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 |
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| container_end_page | 338 |
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| container_issue | 2 |
| container_start_page | 331 |
| container_title | AIAA journal |
| container_volume | 39 |
| creator | Ingham, Michel D Crawley, Edward F |
| description | 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. |
| doi_str_mv | 10.2514/2.1309 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0001-1452 |
| ispartof | AIAA journal, 2001-02, Vol.39 (2), p.331-338 |
| issn | 0001-1452 1533-385X |
| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid mechanics Sound Space Structural and continuum mechanics Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...) Vibrations and mechanical waves |
| title | Microdynamic Characterization of Modal Parameters for a Deployable Space Structure |
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