Integrated Control of Thermally Induced Vibration and Quasi-Static Deformation of Space Truss
Author:
Affiliation:
1. College of Aerospace Science and Engineering, National University of Defense Technology, No. 47 Yanwachi Street, Changsha 410073, China e-mail:
Abstract
Publisher
ASME International
Subject
Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering
Link
http://asmedigitalcollection.asme.org/dynamicsystems/article-pdf/doi/10.1115/1.4033407/6122080/ds_138_08_081003.pdf
Reference21 articles.
1. Johnston, J. D., and Thornton, E. A., 1996, “An Evaluation of Thermally-Induced Structural Disturbances of Spacecraft Solar Arrays,” 31st Intersociety Energy Conversion Engineering Conference, IECEC 96., IEEE, pp. 1–6.
2. Li, L., and Yuan, J., 2014, “Analysis and Modeling of Spacecraft With Flexible Solar Panel Disturbed by Thermally Induced Motion,” 33rd Chinese Control Conference (CCC), IEEE, pp. 6382–6387.
3. Coupled Thermo-Structural Analysis of an Earth Orbiting Flexible Structure,2004
4. On the Stability Problem Caused by Finite Actuator Dynamics in the Collocated Control of Large Space Structures;Int. J. Control,1985
5. Active Vibration Control With Modified Positive Position Feedback;ASME J. Dyn. Syst., Meas., Control,2009
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