›› 2010, Vol. 30 ›› Issue (6): 24-30.

• 研究探讨 • 上一篇    下一篇

基于CEI的航天器交会对接段的轨道监控

李晓杰1, 杜兰1, 黄金2, 潘玲3   

  1. (1 解放军信息工程大学测绘学院,郑州 450052) (2 北京遥感信息研究所,北京 100192) (3 中国人民解放军,成都 610036)
  • 收稿日期:2010-03-11 修回日期:2010-04-20 出版日期:2010-12-25 发布日期:2010-12-25
  • 通讯作者: 李晓杰 现为解放军信息工程大学测绘学院大地测量学与测量工程博士研究生。 E-mail:lxjiant1984@126.com
  • 作者简介:李晓杰 1984年生,2009年获解放军信息工程大学测绘学院天体测量与天体力学专业硕士学位,现为解放军信息工程大学测绘学院大地测量学与测量工程博士研究生。研究方向为卫星轨道确定。
  • 基金资助:

    国家自然科学基金(40974019)

CEI based Real time Orbit Determination of Spacecraft Rendezvous and Docking in the Course of Long Distance Navigation

LI  Xiao-Jie1, DU  Lan1, HUANG  Jin2, PAN  Ling3   

  1. (1 Institute of Surveying & Mapping, The PLA Information Engineering University, Zhengzhou 450052)
    (2 Beijing Remote Sensing Information Academe, Beijing 100192) (3 The Chinese People′s Liberation Army, Chengdu 610036)
  • Received:2010-03-11 Revised:2010-04-20 Online:2010-12-25 Published:2010-12-25

摘要: 文章探讨了CEI技术在飞船交会对接远程导引段的实时监控的能力,采用单一绝对滤波器的方案进行实时轨道计算,仿真结果表明:采用滤波稳定后固定模糊度的方法可以提高轨道的滤波解精度,相对轨道位置精度可达十米级,速度精度可达厘米每秒级,满足远程导引段的精度指标。

关键词: 中短基线相位干涉测量, 交会对接, 整周模糊度, 扩展卡尔曼滤波, 航天器

Abstract: Connected element interferometry (CEI) is a passive angular tracking method with the characteristic of short baselines, flexible network distribution and nearly real time processing. It can make realtime and precise orbit determination for spacecraft rendezvous and docking.CEI based real time orbit determination in the course of long distance navigation of spacecraft rendezvous and docking was discussed, and the method of absolute filter was adopted. The simulation results indicat that the method of fixing integer ambiguity after the filter is stable, and can improve the orbit precision. The relative position precision can reach the magnitude of 10m, and the relative velocity precision reaches the magnitude of 1cm per second.

Key words: Short baseline connected element interferometry, Rendezvous and docking Integer ambiguity, Extended Kalman filter, Spacecraft