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基于CEI的航天器交会对接段的轨道监控
引用本文:李晓杰,杜兰,黄金,潘玲.基于CEI的航天器交会对接段的轨道监控[J].中国空间科学技术,2010,30(6):24-30.
作者姓名:李晓杰  杜兰  黄金  潘玲
作者单位:(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)
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  
收稿时间:2010-03-11

CEI-based Real-time Orbit Determination of Spacecraft Rendezvous and Docking in the Course of Long Distance Navigation
Li Xiaojie,Du Lan,Huang Jin,Pan Ling.CEI-based Real-time Orbit Determination of Spacecraft Rendezvous and Docking in the Course of Long Distance Navigation[J].Chinese Space Science and Technology,2010,30(6):24-30.
Authors:Li Xiaojie  Du Lan  Huang Jin  Pan Ling
Institution:(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)
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.
Keywords:Short baseline connected element interferometry  Rendezvous and docking Integer ambiguity  Extended Kalman filter  Spacecraft  
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