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旋转大气下火星探测器轨道捕获

吕敬 张明明 龚胜平

吕敬, 张明明, 龚胜平等 . 旋转大气下火星探测器轨道捕获[J]. 北京航空航天大学学报, 2013, 39(3): 315-319,375.
引用本文: 吕敬, 张明明, 龚胜平等 . 旋转大气下火星探测器轨道捕获[J]. 北京航空航天大学学报, 2013, 39(3): 315-319,375.
Lü Jing, Zhang Mingming, Gong Shengpinget al. Aerocaptureperiod under rotating atmospheric environment for Mars vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(3): 315-319,375. (in Chinese)
Citation: Lü Jing, Zhang Mingming, Gong Shengpinget al. Aerocaptureperiod under rotating atmospheric environment for Mars vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(3): 315-319,375. (in Chinese)

旋转大气下火星探测器轨道捕获

基金项目: 国家自然科学基金资助项目(10832004,11102006);凡舟基金资助项目(20110502)
详细信息
    作者简介:

    吕敬(1979-),女,河北廊坊人,讲师,lvjing@buaa.edu.cn.

  • 中图分类号: V412.4+1

Aerocaptureperiod under rotating atmospheric environment for Mars vehicle

  • 摘要: 针对大气辅助捕获下多次穿越的方式,分别建立探测器气动捕获段在静止大气和旋转大气模型下的轨道动力学方程并进行相应的动力学仿真,分析旋转大气对轨道捕获的影响.根据仿真结果,给出了在两种大气模型下完成目标捕获时,任务耗时以及探测器所受的热量、过载情况,通过给定不同目标轨道近火点高度,得出两种大气模型下卫星轨道的轨道参数变化形式.结论表明:当目标轨道近火点高度较低时,旋转大气对探测器轨道参数的变化形式影响较大,应该考虑旋转大气的影响.

     

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出版历程
  • 收稿日期:  2012-02-28
  • 网络出版日期:  2013-03-31

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