Multi-objective topology optimization to reduce vibration of micro-satellite primary supporting structure
Author:
Publisher
JVE International Ltd.
Subject
Mechanical Engineering,General Materials Science
Link
http://www.jvejournals.com/Vibro/fulltextpdf/JVE-17517.pdf
Reference22 articles.
1. Johnson C. D. Protecting satellites from the dynamics of the launch environment. AIAA-2003-6266, 2003.
2. Johnson Conor D., Wilke Paul S. Protecting satellites from the dynamics of the launch environment. SPC & LPV Dynamics Environments Workshop, 2004.
3. Bronowicki A. J. Vibration isolator for large space telescope. AIAA Journal of Spacecraft and Rockets, 2005.
4. Kaj Lundadhl, von Scheele Fredrik Swedish small satellites. Technovation, Vol. 2, Issue 3, 2000, p. 287-297.
5. Wei L., Jin G., Xie X. G. Optimized design and test for primary load-bearing structure of earth observation micro-satellite. Optics and Precision Engineering, Vol. 23, Issue 11, 2015, p. 3183-3191.
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