Orbital stability of planar oscillations of a satellite in a circular orbit

被引：3

作者：

Bardin, B. S. ^{[1
]}

Chekin, A. M. ^{[1
]}

机构：

[1] Moscow Inst Aviat Technol, Moscow 125080, Russia

来源：

COSMIC RESEARCH | 2008年 / 46卷 / 03期

基金：

俄罗斯基础研究基金会;

关键词：

D O I：

10.1134/S0010952508030118

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

We consider the attitude motion of a satellite with a circular orbit in a central Newtonian gravitational field. The satellite is a solid body whose mass geometry is that of a plate. A nonlinear analysis is made of orbital stability of planar oscillations of the satellite at which its middle or major axis of inertia is perpendicular to the orbit plane. At small amplitudes of oscillations the analysis of stability was made analytically, while for arbitrary amplitudes the numerical analysis was performed.

引用

页码：273 / 282

页数：10

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