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星载GPS低轨卫星几何法精密定轨研究

胡国荣 欧吉坤

空间科学学报2000,Vol.20Issue(1):32-39,8.
空间科学学报2000,Vol.20Issue(1):32-39,8.

星载GPS低轨卫星几何法精密定轨研究

THE THEORY OF GPS-BASED GEOMETRIC ORBIT DETERMINATION FOR LOW-EARTH SATELLITE

胡国荣 1欧吉坤1

作者信息

  • 1. 中国科学院测量与地球物理研究所武汉 430077
  • 折叠

摘要

Abstract

Methods of single frequency carrier phase-basedrelative orbit determination (OD) and kinematic network OD for low-earthsatellite are developed. From the results calculated using L1 datacollected by GPS/DR onboard Topex/Poseidon, we can draw followingconclusions: (a) the accuracy of single frequency carrier phase-basedrelative OD may attain the order of a few decimeters; (b) the accuracyof relative OD depends on the data quality of ground tracking stations; (c)the accuracy of kinematic network OD is equavalent to a weighting amongrelative ODs of different ground tracking stations and can improve the reliabilityand precision of OD due to its redundant condition and goodgeometric configuration.

关键词

相对定轨—动态网定轨—GPS

Key words

Relative orbit determination/Kinematic networkorbit determination/Global Positiong System

分类

航空航天

引用本文复制引用

胡国荣,欧吉坤..星载GPS低轨卫星几何法精密定轨研究[J].空间科学学报,2000,20(1):32-39,8.

基金项目

国防科工委重大项目子课题, 中国科学院动力大地测量学开放研究实验室资助课题 ()

空间科学学报

OA北大核心CSCDCSTPCD

0254-6124

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