Fundamental earth orientation parameters in determining the accuracy of the long-term ephemeris-time corrections in satellite navigation

被引：1

作者：

Markov, Yu. G. ^{[1
]}

Perepelkin, V. V. ^{[1
]}

Chazov, V. V. ^{[2
]}

Shemyakov, A. O. ^{[1
]}

机构：

[1] Natl Res Univ, Moscow Aviat Inst, Moscow 119334, Russia

[2] Moscow MV Lomonosov State Univ, Sternberg Astron Inst, Moscow 119991, Russia

来源：

DOKLADY PHYSICS | 2015年 / 60卷 / 12期

基金：

俄罗斯基础研究基金会;

关键词：

Etalons;

D O I：

10.1134/S1028335815120113

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

A few-parameter numerical-analytical model for the rotational-oscillatory motions of the Earth is used on long time intervals in the processing of the highly accurate measurements of the topocentric distances to the Etalon-1 and Etalon-2 artificial Earth satellites. A proposed model can be used in satellite navigation algorithms.

引用

页码：577 / 581

页数：5

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