Microdynamic Characterization of Modal Parameters for a Deployable Space Structure

Results are presented from an experimental investigation of the microdynamics of deployable space structures. The dynamic response of a representative deployable truss at submicrostrain levels of vibration was chacterized in terms of modal parameters.

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Veröffentlicht in:AIAA journal 2001-02, Vol.39 (2), p.331-338
Hauptverfasser: Ingham, Michel D, Crawley, Edward F
Format: Artikel
Sprache:eng
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Zusammenfassung:Results are presented from an experimental investigation of the microdynamics of deployable space structures. The dynamic response of a representative deployable truss at submicrostrain levels of vibration was chacterized in terms of modal parameters.
ISSN:0001-1452
1533-385X
DOI:10.2514/2.1309