Attitude-Orbit Dynamical Coupling in Tethered Systems

机译：系留系统中的姿态-轨道动力耦合

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Conductive tethered systems taking advantage of electrodynamics force are currently proposed for spacecraft deorbiting. In the present paper a simplified model is considered, namely a dumbbell subjected to the gravity and electrodynamics field. The attitude and orbital coupling on this model is analysed in order to study the impact on the stability of the complete system. Then a more complex model of the tethered system is developed to simulate the dynamic wire behaviour. Numerical simulations are performed to test the feasibility of tethered as deorbit device.

机译：当前提出了利用电动力的导电系留系统用于航天器的去轨道化。在本文中，考虑了简化模型，即哑铃受到重力和电动力学场的影响。分析了该模型的姿态和轨道耦合，以研究对整个系统稳定性的影响。然后，开发了一个更复杂的系留系统模型，以模拟动态导线行为。进行数值模拟以测试系留装置作为脱轨装置的可行性。

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来源
《Cranfield Conference on Dynamica and Control of Systems and Structures in Space; 2004; Liguria; IT》|2004年|P.475-487|共13页
会议地点 Liguria(IT)
作者
Silvano Sgubini; Paolo Teofilatto;
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Scuola di Ingegneria Aerospaziale di Roma Universita degli Studi di Roma 'La Sapienza', Roma, Italy;

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原文格式 PDF
正文语种 eng
中图分类动力装置;
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Attitude-Orbit Dynamical Coupling in Tethered Systems

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