Publication Date:
2014-09-25
Description:
The optimal control of structures which consist of composite materials or of perforated materials is discussed. Asymptotic formula, derived from the so-called homogenization theory, are presented which allow the replacement of very complicated problems by much simpler ones.
Keywords:
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Type:
JPL Proc. of the Workshop on Identification and Control of Flexible Space Struct., Vol. 2; p 83-100
Format:
text
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