In-Plane/Out-of-Plane Librations of a Tethered System in Elliptical Orbits

By Noboru Takeichi; M.C.Natori; Nobukatsu Okuizumi

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In-Plane/Out-of-Plane Librations of a Tethered System in Elliptical Orbits

机译：椭圆轨道上的系留系统的平面内/平面外平动

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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. Peri- odic solutions and their stability of a simplified 3-DOF model analyzed, in which in-plant/out-of-plane libraions and longitudinal elongation of the tether are considered. It is shown that the libratoins become asymptotically stable or unstable because of atmospheric drag.

机译：研究了椭圆轨道上系留系统的平面内/平面外自由度。目的在于阐明在轨道运动和大气阻力作用下的系留系统的解放的基本特征。对简化的3-DOF模型的周期解及其稳定性进行了分析，其中考虑了植物内/平面外自由度和系链的纵向伸长率。结果表明，由于大气阻力，天冬酰胺变得渐近稳定或不稳定。

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来源
《Transactions of the Japan society for aeronautical and space sciences》 |2001年第142期|p.196-202|共7页
作者
By Noboru Takeichi; M.C.Natori; Nobukatsu Okuizumi;
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作者单位

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空;
关键词
Tethered Systems; Elliptical Orbits; Atmospheric Drag;

机译：系留系统;椭圆轨道大气阻力;

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7. Libration Control of a Tethered System in Elliptic Orbits. [O] . Noboru TAKEICHI, M.C. NATORI, Nobukatsu OKUIZUMI 2001

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8. Orbit Determination Error Analysis for an Interior Libration Point Orbit in the Sun-Earth+Moon Elliptic Restricted Three-Body Problem. [R] . Gordon, S. C. 1991

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In-Plane/Out-of-Plane Librations of a Tethered System in Elliptical Orbits

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