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Test and analysis correlation for structural dynamic systemsActivities in modifying a structural mathematical model to correlate with its modal test results are summarized. Results from the Viking and Galileo spacecraft, and developments in the parameter estimation of structural mathematical models of large flexible structures using multiple boundary condition tests are presented.
Document ID
19860021210
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wada, B. K. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chen, J. C. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: DGLR The 2nd International Symposium on Aeroelasticity and Structural Dynamics
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86N30682
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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