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

影响环月飞行器定轨精度的误差源分析
引用本文:王威,胡小工,黄勇,黄城.影响环月飞行器定轨精度的误差源分析[J].飞行器测控学报,2005,24(4):26-33.
作者姓名:王威  胡小工  黄勇  黄城
作者单位:中国科学院上海天文台·上海·200030;中国科学院研究生院·北京·100039;中国科学院上海天文台·上海·200030
摘    要:以我国正在实施的探月计划“嫦娥1号”工程为背案,在现有测控网分布、观测弧段以及尽可能接近真实情况的误差源等前提下,利用仿真模拟的方法对影响环月飞行器定轨精度的误差源进行了初步探讨和分析。重点考察了月球重力场误差、观测量精度、初始时刻的先验轨道误差以及观测资料类型等对环月飞行器定轨精度的影响。

关 键 词:环月飞行器  月球重力场  误差源  精密定轨
收稿时间:2005-01-04
修稿时间:2005-05-19

Analysis of Error Sources for Circumlunar Spacecraft Orbit Determination
Wang Wei;Hu XiaoGong;Huang Yong;Huang Cheng.Analysis of Error Sources for Circumlunar Spacecraft Orbit Determination[J].Journal of Spacecraft TT&C Technology,2005,24(4):26-33.
Authors:Wang Wei;Hu XiaoGong;Huang Yong;Huang Cheng
Abstract:To meet requirements of the on-going lunar exploration program Chang'E-1 on orbit determination, this paper uses simulation tests to analyze various error sources that would affect the orbital determination accuracy of the lunar orbiter, such as the distribution of tracking network, the observation arcs, systematic and stochastic measurement noise. Especially, the effects of lunar gravity, observation accuracy, orbital error and observation data types on the orbital determination accuracy of the lunar orbiter have been carefully investigated.
Keywords:Circumlunar Spacecraft  Lunar Gravity Field  Error Sources  Precision Orbit Determination
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《飞行器测控学报》浏览原始摘要信息
点击此处可从《飞行器测控学报》下载免费的PDF全文
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