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http://dx.doi.org/10.20910/JASE.2018.12.6.50

Optimal Design of a Composite Solar Panel for Vibration Suppression  

Kim, Yongha (Graduate School of Aerospace and Mechanical Engineering, Korea Aerospace University)
Kim, Hiyeop (Graduate School of Aerospace and Mechanical Engineering, Korea Aerospace University)
Park, Jungsun (Department of Aerospace and Mechanical Engineering, Korea Aerospace University)
Publication Information
Journal of Aerospace System Engineering / v.12, no.6, 2018 , pp. 50-57 More about this Journal
Abstract
This paper proposes the use of supports as passive vibration absorber to a composite solar panel for a high-agility satellite. We further defined the dynamic model of the composite solar panel with the help of the Ritz method and verified vibration suppression performance of the support by performing vibration analysis. Finally, this research ensures optimal design of the composite solar panel with the support for maximizing vibration suppression performance in limited mass. The proposed results of the optimal design can be applied in actual structural design of satellites.
Keywords
Composite Solar Panel; High-Agility Satellite; Vibration Suppression; Ritz Method; Optimal Design;
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Times Cited By KSCI : 1  (Citation Analysis)
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1 P. S. Thomas, and J. L. Wiley, Spacecraft Structures and Mechanisms From Concept to Launch, Space Technology Library, 1995.
2 J. H. Lim, "Recent Trend of the Configuration Design of High Resolution Earth Observation Satellites," Current Industrial and Technological Trends in Aerospace, vol. 8, pp. 45-54, 2010.
3 R. G. Ross, "Vibration suppression of advanced space cryocoolers - an overview", International Society of Optical Engineering (SPIE) Smart Structures and Materials Conference, 2003.
4 C. D. Johnson, "Design and Application of Passive Vibration Suppression", Technology Overview 2001 International Symposium on Smart Structures and Materials, 2001.
5 K. J. Pendergast, and C. J. Schauwecker, "Use of a passive reaction wheel jitter isolation system to meet the Advanced X-ray Astrophysics Facility imaging performance requirements", International Society of Optical Engineering Conference on Space Telescoped and Instruments, 1998.
6 K. Shirey, S. Banks, R. Boyle, and R. Unger, "Design and Qualification of the Ams-02 Flight Cryocoolers", Space Cryogenics Workshop, 2005.
7 E. H. Anderson, M. E. Evert, and R. M. Glasese, "Satellite ultraquiet isolation technology experiment (SUITE): Electro-mechanical subsystems", International Society for Optical Engineering, no. 3674-36, pp. 308-328, 1995.
8 S. W. Kim, W. G. Kim, Y. W. You, J. H. Lim, and H. S. Kim, "Structural Analysis of Solar Array Panel for Highly Agile Satellite", Proceeding of the 2013 KSAS Fall Conference, pp. 649-652, 2013.
9 Z. Bai, Y. Zhao, W. Ma, and H. Tian, "Modal Analysis for Small Satellite System with Finite Element Method," 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, pp. 1-5, 2008.
10 J. H. Holland, Adaptation in Natural and Artificial System, University of Michigan Press, 1975.
11 Gordberg, Genetic Algorithms in Search, Optimization, and Machine Learning, Pearson Education, 2013.
12 Y. H. Kim, P. H. Kim, H. Y. Kim, and J. S. Park, "Optimal Design of a Composite Lattice Rectangular Plate for Solar Panels of a High-Agility Satellite," International Journal of Aeronautical and Space Sciences, vol. 19, no. 3, pp. 762-775, 2018.   DOI