DRAG PERTURBATIONS IN ARTIFICIAL-SATELLITE ORBITAL MOTION BASED ON THE TOTAL DENSITY MODEL

被引：4
|
作者：
MIOC, V
机构：
[1] Astronomical Observatory, Cluj
来源：
ASTRONOMISCHE NACHRICHTEN | 1991年 / 312卷 / 02期
关键词：
ARTIFICIAL SATELLITES; ATMOSPHERIC DRAG PERTURBATIONS; TD THERMOSPHERIC MODEL;
D O I：
10.1002/asna.2113120215
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
Analytical expressions for the aerodynamic drag perturbations undergone by five independent orbital elements of an artificial satellite moving in an orbit with small eccentricity, over a nodal period, are established. All three components of the perturbing acceleration are taken into account. The TD model is used to describe the density distribution of the upper atmosphere.
引用
收藏
页码：127 / 132
页数：6
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