柔性系留卫星系统建模与仿真

2018 15th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE) Pub Date : 2018-09-01 DOI:10.1109/ICEEE.2018.8533913

Najmeh Keshtkar, Manuel Sanjurjo Rivo, A. Poznyak, S. Keshtkar

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引用次数: 1

摘要

本文给出了圆形轨道上柔性系留卫星系统的动力学方程。该缆绳被建模为点质量与无质量杆连接的组合。该模型考虑了锚索的柔度和分布质量。数值实验结果表明，该模型对分析系统的纵向和横向振动是有效的。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Modeling and Simulation of Flexible Tethered Satellite System

This paper presents the dynamic equations of a flexible tethered satellite system in a circular orbit. The tether is modelled as a combination of point masses connected with massless rods. Through this model the flexibility and distributed mass of tether are considered. The results of the numerical experiments show the effectiveness of the proposed model for analysing the longitudinal and transverse oscillations of the system.

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来源期刊

2018 15th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)

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