DAMPING SYNTHESIS FOR A SPACECRAFT USING SUBSTRUCTURE AND COMPONENT DATA

Authors
  1. Lips, K.W.
  2. Vigneron, F.R.
Corporate Authors
Communications Research Centre, Ottawa ONT (CAN)
Abstract
The 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/subtructure level. Also, it illustrates the use of the method and the level of accuracy obtained, in a case study of the Hermes spacecraft.
Report Number
1365 —
Date of publication
15 Aug 1984
Number of Pages
88
DSTKIM No
85-00051
CANDIS No
44891
Format(s):
Hardcopy;Originator's fiche received by DSIS

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