Predicting the on-orbit thermally induced vibration through the integrated numerical and experimental approach-Reference-Cited by-同舟云学术

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Predicting the on-orbit thermally induced vibration through the integrated numerical and experimental approach

Published:2022-03 Issue: Volume:192 Page:341-350
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Wang Jing,Jin Dengge^ORCID,Fan Chao^ORCID,Bi Yanqiang,Su Xinming,Liu Guoqing,Xiang Zhihai

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Attitude drift of space vehicles;Thomson;J. Astronaut. Sci.,1960

2. Explanation of the anomalous spin behavior of satellites with long flexible antennae;Etkin;J. Spacecraft Rockets,1967

3. Gravity-gradient stabilization of earth satellites;Kershner;IFAC Proceedings Volumes,1965

4. Thermally Induced Vibrations of Spacecraft Booms;Foster,1998

5. Thermally induced vibrations of beams;Boley;J. Aeronaut. Sci.,1956

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