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Study of modal coupling procedures for the shuttle: A matrix method for damping synthesisThe damping method was applied successfully to real structures as well as analytical models. It depends on the ability to determine an appropriate modal damping matrix for each substructure. In the past, modal damping matrices were assumed diagonal for lack of being able to determine the coupling terms which are significant in the general case of nonproportional damping. This problem was overcome by formulating the damped equations of motion as a linear perturbation of the undamped equations for light structural damping. Damped modes are defined as complex vectors derived from the complex frequency response vectors of each substructure and are obtained directly from sinusoidal vibration tests. The damped modes are used to compute first order approximations to the modal damping matrices. The perturbation approach avoids ever having to solve a complex eigenvalue problem.
Document ID
19750002910
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hasselman, T. K.
(TRW Systems Group Redondo Beach, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1972
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
TRW-18058-6001-RU-00
NASA-CR-112253
MEL-72-D-44
Report Number: TRW-18058-6001-RU-00
Report Number: NASA-CR-112253
Report Number: MEL-72-D-44
Accession Number
75N10982
Funding Number(s)
CONTRACT_GRANT: NAS1-10635
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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