In-plane/out-of-plane librations of a tethered system in elliptical orbits

被引：6
|
作者：
Takeichi, N [1 ]
Natori, MC
Okuizumi, N
机构：
[1] Univ Tokyo, Grad Sch Engn, Dept Aeronaut & Astronaut, Tokyo, Japan
[2] Inst Space & Astronaut Sci, Sagamihara, Kanagawa 229, Japan
来源：
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 2001年 / 43卷 / 142期
关键词：
tethered systems; elliptical orbits; atmospheric drag;
D O I：
10.2322/tjsass.43.196
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In-plane/out-of-plane librations of a tethered system in elliptical orbits are investigated. It is aimed to clarify the fundamental characteristics of libration of the tethered system subjected to orbital motion and atmospheric drag. Periodic solutions and their stability of a simplified 3-DOF model are analyzed in which in-plane/out-of-plane librations and longitudinal elongation of the tether are considered. It is shown that the librations become asymptotically stable or unstable because of atmospheric drag. The effects of system parameters on stability are analyzed and it is shown that the property of longitudinal elongation of the tether determines the nature of stability that is, asymptotically stable or unstable. It is also shown that the property of atmospheric drag determines only the degree of stability. Results of direct numerical simulations show the validity of the results of stability analyses. Physical interpretation of the phenomena is also clearly shown.
引用
收藏
页码：196 / 202
页数：7
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