Dynamics and control of tethered satellite systems

被引：107
|
作者：
Misra, A. K. [1 ]
机构：
[1] McGill Univ, Montreal, PQ H3A 2K6, Canada
来源：
ACTA ASTRONAUTICA | 2008年 / 63卷 / 11-12期
关键词：
Tethered satellites; Deployment/retrieval dynamics; Elastic oscillations;
D O I：
10.1016/j.actaastro.2008.06.020
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Dynamics and control of two-body and n-body tethered satellites are considered. At first, nonlinear roll and pitch motions of two-body systems are examined. Then the effects of aerodynamic and electrodynamic forces on the stability of a tethered satellite are discussed. Various control schemes to stabilize the dynamics during retrieval of the subsatellite are described. Finally, some dynamics and stability results for n-body tethered satellites are presented. (c) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码：1169 / 1177
页数：9
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