Dynamics and control of spacecraft solar array deployment considering physical contacts between locking mechanisms-Reference-Cited by-同舟云学术

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Dynamics and control of spacecraft solar array deployment considering physical contacts between locking mechanisms

Published:2022-06 Issue: Volume:195 Page:481-492
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Wang Hongdong^ORCID,Wang Jianyao^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. A minimum state multibody/FEM approach for modeling flexible orbiting space systems[J];Pisculli;Acta Astronaut.,2015

2. Integral dynamics modelling of chain-like space robot based on n-order dual number[J];Wu;Acta Astronaut.,2020

3. Active control technology for flexible solar array disturbance suppression[J];Guo;Aero. Sci. Technol.,2020

4. Modeling of the deployment process dynamics for large-sized transformable space structures;Bakulin;Russian Aeronaut.,2020

5. Deployment analysis and control of deployable space antenna[J];Li;Aero. Sci. Technol.,2012

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2. Effects of different deployment strategies on the dynamic characteristics of bidirectional solar array;Journal of Physics: Conference Series;2024-05-01

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