Deployment of a tethered satellite under the action of a braking force

被引：0
|
作者：
Wiedermann, G [1 ]
Steindl, A [1 ]
Troger, H [1 ]
机构：
[1] Vienna Univ Technol, Inst Mech, A-1040 Vienna, Austria
来源：
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK | 2000年 / 80卷
关键词：
D O I：
暂无
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
Force braked deployment for a system of two satellites in orbit around the earth connected by a thin tether is simulated by means of a Finite Element analysis following the approach proposed in [5].
引用
收藏
页码：S853 / S854
页数：2
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