LAGEOS spin axis and non-gravitational excitations of its orbit

被引:18
作者
Métris, G
Vokrouhlicky, D
Ries, JC
Eanes, RJ
机构
[1] Observ Cote Azur, Dept CERGA, F-06130 Grasse, France
[2] Charles Univ, Inst Astron, CR-18000 Prague 8, Czech Republic
[3] Univ Texas, Ctr Space Res, Austin, TX 78712 USA
来源
SATELLITE DYNAMICS, ORBIT ANALYSIS AND COMBINATION OF SPACE TECHNIQUES | 1999年 / 23卷 / 04期
关键词
D O I
10.1016/S0273-1177(99)00142-8
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The analysis of the orbit residuals of LAGEOS-type satellites provides an opportunity to measure tiny perturbing forces of non-gravitational origin. Some of these effects require a knowledge of the satellite spin axis orientation. Until 1996, a standard dynamical model of the LAGEOS spin axis evolution was able to explain most of the residual excitations. This is no longer the case after 1996. However, the orbit residuals can still be successfully explained if the axis dynamical model is supplemented by empirical corrections. A good agreement with direct observations of the LAGEOS axis orientation in 1995 and 1996 enhances credibility of these empirical modifications. Their theoretical understanding remains an interesting challenge for the future. (C) 1999 COSPAR. Published by Elsevier Science Ltd.
引用
收藏
页码:721 / 725
页数:5
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