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Research Article

Coupled attitude-vibration analysis of an E-sail using absolute nodal coordinate formulation

Ce Zhao1Mingying Huo1( )Ji Qi2Shilei Cao1Dongfang Zhu3Lujun Sun3Hongli Sun3Naiming Qi1
School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
Ming Hsieh Department of Electrical and Computer Engineering, University of Southern California, Los Angeles, CA 90007, USA
Shanghai Academy of Spaceflight Technology, Shanghai 201109, China
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Abstract

In this study, the effects of solar wind on an electric sail (E-sail) are modeled and analyzed using an absolute nodal coordinate formulation (ANCF). First, the thrust of the charged metal tether that makes up the E-sail was analyzed and a model was established. Numerical simulations of a single metal tether were performed. Then, an overall E-sail model was established using the connection matrix, and E-sails subjected to different angular velocities were compared. Simulation results of the ANCF model and a dumbbell model were compared at different angular velocities. The results confirm that with a relatively high angular velocity, the flexible metal chain can be approximately regarded as a rigid body. However, with a small angular velocity, the flexibility of the metal chain cannot be ignored.

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Astrodynamics
Pages 249-263

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Cite this article:
Zhao C, Huo M, Qi J, et al. Coupled attitude-vibration analysis of an E-sail using absolute nodal coordinate formulation. Astrodynamics, 2020, 4(3): 249-263. https://doi.org/10.1007/s42064-020-0081-x

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Received: 27 January 2020
Accepted: 11 April 2020
Published: 13 August 2019
© Tsinghua University Press 2020