Dynamics of Lagrangian point multi-tethered satellite systems

被引：0
|
作者：
Wong, B [1 ]
Misra, AK [1 ]
机构：
[1] McGill Univ, Dept Mech Engn, Montreal, PQ H3A 2K6, Canada
来源：
JOURNAL OF THE ASTRONAUTICAL SCIENCES | 2005年 / 53卷 / 03期
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper examines the dynamics of a tether-connected multi-spacecraft system, arranged in a wheel-spoke configuration, in the vicinity of the L-2 Lagrangian point of the Sun-Earth system. Equilibrium configurations of the system are determined and small motions about one of these configurations are analyzed. A simple feedback controller is also developed to stabilize the motion of the system. Numerical simulation of the free and controlled motion of the parent mass and tether librations is carried out for a three-mass case.
引用
收藏
页码：221 / 250
页数：30
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