DYNAMICS OF A TETHERED SATELLITE SUBJECTED TO AERODYNAMIC FORCES

被引：15
作者：
DEMATTEIS, G
DESOCIO, LM
机构：
[1] Department of Mechanics and Aeronautics, University of Rome “La Sapienza”, Rome, 00184
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1991年 / 14卷 / 06期
关键词：
D O I：
10.2514/3.20767
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The equations of motion of a subsatellite and its tether are studied to show the influence of the aerodynamic forces on the equilibrium states of the system and the corresponding perturbed motion. It is shown that aerodynamic forces can play a major role in determining the stability of the system equilibrium states in situations of practical interest.
引用
收藏
页码：1129 / 1135
页数：7
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