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Vibration Control of Deployable Astromast Boom: Preliminary ExperimentsThis paper deals with the dynamic characterization of a flexible aerospace solar boom. The modeling issues and sine dwell vibration testing to determine natural frequencies and mode shapes of a continuous-longer on deployable ASTROMAST lattice boom are discussed. The details of the proof-of-concept piezoelectric active vibration experiments on a simple cantilever beam to control its vibrations are presented. The control parameters like voltage to the controller crystal and its location are investigated, to determine the effectiveness of control element to suppress selected resonant vibrations of the test specimen. Details of this experiment and plans for its future adaptation to the prototype structure are also discussed.
Document ID
19960021772
Document Type
Conference Paper
Authors
Swaminadham, M.
(Texas A&M Univ. College Station, TX United States)
Hamilton, David A.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1994
Publication Information
Publication: Dual-Use Space Technology Transfer Conference and Exhibition
Volume: 1
Subject Category
Structural Mechanics
Accession Number
96N25047
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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