中国空间科学技术

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月球垂直软着陆轨道初步设计

林胜勇,李珠基,和兴锁   

  1. 西北工业大学,上海宇航系统工程研究所,西北工业大学 西安710072 ,上海201108 ,西安710072
  • 发布日期:2005-04-25

Preliminary Design and Characteristics of Vertical Soft-landing Trajectory to the Moon

Lin Shengyong * Li Zhuji ** He Xingsuo * (*Northwestern Polytechnical University, Xi'an 710072) (**Aerospace System Engineering of Shanghai, Shanghai 201108)   

  • Online:2005-04-25

被引次数

5

摘要： 采用圆锥曲线拼接法,建立了月球垂直着陆的数学模型;推导了地月转移轨道和一些重要参数的初步设计和计算方法。通过仿真,给出了理想情况下和考虑推力大小时月球垂直着陆轨道运动特性。对运动特性的分析结果可为轨道初步设计提供一定的参考。

关键词: 垂直着陆, 软着陆, 轨道分析, 月球探测

Abstract: A patched-conic technique is used to formulate the mathematical model of vertical soft-landing trajectory to the moon. Some formulas of preliminary design of transfer orbit from the earth to the moon are derived. The characteristics of the trajectory are presented by simulation. The analysis results can serve as a guidance for preliminary trajectory design.