Constrained Motion of Tethered Satellites

Aaron D. Schutte; Brian A. Dooley

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Constrained Motion of Tethered Satellites

机译：系留卫星的运动受限

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摘要

The orbital motion of tethered satellites is a highly complex nonlinear problem. This investigation formulates a new method that significantly simplifies the dynamic analysis of tethered satellite systems. This is accomplished using the fundamental equation for constrained dynamic systems, which was formulated by Udwadia and Kalaba. As a result of this new method, a study of the periodicity of tethered satellite motion is conducted and an extension to formation flying satellites is made. With varying fixed tether lengths, the system motion seems to transition from periodic to quasi-periodic. The simplified method is also applied to the computation of the control force required for formation flight.

机译：系留卫星的轨道运动是一个高度复杂的非线性问题。这项研究制定了一种新方法，可以大大简化系留卫星系统的动态分析。这是由约束动力系统的基本方程式完成的，该方程式由Udwadia和Kalaba制定。作为这种新方法的结果，对系留卫星运动的周期性进行了研究，并扩展了编队飞行卫星。随着固定绳索长度的变化，系统的运动似乎从周期性过渡到准周期性。简化的方法也适用于编队飞行所需的控制力的计算。

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来源
《Journal of aerospace engineering》 |2005年第4期|p.242-250|共9页
作者
Aaron D. Schutte; Brian A. Dooley;
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作者单位

M4-971 Control Analysis Dept., The Aerospace Corporation, P.O. Box 92957, Los Angeles, CA 90009-2957;

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原文格式 PDF
正文语种 eng
中图分类航空、航天;建筑科学;
关键词
satellites; motion; nonlinear response;

机译：卫星;运动;非线性响应;

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专利

1. Tethered Satellite Systems: Applications, Modelling and Formulation of the Equations of Motion for Very Stiff Tethers [J] . KUHN A., STEINER W., TROGER H. Zeitschrift fur Angewandte Mathematik und Mechanik . 1996,第S4期

机译：系留卫星系统：非常僵硬的系链的运动方程的应用，建模和公式化
2. Control of pendular motion on tethered satellites systems [J] . Tirop Paul Kimutai, Zhang Jingrui Aircraft Engineering and Aerospace Technology . 2018,第9期

机译：控制系留卫星系统上的摆动
3. A "Spring-mass" model of tethered satellite systems: Properties of planar periodic motions [J] . Sidorenko V.V., Celletti A. Celestial Mechanics and Dynamical Astronomy: An international journal of space dynamics . 2010,第1a2期

机译：系留卫星系统的“弹簧质量”模型：平面周期性运动的性质
4. CONSTRAINED MOTION OF TETHERED SATELLITES [C] . Aaron Schutte, Brian Dooley American Society of Mechanical Engineers(ASME) International Design Engineering Technical Conference and Computers and Information in Engineering Conference(DETC2005) vol.6 pt.A: International Conference on Multibody Systems, Nonlinear Dynamics, and Cont . 2005

机译：人造卫星的约束运动
5. Using an electrodynamic tethered satellite as an ionospheric electric double probe to estimate tethered satellite motion and measure vertical electric field. [D] . Williams, Scott Dennis. 1999

机译：使用电动系留卫星作为电离层电双探头，以估计系留卫星的运动并测量垂直电场。
6. Comparison of the peak resolution and the stationary phase retention between the satellite and the planetary motions using the coil satellite centrifuge with counter-current chromatographic separation of 4-methylumbelliferyl sugar derivatives [O] . Kazufusa Shinomiya, Kazumasa Zaima, Yukina Harada, -1

机译：使用盘旋卫星离心机和4-甲基伞形糖衍生物的逆流色谱分离比较卫星和行星运动的峰分辨率和固定相保留
7. Orbital Transfer of a Tethered Satellite System Using Pitching Motion Control through Tether Length Variation [O] . Naritoyo SHIBATA, Shinji HOKAMOTO 2008

机译：通过系绳长度变化使用俯仰运动控制的系绳卫星系统的轨道转移
8. Dynamics Analysis of Electrodynamic Satellite Tethers. Equations of Motion and Numerical Solution Algorithms for the Tether [R] . Nacozy, P. E. 1984

机译：电动卫星系绳的动力学分析。系绳的运动方程和数值解算法

Constrained Motion of Tethered Satellites

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