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May 31, 2026Zhongguo kexue. Wulixue Lixue Tianwenxue0 citations

Application of satellite laser ranging to precise orbit determination of cislunar spacecraft

RGRenfang GengYMYunlong MaZZZhenghao Zhang

Key Points

  • The aim is to enhance the orbit determination accuracy of cislunar spacecraft using satellite laser ranging data.
  • Conducted laser ranging tests with TD-1 and DRO-A spacecraft in April 2025.
  • Compared laser ranging data with existing radio ranging results for accuracy validation.
  • Integrated laser and radio ranging data for joint orbit determination analysis.
  • Achieved radial accuracy of under 5 m for TD-1 and under 20 m for DRO-A.
  • Improved TD-1 3D positioning accuracy from 656 m to 179 m.
  • Enhanced DRO-A 3D positioning accuracy from 854 m to 266 m.

Abstract

地月空间飞行器高精度测定轨是保障各类探测任务顺利实施的重要基础. 2025年4月, 天都一号通导技术试验星(TD-1)和绕月远距离逆行轨道卫星(DRO-A)成功开展了地月空间大口径单角锥反射器激光测距试验, 本文对试验获得的激光测距数据进行了分析, 开展基于激光测距数据的地月空间飞行器精密定轨研究. 首先利用卫星激光测距数据对基于深空测控网无线电测距数据的定轨结果进行外部检核, DRO-A和TD-1无线电测距精密定轨的径向精度分别优于5 m和20 m; 进一步分析了地月空间卫星激光测距对轨道预报精度的需求, 对于运行于地月2:1共振轨道的DRO-A和地月往返轨道的TD-1而言, 采用2天地基无线电测距数据可满足卫星激光测距对轨道预报的需求, 无线电测距辅助卫星激光测距建链的模式可降低对预报轨道精度的依赖; 最后融合无线电测距与卫星激光测距数据开展联合定轨, TD-1重叠弧段三维位置精度由656 m提高至179 m, DRO-A三维位置精度由854 m提高至266 m.

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Cite This Study

Geng et al. (2026) studied this question.

synapsesocial.com/papers/6a1bcfe15783ba022b6fbc1chttps://doi.org/10.1360/sspma-2026-0280
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