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嫦娥六号飞行方案的任务几何规划方法

孟占峰 高珊 赵峭 张相宇

中国空间科学技术(中英文)2024,Vol.44Issue(6):1-15,15.
中国空间科学技术(中英文)2024,Vol.44Issue(6):1-15,15.DOI:10.16708/j.cnki.1000-758X.2024.0086

嫦娥六号飞行方案的任务几何规划方法

Chang'e-6 mission planning leveraging geometry approach

孟占峰 1高珊 1赵峭 1张相宇1

作者信息

  • 1. 北京空间飞行器总体设计部,北京 100094
  • 折叠

摘要

Abstract

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.

关键词

嫦娥六号/任务几何/飞行方案规划/逆行轨道/月球探测

Key words

Chang'e-6 mission/mission geometry/mission planning/retrograde orbit/lunar exploration

分类

航空航天

引用本文复制引用

孟占峰,高珊,赵峭,张相宇..嫦娥六号飞行方案的任务几何规划方法[J].中国空间科学技术(中英文),2024,44(6):1-15,15.

中国空间科学技术(中英文)

OA北大核心CSTPCD

1000-758X

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