Thermal-structural analysis for flexible spacecraft with single or double solar panels: A comparison study-Reference-Cited by-同舟云学术

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Thermal-structural analysis for flexible spacecraft with single or double solar panels: A comparison study

Published:2019-01 Issue: Volume:154 Page:33-43
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Liu Lun,Sun Shupeng,Cao Dengqing,Liu Xiyu

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Shandong Provincial Natural Science Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

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

2. Dynamic modeling for a flexible spacecraft with solar arrays composed of honeycomb panels and its proportional-derivative control with input shaper;Liu;ASME J. Dyn. Syst., Meas. Contr.,2016

3. Dynamic modeling and simulation for flexible spacecraft with flexible jointed solar panels;Wei;Int. J. Mech. Sci.,2017

4. Adaptive variable structure and commanding shaped vibration control of flexible spacecraft;Hu;J. Guid. Contr. Dynam.,2007

5. Experimental study and numerical simulation of active vibration control of a highly flexible beam using piezoelectric intelligent material;Wu;Aero. Sci. Technol.,2014

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