Nonlinear dynamic modeling for analysis of large spacecraft with extendible appendages-Reference-Cited by-同舟云学术

Nonlinear dynamic modeling for analysis of large spacecraft with extendible appendages

Published:2023-11 Issue: Volume:123 Page:526-545
ISSN:0307-904X
Container-title:Applied Mathematical Modelling
language:en
Short-container-title:Applied Mathematical Modelling

Author:

Sun Tongtong,Zhang Shuo,Du Lin,Niu Lizhi,Li Qingjun^ORCID,Deng Zichen

Publisher

Elsevier BV

Subject

Applied Mathematics,Modeling and Simulation

Reference43 articles.

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3. Deployable structures: structural design and static/dynamic analysis;Zhang;J. Elast.,2021

4. Advances in dynamics and vibration control of large-scale flexible spacecraft;Cao;Chin. J. Theor. Appl. Mech.,2019

5. Attitude and orbit control of a very large geostationary solar power Satellite;Wie;J. Guidance Control Dyn.,2005

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