基于同波束VLBI测量对嫦娥五号卫星交汇对接的相对实时定位

doi:10.11947/j.AGCS.2023.20210351

测绘学报 ›› 2023, Vol. 52 ›› Issue (3): 375-382.doi: 10.11947/j.AGCS.2023.20210351

基于同波束VLBI测量对嫦娥五号卫星交汇对接的相对实时定位

郭丽^1,2, 黄逸丹¹, 李金岭^1,2, 王广利^1,2, 王文彬¹, 郑为民^1,2,3

1. 中国科学院上海天文台, 上海 200030;
2. 上海市空间导航与定位技术重点实验室, 上海 200030;
3. 国家基础学课公共科学数据中心, 北京 100190

收稿日期:2021-06-28 修回日期:2022-04-27 发布日期:2023-04-07
作者简介:郭丽(1979-),女,博士,副研究员,研究方向为卫星VLBI定位与脉冲星天体测量。E-mail:lguo@shao.ac.cn
基金资助:
国家自然科学基金(11873076;11973011); 中国探月工程(嫦娥五号任务);中国科学院关键技术人才项目;上海市领军人才项目

Real-time relative positioning of Chang'e-5 satellite in rendezvous and docking with the same-beam VLBI differential observations

GUO Li^1,2, HUANG Yidan¹, LI Jinling^1,2, WANG Guangli^1,2, WANG Wenbin¹, ZHENG Weinmin^1,2,3

1. Shanghai Astronomical Observatory, Chinese Academy of Science, Shanghai 200030, China;
2. Shanghai Key Laboratory of Space Navigation and Positioning Techniques, Shanghai 200030, China;
3. National Basic Science Data Center, Beijing 100190, China

Received:2021-06-28 Revised:2022-04-27 Published:2023-04-07
Supported by:
The National Natural Science Foundation of China (Nos. 11873076;11973011 );Chinese Lunar Exploration Project(Chang'e-5);The Key Technologies Project for the Talents by the Chinese Academy of Sciences;The Leading Talent Projects of Shanghai

摘要/Abstract

摘要： 嫦娥五号(CE-5)卫星调姿复杂,包括多次星上探测器分离及交汇对接,在两器分离或靠近阶段,我国甚长基线干涉网对其进行同波束测量。CE-5首次实现了月球距离上的卫星交汇对接。基于VLBI差分时延,本文采用差分定位方法首次实时测定了CE-5轨返组合体与上升器交汇对接过程中的相对位置。该方法能够更加直观快速地判断对接状态。CE5首次在月球以远的距离上对卫星实施月球轨道逃逸制动,本文采用瞬时状态归算方法实时监测了CE-5轨返组合体两次月地转移入射的制动过程,精确判断了轨道制动的状态,为后续深空探测的定位及轨道制动提供借鉴。

关键词: 甚长基线干涉, 定位归算, 瞬时状态参量归算, 嫦娥五号, 轨道制动

Abstract: Chang'e-5 is the most complicated mission of Chinese lunar project. Many separations of several detectors and unmanned rendezvous and docking in lunar orbit are accomplished. During the course of separating and approaching of two detectors, the same-beam very long baseline interferometry (VLBI) observations are carried on. We firstly present the real-time positioning for multi-detectors and differential positioning of CE-5 ascender and combination of orbiter-returner, which is the more direct and quick method to charge the orbit status. The CE-5 mission first achieved the orbital maneuver of CE-5 orbiter-returner combination from the lunar gravity back to the Earth at the distance of lunar orbit. We use the method of instantaneous states reduction to monitor the twice orbital transfer from the lunar to the Earth in real time, and precisely present the status of orbital maneuver, which provides the important reference for the positioning and orbit determination in the future deep-space exploration.

Key words: VLBI, positioning reduction, instantaneous states vector reduction, Chang'e-5, orbital maneuver

中图分类号:

P228

郭丽, 黄逸丹, 李金岭, 王广利, 王文彬, 郑为民. 基于同波束VLBI测量对嫦娥五号卫星交汇对接的相对实时定位[J]. 测绘学报, 2023, 52(3): 375-382.

GUO Li, HUANG Yidan, LI Jinling, WANG Guangli, WANG Wenbin, ZHENG Weinmin. Real-time relative positioning of Chang'e-5 satellite in rendezvous and docking with the same-beam VLBI differential observations[J]. Acta Geodaetica et Cartographica Sinica, 2023, 52(3): 375-382.

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基于同波束VLBI测量对嫦娥五号卫星交汇对接的相对实时定位

Real-time relative positioning of Chang'e-5 satellite in rendezvous and docking with the same-beam VLBI differential observations

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