A second order analytical atmospheric drag theory based on the TD88 thermospheric density model

被引：0

作者：

Abd El-Salam, FA ^{[1
]}

Sehnal, L

机构：

[1] Cairo Univ, Fac Sci, Dept Astron, Cairo, Egypt

[2] Acad Sci Czech Republ, Ondrejov Astron Inst, Ondrejov, Czech Republic

来源：

CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY | 2004年 / 90卷 / 3-4期

关键词：

drag perturbations; TD88; model; artificial satellites; ROHINI; MIMOSA;

D O I：

暂无

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

A second order atmospheric drag theory based on the usage of TD88 model is constructed. It is developed to the second order in terms of TD88 small parameters K-n,K-j. The short periodic perturbations, of all orbital elements, are evaluated. The secular perturbations of the semi-major axis and of the eccentricity are obtained. The theory is applied to determine the lifetime of the satellites ROHINI (1980 62A), and to predict the lifetime of the microsatellite MIMOSA. The secular perturbations of the nodal longitude and of the argument of perigee due to the Earth's gravity are taken into account up to the second order in Earth's oblateness.

引用

页码：361 / 389

页数：29