嫦娥六号飞行方案的任务几何规划方法

V412.4; 嫦娥六号任务实现了国际首次月背无人采样返回.飞行方案规划是探测器总体设计中重要的工作之一.传统的飞行方案规划方法通常将飞行方案规划转化为约束优化问题,存在着约束条件不能直接满足的缺点,并带来设计变量多、计算效率低、物理意义不明确等问题.提出了一种新的基于任务几何的飞行方案规划方法.该方法通过空间任务几何分析,充分利用地月和月地转移轨道对近月点位置的约束、日-地-月天体运动约束以及采样点与环月轨道面的几何约束,降低了设计变量维度,进而直接导出了飞行任务规划结果.该方法由于任务几何条件直接满足设计约束,因此大幅度提升了计算效率,同时还具有几何意义直观明确、设计结果易于验证等优点.该...

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Published in中国空间科学技术（中英文） Vol. 44; no. 6; pp. 1 - 15
Main Authors 孟占峰, 高珊, 赵峭, 张相宇
Format Journal Article
LanguageChinese
Published 北京空间飞行器总体设计部,北京 100094 05.12.2024
Subjects
月球探测
retrograde orbit
mission geometry
嫦娥六号
mission planning
飞行方案规划
逆行轨道
lunar exploration
任务几何
Chang'e-6 mission
Online AccessGet full text
ISSN1000-758X
DOI10.16708/j.cnki.1000-758X.2024.0086

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Abstract V412.4; 嫦娥六号任务实现了国际首次月背无人采样返回.飞行方案规划是探测器总体设计中重要的工作之一.传统的飞行方案规划方法通常将飞行方案规划转化为约束优化问题,存在着约束条件不能直接满足的缺点,并带来设计变量多、计算效率低、物理意义不明确等问题.提出了一种新的基于任务几何的飞行方案规划方法.该方法通过空间任务几何分析,充分利用地月和月地转移轨道对近月点位置的约束、日-地-月天体运动约束以及采样点与环月轨道面的几何约束,降低了设计变量维度,进而直接导出了飞行任务规划结果.该方法由于任务几何条件直接满足设计约束,因此大幅度提升了计算效率,同时还具有几何意义直观明确、设计结果易于验证等优点.该方法已经成功应用于嫦娥五号和嫦娥六号任务的飞行方案规划和轨道设计中,对后续月球探测型号也有推广和应用价值.
AbstractList V412.4; 嫦娥六号任务实现了国际首次月背无人采样返回.飞行方案规划是探测器总体设计中重要的工作之一.传统的飞行方案规划方法通常将飞行方案规划转化为约束优化问题,存在着约束条件不能直接满足的缺点,并带来设计变量多、计算效率低、物理意义不明确等问题.提出了一种新的基于任务几何的飞行方案规划方法.该方法通过空间任务几何分析,充分利用地月和月地转移轨道对近月点位置的约束、日-地-月天体运动约束以及采样点与环月轨道面的几何约束,降低了设计变量维度,进而直接导出了飞行任务规划结果.该方法由于任务几何条件直接满足设计约束,因此大幅度提升了计算效率,同时还具有几何意义直观明确、设计结果易于验证等优点.该方法已经成功应用于嫦娥五号和嫦娥六号任务的飞行方案规划和轨道设计中,对后续月球探测型号也有推广和应用价值.
Abstract_FL The Chang'e-6 mission is the first lunar far-side sampling return mission in the world.The mission planning is an important assignment in the spacecraft system design.Mission planning problem is conventionally converted to the numerical constraints optimization problem in the traditional method.However,by using this method,the constraints could not be satisfied directly,and at the same time,the design variables dimension increased,the computing efficiency decreased,and the physical meaning was not apparent.A new mission planning approach using the mission geometry is proposed in this paper.According to the new approach,the periapsis constraints of the Earth-to-Moon and Moon-to-Earth transfer trajectories,the relative geometry constraints on sampling point and lunar orbit plane,and the geometry relationship of the Sun-Earth-Moon are fully considered.The new approach reduced the design variables dimension,improved the computing efficiency.In addition,it also has the advantage of intuitive spatial geometric interpretation,and the result can be verified easily.The new approach has been applied to mission planning and trajectory design in the Chang'e-5 and Chang'e-6 missions successfully,and will be adopted in the future lunar exploration mission.
Author 高珊
赵峭
张相宇
孟占峰
AuthorAffiliation 北京空间飞行器总体设计部,北京 100094
AuthorAffiliation_xml – name: 北京空间飞行器总体设计部,北京 100094
Author_FL MENG Zhanfeng
ZHAO Qiao
GAO Shan
ZHANG Xiangyu
Author_FL_xml – sequence: 1
  fullname: MENG Zhanfeng
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  fullname: ZHANG Xiangyu
Author_xml – sequence: 1
  fullname: 孟占峰
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Keywords 月球探测
retrograde orbit
mission geometry
嫦娥六号
mission planning
飞行方案规划
逆行轨道
lunar exploration
任务几何
Chang'e-6 mission
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PublicationTitle 中国空间科学技术（中英文）
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Snippet V412.4; 嫦娥六号任务实现了国际首次月背无人采样返回.飞行方案规划是探测器总体设计中重要的工作之一.传统的飞行方案规划方法通常将飞行方案规划转化为约束优化问题,存在...
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Title 嫦娥六号飞行方案的任务几何规划方法
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