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Research Article

Dynamic analysis of tethered defunct satellites with solar panels

Rui Qi1( )Yang Zhang1Heng Jiang2Rui Zhong2
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
School of Aerospace Astronautics, Beihang University, Beijing 100191, China
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Abstract

A precise dynamic model for towing and removing a defunct satellite with solar panels in orbit using a tethered net often has low computational efficiency owing to the complex contact and collision between the net and panels, which is not conducive to research. To solve this problem, a “single main tether-multiple subtether” bifurcation structure with beads was employed as the tethered net model. This study investigated the dynamics of tethered defunct satellites with solar panels, particularly the behavior of the attitude of the tethered satellite, oscillation of the main tether, and vibration of solar panels under different conditions. The results showed that different attachment configurations of the subtethers and the flexibility of the main tether have an evident impact on the dynamic characteristics of the system.

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Astrodynamics
Pages 297-309
Cite this article:
Qi R, Zhang Y, Jiang H, et al. Dynamic analysis of tethered defunct satellites with solar panels. Astrodynamics, 2024, 8(2): 297-309. https://doi.org/10.1007/s42064-024-0206-8

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Received: 16 November 2023
Accepted: 18 February 2024
Published: 13 May 2024
© Tsinghua University Press 2024
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