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Damping synthesis for a spacecraft using substructure and component data / by K.W. Lips and F.R. Vigneron.: Co24-3/7-1365-1984E-PDF

"This report demonstrates a method for the synthesis of modal damping factors and other modal data for a spacecraft in orbit, based on input information at the component/substructure level. Also, it illustrates the use of the method and the level of accuracy obtained, in a case study of the Hermes spacecraft"--Abstract, page i.

Permanent link to this Catalogue record:
publications.gc.ca/pub?id=9.895028&sl=0

Publication information
Department/Agency
  • Communications Research Centre (Canada), issuing body.
TitleDamping synthesis for a spacecraft using substructure and component data / by K.W. Lips and F.R. Vigneron.
Series title
  • CRC report ; no. 1365
Publication typeMonograph - View Master Record
Language[English]
FormatDigital text
Electronic document
Note(s)
  • "Space Technology and Applications Branch."
  • Digitized edition from print [produced by Innovation, Science and Economic Development Canada].
  • Some pages rotated in this copy.
  • Includes bibliographical references (pages 55-58).
  • Issued also in print format.
Publishing information
  • Ottawa : Communications Research Centre, August 1984.
Author / Contributor
  • Lips, Kenneth Wayne, 1944- author.
Description1 online resource (xv, 72 pages) : illustrations.
Catalogue number
  • Co24-3/7-1365-1984E-PDF
Subject terms
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