Stability analysis of in-plane and out-of-plane periodic motions of electrodynamic tether system in inclined elliptic orbit

被引:33
|
作者
Kojima, Hirohisa [1 ]
Sugimoto, Tetsuro [2 ]
机构
[1] Tokyo Metropolitan Univ, Dept Aerosp Engn, Tokyo 1910065, Japan
[2] JSAT Corp, Tokyo, Japan
关键词
Electrodynamic tether; Chaotic motion periodic orbit; Delayed feedback control; DELAYED FEEDBACK-CONTROL; GRADIENT-ORIENTED SYSTEM; LIBRATION CONTROL; NONLINEAR CONTROL; SATELLITES; DYNAMICS;
D O I
10.1016/j.actaastro.2009.02.006
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper analyzes the stability of in-plane/out-of-plane motion of electrodynamic tether (EDT) systems in elliptic and inclined orbits. The chaotic librational motion of all EDT system in inclined elliptic orbits has been studied extensively and it is believed that delayed feedback control cannot stabilize the librational motion of an EDT in an inclined and elliptic orbit with high eccentricity. Contrary to previously Published results, the analytical results in this paper reveal that delayed feedback control call the in-plane/out-of-plane coupling librational motion of EDT systems in inclined elliptic orbits with high eccentricity to a periodic motion because the in-plane and out-of-plane coupling motions do not have the odd number condition if the electric current call flow on tether in both direction, and appropriate control gains are chosen. The validity of the stability analyses in this paper is confirmed through numerical simulations in which a delayed feedback control with appropriate control gains is applied to the in-plane/out-of-plane coupling periodic motion of,in EDT system in inclined elliptic orbit with high eccentricity. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:477 / 488
页数:12
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