首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于△DOR信号的高精度VLBI技术
引用本文:吴伟仁,王广利,节德刚,张秀忠,蒋栋荣.基于△DOR信号的高精度VLBI技术[J].中国科学:信息科学,2013(2):185-196.
作者姓名:吴伟仁  王广利  节德刚  张秀忠  蒋栋荣
作者单位:[1]探月与航天工程中心,北京100037 [2]中国科学院上海天文台,上海200030
基金项目:探月工程重人科技专项资助项目
摘    要:在嫦娥二号(CE-2)工程中,我国首次开展了X波段ADOR测量实验,获取了ADOR信号的VLBI时延数据,并用于精密定轨.本文给出了CE-2中ADOR信号的VLBI测量与数据处理方法,结合我国VLBI测量系统对时延数据进行了误差分析及精密定轨分析.结果表明:ADOR信号的VLBI时延精度优于0.5ns,比利用S波段信标的测量精度提高约一个数量级.本研究成果为后续的月球及深空探测高精度测定轨提供了重要的技术手段.

关 键 词:嫦娥二号  VLBI技术  △DOR测量  误差分析  航天器导航设备  信号处理

High-accuracy VLBI technique using △DOR signals
WU WeiRen,WANG GuangLi,JIE DeGang,ZHANG XiuZhong & JIANG DongRong.High-accuracy VLBI technique using △DOR signals[J].Scientia Sinica Techologica,2013(2):185-196.
Authors:WU WeiRen  WANG GuangLi  JIE DeGang  ZHANG XiuZhong & JIANG DongRong
Institution:1 Lunar Exploration and Space Engineer Center, Beijing 100037, China; 2 Shanghai Astronomical Observatory, Chinese Academy of Sciences, Shanghai 200030, China
Abstract:During the Chinese Lunar Project Chang'E-2 mission, a series of experiments on △DOR (delta differential one-way ranging) technology was carried out over a two week period starting on April 2, 2011. △DOR technology was first adopted in China deep space navigation, and the ADOR delay observables were obtained and used for orbit determination. In this paper, we introduce the ADOR observing technology, including the ADOR measurenmnt principles. We also discuss the experiment design, the rules for selecting the calibration quasars, the switching time choice, the signal recording setup for the channels, the △DOR data processing method implemented in the software, and our analysis of the error sources of the ADOR delay and its contribution to orbit determination based on the characteristics of the Chinese VLBI network. Through these analyses and verification studies on the orbit determination from the satellite orbits in the CE-1 and CE-2 missions, we conclude that the accuracy of the ADOR delay is about 0.5 ns, an improvement of about one order of magnitude compared with that from S-band telemetry signals of less than 1 MHz. This study presents an important technique for high precision orbit determination of lunar and deep space explorations.
Keywords:CE-2  VLBI  △DOR  error analysis  spacecraft navigation aids  signal processing
本文献已被 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号