Coupled vibration analysis of the spacecraft with the flexible shaft and solar panels assembly-Reference-Cited by-同舟云学术

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Coupled vibration analysis of the spacecraft with the flexible shaft and solar panels assembly

Published:2024-08 Issue: Volume:151 Page:109259
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cao Yuteng,Zhang Xudong,Hao Yuxin,Ge Xinsheng,Cao Dengqing^ORCID

Publisher

Elsevier BV

Reference46 articles.

1. Nonlinear attitude maneuvering of a flexible spacecraft for space debris tracking and collision avoidance;Madonna;Acta Astronaut.,2023

2. Vibration characteristics analysis of rigid-flexible spacecraft with double-direction hinged solar arrays;Xing;Acta Astronaut.,2022

3. A novel nonlinear finite element method for structural dynamic modeling of spacecraft under large deformation;Ji;Thin-Walled Struct.,2021

4. Study on the coupled dynamics of rigid-liquid-flexible spacecraft by using isogeometric analysis for liquid sloshing;Yu;Appl. Math. Model.,2023

5. Rigid-flexible coupling identification and attitude control based on deep neural networks;Zhong;Adv. Space Res.,2022

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