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Structural dynamics system model reductionLoads analysis for structural dynamic systems is usually performed by finite element models. Because of the complexity of the structural system, the model contains large number of degree-of-freedom. The large model is necessary since details of the stress, loads and responses due to mission environments are computed. However, a simplified model is needed for other tasks such as pre-test analysis for modal testing, and control-structural interaction studies. A systematic method of model reduction for modal test analysis is presented. Perhaps it will be of some help in developing a simplified model for the control studies.
Document ID
19870013294
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chen, J. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rose, T. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wada, B. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures
Subject Category
Structural Mechanics
Accession Number
87N22727
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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