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基于地基测量数据的月球DRO轨道定轨精度分析

黄逸丹 黄勇 樊敏 李培佳

深空探测学报(中英文)2024,Vol.11Issue(4):405-413,9.
深空探测学报(中英文)2024,Vol.11Issue(4):405-413,9.DOI:10.15982/j.issn.2096-9287.2024.20230099

基于地基测量数据的月球DRO轨道定轨精度分析

Analysis of Cislunar DRO Orbit Determination Accuracy Using Earth-Based Simulated Observations

黄逸丹 1黄勇 2樊敏 3李培佳4

作者信息

  • 1. 中国科学院 上海天文台,上海 200030
  • 2. 中国科学院 上海天文台,上海 200030||中国科学院大学,北京 100049||上海市空间导航与定位技术重点实验室,上海 200030||中国科学院 行星科学重点实验室,上海 200030
  • 3. 北京跟踪与通信技术研究所,北京 100094
  • 4. 中国科学院 上海天文台,上海 200030||上海市空间导航与定位技术重点实验室,上海 200030||中国科学院 行星科学重点实验室,上海 200030
  • 折叠

摘要

Abstract

Based on the existing tracking and measuring conditions of China's deep space exploration missions,the orbit determination accuracy of the DRO probe was simulated and analyzed.For the Cislunar space DRO exploration,the simulation adopted batch processing orbit determination method,selected celestial bodies centered on the Earth for orbit integration,and increased non-spherical gravitational perturbation of the moon.Under the current measurement conditions,the position and velocity accuracy of 2-day short-arc orbit determination using only range tracking data were the order of km and better than 3 cm/s respectively;for 7-day predictions,the maximum differences in the position and velocity are the order of ten kilometers and 6 cm/s respectively.When using ranging data combined with VLBI data,the position and velocity accuracy were the order of hundreds of meters and less than 0.4 cm/s respectively;for 7-day predictions,the maximum differences in the position and velocity were the order of kilometers and 2 cm/s respectively,which shows that VLBI data significantly improved the accuracy of short-arc orbit determination and prediction.Moreover,the position and velocity accuracy were better than 1 km and 1cm/s respectively when using 5-day long-arc range tracking data.For 7-day predictions,the maximum differences in the position and velocity were less than 2 km and 1cm/s respectively.This shows that an increase of ranging data significantly contributes to the accuracy of orbit determination and prediction for DRO.

关键词

地月系/远距离逆行轨道(DRO)/甚长基线干涉测量(VLBI)/定轨/预报

Key words

cislunar/Distant Retrograde Orbit(DRO)/Very Long Baseline Interferometry(VLBI)/orbit determination/orbit prediction

分类

航空航天

引用本文复制引用

黄逸丹,黄勇,樊敏,李培佳..基于地基测量数据的月球DRO轨道定轨精度分析[J].深空探测学报(中英文),2024,11(4):405-413,9.

基金项目

中国科学院战略性先导科技专项(XDA30000000) (XDA30000000)

科工局民用航天技术预先研究项目(D010105) (D010105)

国家重点研发计划资助(2020YFC2200903) (2020YFC2200903)

国家重点研究计划"协同精准定位项目"(2016YFB0501900) (2016YFB0501900)

上海市科学技术委员会(12DZ2273300) (12DZ2273300)

航天飞行动力学技术重点实验室基金(KGJ6142210200201) (KGJ6142210200201)

深空探测学报(中英文)

OA北大核心CSTPCD

2096-9287

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