Reducing Influence of Gravity Model Error in Precise Orbit Determination of Low Earth Orbit Satellites

被引：0
|
作者：
Guo Jinlai [1 ]
Hu Min [1 ]
Zhao Qile [1 ]
Guo Daoyu [1 ]
机构：
[1] Wuhan Univ, Sch Geodesy & Geomat, 129 Luoyu Rd, Wuhan 430079, Hubei, Peoples R China
来源：
GEO-SPATIAL INFORMATION SCIENCE | 2007年 / 10卷 / 02期
基金：
中国国家自然科学基金;
关键词：
precise orbit determination; gravity model; orbit fitting;
D O I：
10.1007/s11806-007-0055-7
中图分类号：
TP7 [遥感技术];
学科分类号：
081102 ; 0816 ; 081602 ; 083002 ; 1404 ;
摘要：
Based on the orbit integration and orbit fitting method, the influence of the characters of the gravity model, with different precisions, on the movement of low Earth orbit satellites was studied. The way and the effect of absorbing the influence of gravity model error on CHAMP and GRACE satellite orbits, using linear and periodical empirical acceleration models and the so-called "pseudo-stochastic pulses" model, were also analyzed.
引用
收藏
页码：105 / 110
页数：6
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