Dynamic characteristics of flexible spacecraft with double solar panels subjected to solar radiation-Reference-Cited by-同舟云学术

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Dynamic characteristics of flexible spacecraft with double solar panels subjected to solar radiation

Published:2019-02 Issue: Volume:151 Page:22-32
ISSN:0020-7403
Container-title:International Journal of Mechanical Sciences
language:en
Short-container-title:International Journal of Mechanical Sciences

Author:

Liu Lun,Wang Xiaodong,Sun Shupeng,Cao Dengqing,Liu Xiyu

Funder

China Postdoctoral Science Foundation

National Natural Science Foundation of China

Shandong Provincial Natural Science Foundation, China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering

Reference40 articles.

1. Solar-array-induced disturbance of the hubble space telescope pointing system;Foster;J Spacecr Rockets,1995

2. A study on composite honeycomb sandwich panel structure;He;Mater Des,2008

3. Thermally induced bending vibrations of a flexible rolled-up solar array;Thornton;J. Spacecr Rocket,1993

4. A composite control scheme for attitude maneuvering and elastic mode stabilization of flexible spacecraft with measurable output feedback;Hu;Aerosp Sci Technol,2009

5. Vibration suppression and adaptive-robust control of a smart flexible satellite with three axes maneuvering;Azadi;Acta Astronaut,2011

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