AAS/AIAA Space Flight Mechanics Conference Tampa, Florida, January 22-26, 2006 p367

    [9]

    Farquhar R W 1970 NASA Technical Report TR R-346,1970 p31

    [10]

    Kathryn H, Todd M, Mark G, Robert P, Leon S, Joseph T AIAA: 26th International Communications Satellite Syetems Conferencee San Diego, CA, June. 10-12, 2008 p5480

    [11]

    Chen Y L, Wu X 2013 Acta Phys. Sin. 62 140501 (in Chinese) [陈云龙, 伍歆 2013 物理学报 62 140501]

    [12]

    Szebehely V 1967 Theory of Orbits: The Res (Academic Press) p159

    [13]

    Poincare H 1993 History of Modern Physics and Astronomy (Vol. 13) (College Park: American Institute of Physics)

    [14]

    Richardson D L 1980 Celest. Mech. 22 3 241

    [15]

    Dichmann D, Doedel E, Paffenroth R 2003 Libration Point Orbits and Applications (Hong Kong: World Scientific Press) p171

    [16]

    Zhang Y D 2012 Ph. D. Dissertation (Changsha: National University of Defense Technology) (in Chinese) [张跃东 2012 博士学位论文 (长沙: 国防科学技术大学)]

    [17]

    Doedel E J, Romanov V, Paffenroth R C, Keller H B, Dichmann D J, et al. 2007 Int. J. Bifurcat. Chaos Appl. Sci. Engineer. 17 8

    [18]

    Meng Y H, Chen K J, Dai J H 2009 39 3 (in Chinese) [孟云鹤, 陈克俊, 戴金海 2009 中国科学E辑: 技术科学 39 3]

    [19]

    Sun H T, Wang C H, Feng J D 2004 Electro-Optic Technol. Appl. 19 3 (in Chinese) [孙洪拓, 王长青, 冯继东 2004 光电技术应用 19 3]

    [20]

    Karunanayake M D, Cannon M E, Lachapelle G 2004 Proceedings of the Institute of Navigation GNSS Conference Long Beach, CA, September 21-24, 2004 p1107

    [21]

    Fan L T 2009 Ph. D. Dissertation (Changsha: National University of Defense Technology) (in Chinese) [范利涛 2009 博士学位论文 (长沙: 国防科学技术大学)]

    [22]

    Yang C, Guo L X, Wu Z S 2010 Chin. Phys. B 19 054101

  • [1]

    Zhang S X 1996 GPS Satellite Positioning and Measurement: Theory and Application (Changsha: National University of Defense Technology Press) pp1-5 (in Chinese) [张守信 1996 GPS卫星测量定位理论与应用 (长沙: 国防科技大学出版社) 第1–5页]

    [2]

    Yuan J P, Luo J J, Yue X K, Fang Q 2003 Satellite Navigation System: Principle and Application (Beijing: China Astronautic Publishing House) p40, 193 (in Chinese) [袁建平, 罗建军, 岳晓奎, 方群 2003 卫星导航原理与应用(北京: 中国宇航出版社) 第40, 193页]

    [3]

    Bhasin K, Hayden J L 2004 AIAA International Communications Satellite Systems Conference and Exhibit Monterey, United State, May 9-12, 2004 p1180

    [4]

    Kulkarni T R, Dharne A, Mortari D 2005 Space Exploration Conference: Continuing the Voyage of Discovery Orlando, United State, Jan. 30-Feb. 1, 2005 p382

    [5]

    Lee S, Kim J H, Lee S P 2003 J. Astronanfical Space Sci. 20 4

    [6]

    Xu S J, Xu M 2006 International Astronautical Congress Spain, Oct. 2-6, 2006 IAC-06-A3.4.03

    [7]

    Space Communication Architecture Working Group (SCAWG) 2006 NASA Space Communication and Navigation Architecture Recommendations for 2005-2030 May, 2006 p100

    [8]

    Grebow D, Ozimek M, Howell K, Folta D 2006 AAS 06-179, AAS/AIAA Space Flight Mechanics Conference Tampa, Florida, January 22-26, 2006 p367

    [9]

    Farquhar R W 1970 NASA Technical Report TR R-346,1970 p31

    [10]

    Kathryn H, Todd M, Mark G, Robert P, Leon S, Joseph T AIAA: 26th International Communications Satellite Syetems Conferencee San Diego, CA, June. 10-12, 2008 p5480

    [11]

    Chen Y L, Wu X 2013 Acta Phys. Sin. 62 140501 (in Chinese) [陈云龙, 伍歆 2013 物理学报 62 140501]

    [12]

    Szebehely V 1967 Theory of Orbits: The Res (Academic Press) p159

    [13]

    Poincare H 1993 History of Modern Physics and Astronomy (Vol. 13) (College Park: American Institute of Physics)

    [14]

    Richardson D L 1980 Celest. Mech. 22 3 241

    [15]

    Dichmann D, Doedel E, Paffenroth R 2003 Libration Point Orbits and Applications (Hong Kong: World Scientific Press) p171

    [16]

    Zhang Y D 2012 Ph. D. Dissertation (Changsha: National University of Defense Technology) (in Chinese) [张跃东 2012 博士学位论文 (长沙: 国防科学技术大学)]

    [17]

    Doedel E J, Romanov V, Paffenroth R C, Keller H B, Dichmann D J, et al. 2007 Int. J. Bifurcat. Chaos Appl. Sci. Engineer. 17 8

    [18]

    Meng Y H, Chen K J, Dai J H 2009 39 3 (in Chinese) [孟云鹤, 陈克俊, 戴金海 2009 中国科学E辑: 技术科学 39 3]

    [19]

    Sun H T, Wang C H, Feng J D 2004 Electro-Optic Technol. Appl. 19 3 (in Chinese) [孙洪拓, 王长青, 冯继东 2004 光电技术应用 19 3]

    [20]

    Karunanayake M D, Cannon M E, Lachapelle G 2004 Proceedings of the Institute of Navigation GNSS Conference Long Beach, CA, September 21-24, 2004 p1107

    [21]

    Fan L T 2009 Ph. D. Dissertation (Changsha: National University of Defense Technology) (in Chinese) [范利涛 2009 博士学位论文 (长沙: 国防科学技术大学)]

    [22]

    Yang C, Guo L X, Wu Z S 2010 Chin. Phys. B 19 054101

  • 引用本文:
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出版历程
  • 收稿日期:  2014-05-26
  • 修回日期:  2014-08-11
  • 刊出日期:  2014-12-05

地月平动点导航星座的概要设计与性能分析

  • 1. 国防科技大学航天科学与工程学院, 长沙 410073
    基金项目: 

    国家自然科学基金(批准号: 10702078)和国防科技大学基础科学预研计划(批准号: JC13-01-08)资助的课题.

摘要: 研究应用地月平动点轨道的深空导航星座的概要设计问题. 首先, 建立三体平动点动力学模型, 给出计算平动点周期轨道族的微分校正算法, 并介绍周期轨道的稳定性因子概念; 然后, 定义有效覆盖概念, 分析实现有效覆盖的平动点导航星座的相关要素, 给出设计步骤; 在此基础上, 分别从轨道选择、空间覆盖率、几何精度衰减因子、导航信号传输、导航精度等角度, 对平动点导航星座进行设计、分析与估算, 以全球定位系统为参照, 通过综合对比分析, 全面论证平动点导航星座的可行性, 并给出技术指标与性能. 研究表明: 采用所设计的地月L3 平动点Vertical轨道的5星星座可为地月空间各种飞行器提供有效覆盖的导航服务, 在不考虑星座卫星等误差因素情况下, 导航精度可优于10 m, 并可随导航卫星数目增加而进一步提高.

English Abstract

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