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利用太阳光压力进行Halo轨道编队控制

龚胜平 李俊峰 宝音贺西

龚胜平, 李俊峰, 宝音贺西. 利用太阳光压力进行Halo轨道编队控制[J]. 应用数学和力学, 2009, 30(8): 945-952. doi: 10.3879/j.issn.1000-0887.2009.08.007
引用本文: 龚胜平, 李俊峰, 宝音贺西. 利用太阳光压力进行Halo轨道编队控制[J]. 应用数学和力学, 2009, 30(8): 945-952. doi: 10.3879/j.issn.1000-0887.2009.08.007
GONG Sheng-ping, LI Jun-feng, BAOYIN He-xi. Uses of Solar Radiation for Formation Flying Control Around the Sun-Earth Libration Point[J]. Applied Mathematics and Mechanics, 2009, 30(8): 945-952. doi: 10.3879/j.issn.1000-0887.2009.08.007
Citation: GONG Sheng-ping, LI Jun-feng, BAOYIN He-xi. Uses of Solar Radiation for Formation Flying Control Around the Sun-Earth Libration Point[J]. Applied Mathematics and Mechanics, 2009, 30(8): 945-952. doi: 10.3879/j.issn.1000-0887.2009.08.007

利用太阳光压力进行Halo轨道编队控制

doi: 10.3879/j.issn.1000-0887.2009.08.007
基金项目: 国家自然科学基金资助项目(10832004);中国博士后科学基金资助项目(20080440040)
详细信息
    作者简介:

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

  • 中图分类号: V412.4

Uses of Solar Radiation for Formation Flying Control Around the Sun-Earth Libration Point

  • 摘要: 利用太阳光压力可以实现地日限制性三体问题中L2点附近编队控制.该编队需要的控制力量级小,常规的推进方式难以实现.太阳帆能产生微小的连续光压力,可以用于Halo轨道附近的编队控制.由于太阳光压力的方向受到限制,只有部分编队构型可以利用太阳光压力实现.该文主要讨论了两种常见的编队构型——直线编队和圆编队,给出了太阳帆能实现的编队构型需要满足的条件.最后,对每种构型的编队进行了数值仿真,仿真结果表明太阳帆能有效的进行编队控制.
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出版历程
  • 收稿日期:  2008-09-04
  • 修回日期:  2009-06-12
  • 刊出日期:  2009-08-15

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