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| 航天器交会对接远程导引段的精密轨道确定 | |
| 引用本文： | 李晓杰,黄金,潘玲.航天器交会对接远程导引段的精密轨道确定[J].测绘信息与工程,2010,35(5):32-34. |
| 作者姓名： | 李晓杰 黄金 潘玲 |
| 作者单位： | 1. 信息工程大学测绘学院,郑州市陇海中路66号,450052 2. 61768部队,三亚市2019信箱,572011 3. 78155部队,成都市蜀兴西街16号,610036 |
| 基金项目： | 国家自然科学基金资助项目(40974019) |
| 摘 要： | 探讨了CEI技术在飞船交会对接远程导引段的高精度定位与监控的能力,采用了差分相位延迟和相位延迟率为观测量进行轨道解算,仿真结果表明可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 精密轨道确定 |
CEI-BASED ORBIT DETERMINATION OF SPACERAFT RENDEZVOUS AND DOCKING IN COURSE OF LONG DISTANCE NAVIGATION |
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| LI Xiaojie,HUANG Jin,PAN Ling.CEI-BASED ORBIT DETERMINATION OF SPACERAFT RENDEZVOUS AND DOCKING IN COURSE OF LONG DISTANCE NAVIGATION[J].Journal of Geomatics,2010,35(5):32-34. | |
| Authors: | LI Xiaojie HUANG Jin PAN Ling |
| Institution: | LI Xiaojie1 HUANG Jin2 PAN Ling3(1 Institute of Surveying , Mapping,Information Engineering University,66 Middle Longhai Road,Zhengzhou 450052,China,2 61768 Troops,P.O.Box 2019,Sanya 572011,3 78155 Troops,16 West Shuxing Street,Chengdu 610036,China) |
| Abstract: | CEI-based orbit determination precision of spacecraft rendezvous and docking in the course of long distance navigation was analyzed.The simulation results indicated that the relative position precision could be decreased to no more than 100 m,the relative velocity precision reached to magnitude of 1 cm/s when the observation data are abundant. |
| Keywords: | short baseline connected-element interferometry rendezvous docking integer ambiguity precise orbit determination |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |