Application of the GPS system for preliminary satellite orbit determination

被引：0
|
作者：
Chiaradia, APM [1 ]
Fernandes, SD [1 ]
deMoraes, RV [1 ]
机构：
[1] UNESP,FEG,DMA,GRP DYNAM ORBITAL & PLANETOL,BR-12500000 GUARATINGUETA,SP,BRAZIL
来源：
ORBIT DETERMINATION AND ANALYSIS | 1997年 / 19卷 / 11期
关键词：
D O I：
10.1016/S0273-1177(97)00322-0
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this paper, we discuss a method of preliminary orbit determination for an artificial satellite based on the navigation message of the GPS constellation. Orbital elements are considered as state variables and a simple dynamic model, based on the classic two-body problem, is used. The observations are formed by range and range and range-rate with respect to four visible GPS. A discrete Kalman filter with simulated data is used as filtering technique. The data are obtained through numerical propagation (Cowell's method), which considers special perturbations for the GPS satellite constellation and a user satellite. (C) 1997 COSPAR. Published by Elsevier Science Ltd.
引用
收藏
页码：1671 / 1675
页数：5
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