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

行星悬浮轨道附近的编队

龚胜平 李俊峰 宝音贺西

龚胜平, 李俊峰, 宝音贺西. 行星悬浮轨道附近的编队[J]. 应用数学和力学, 2007, 28(6): 675-683.
引用本文: 龚胜平, 李俊峰, 宝音贺西. 行星悬浮轨道附近的编队[J]. 应用数学和力学, 2007, 28(6): 675-683.
GONG Sheng-ping, LI Jun-feng, BAOYIN He-xi. Formation Around Planetary Displaced Orbit[J]. Applied Mathematics and Mechanics, 2007, 28(6): 675-683.
Citation: GONG Sheng-ping, LI Jun-feng, BAOYIN He-xi. Formation Around Planetary Displaced Orbit[J]. Applied Mathematics and Mechanics, 2007, 28(6): 675-683.

行星悬浮轨道附近的编队

基金项目: 国家自然科学基金资助项目(10672084;10602027)
详细信息
    作者简介:

    龚胜平(1981- ),男,湖北人,博士研究生(联系人.Tel:+86-10-62773402;E-mail:gsp04@mails.tsinghua.edu.cn).

  • 中图分类号: V412.4

Formation Around Planetary Displaced Orbit

  • 摘要: 研究了不同类型的地球和火星悬浮轨道附近的相对运动.首先,推导了悬浮轨道附近的相对运动方程并将相对运动方程在悬浮轨道附近线性化.利用两种半自然编队控制率进行编队控制,其中一种为被动控制,对工程应用有很大的价值.在两种控制率下,讨论了每种悬浮轨道的稳定区域.由于两种控制率都不能满足特殊的火星悬浮轨道任务要求,于是,根据该任务的要求设计了一种特殊的半自然控制率.该控制率既能满足编队任务的要求也能使相对运动稳定.
  • [1] West J L. NOAA/DOD/NASA Geostorm Warning Mission[R]. Jet Propulsion Lab, California Institute of Technology, JPL D-13986, Pasadena, CA, Oct,1996.
    [2] Prado J Y,Perret A,Pignolet G,et al.Using a Solar Sail for a Plasma Storm Early Warning System[R]. International Academy of Astronautics, Paper 96-IAA. 3.3.06,Oct,1996.
    [3] McInnes C R.Dynamics stability and control of non-Keplerian orbits[D].Doctoral Thesis for the Degree of Doctor of Science.Glasgow:University of Glasgow,2002.
    [4] Austin R E,Dod R E,Terwilliger C H.The ubiquitous solar electric propulsion stage[J].Acta Astronautica,1977,4(1):671-694. doi: 10.1016/0094-5765(77)90114-X
    [5] Forward R L.Light-levitated geostationary cylindrical orbits[J].Journal of the Astronautical Sciences,1981,29(1):73-80.
    [6] McInnes C R, Simmons F L.Solar sail halo orbits Ⅰ: heliocentric case[J].Journal of Spacecraft and Rockets,1992,29(4):466-471. doi: 10.2514/3.25487
    [7] McInnes C R.Passive control of displaced solar sail orbits[J].Journal of Guidance, Control, and Dynamics,1998,21(6):975-982. doi: 10.2514/2.4334
    [8] McInnes C R, Macpherson K P.Solar sail halo trajectories: dynamics and applications[A].In:42nd International Astronautical Congress[C].IAF-91-334.Montreal, 1991,5-11.
    [9] McInnes C R. Solar sail mission applications for non-Keplerian orbits[J].Acta Astronautica,1999,45(4):567-575. doi: 10.1016/S0094-5765(99)00177-0
    [10] Molostov A A, Shvartsburg A A.Heliocentric halos for a solar sail with absorption[J].Soviet Physics Dokladv,1992,37(4):149-152.
    [11] Molostov A A,Shvartsburg A A.Heliocentric synchronous halos for a solar sail with absorption[J].Soviet Physics Doklady,1992,37(4):195-197.
    [12] GONG Sheng-ping,HBAOYIN He-xi,LI Jun-feng.Solar sail formation flying around a displaced solar orbit[J/L]. Journal of Guidance, Control, and Dynamics.[2007-05-17]. DOI: 10.2514/1.24315.
    [13] McInnes C R, Simmons F L.Solar sail halo orbits Ⅱ:geocentric case[J].Journal of Spacecraft and Rockets,1992,29(4):462-479.
    [14] McInnes, C R.Non-Keplerian orbits for Mars solar reflectors[J].Journal of the British Interplanetary Society,2002,55(3/4):74-84.
  • 加载中
计量
  • 文章访问数:  2564
  • HTML全文浏览量:  132
  • PDF下载量:  598
  • 被引次数: 0
出版历程
  • 收稿日期:  2006-12-08
  • 修回日期:  2007-03-20
  • 刊出日期:  2007-06-15

目录

    /

    返回文章
    返回