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  • SPACECRAFT DESIGN, TESTING AND PERFORMANCE  (1)
  • 1
    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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