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Dynamic model verification of large structural systemsThe objective of the present methodology is two-fold: (1) to process test data obtained from either modal survey tests, or slow sine-sweep tests, to extract a set of orthogonal modes best matching the test data while being commensurate with the dynamic model, and (2) to modify submatrices of the dynamic model mass and stiffness matrices to adjust the model to best fit the test data. The method has been implemented using a linear statistical sequential estimator for computation on a CDC computer. Demonstration problems involving Space Shuttle quarter-scale vibration test data and dynamic models have been run. This paper will discuss the general methodology and experience to date.
Document ID
19790041901
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lee, L. T.
(Wiggins (J. H.) Co. Redondo Beach, CA, United States)
Hasselman, T. K.
(J. H. Wiggins Co. Redondo Beach, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1978
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
SAE PAPER 781047
Report Number: SAE PAPER 781047
Meeting Information
Meeting: Society of Automotive Engineers, Aerospace Meeting
Location: San Diego, CA
Start Date: November 27, 1978
End Date: November 30, 1978
Sponsors: Society of Automotive Engineers
Accession Number
79A25914
Funding Number(s)
CONTRACT_GRANT: NAS8-31950
Distribution Limits
Public
Copyright
Other

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