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System identification using modal residues and rootsThis presentation will address an approach for using modal residues and roots, typically derived from vibration testing, to solve for the lumped parameters of a finite element model. The uniqueness of the approach is that the mass, stiffness, or damping matrices of a structure do not need to be known or estimated a-priori. Instead just the connectivity of the structure needs to be estimated. In addition, the presentation will demonstrate how models with orders larger than the number of modes obtained by the test program can be solved. The presentation will start by covering the basis of the approach, then illustrate a trivial application of how it works, and finally illustrate its use on a cantilevered beam using only a fraction of the mode to solve the mass, stiffness, and damping matrices.
Document ID
19930075334
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wendler, Bruce H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1988
Publication Information
Publication: JPL, Model Determination for Large Space Systems Workshop, Volume 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N72781
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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