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Correlation Filtering of Modal Dynamics using the Laplace WaveletWavelet analysis allows processing of transient response data commonly encountered in vibration health monitoring tasks such as aircraft flutter testing. The Laplace wavelet is formulated as an impulse response of a single mode system to be similar to data features commonly encountered in these health monitoring tasks. A correlation filtering approach is introduced using the Laplace wavelet to decompose a signal into impulse responses of single mode subsystems. Applications using responses from flutter testing of aeroelastic systems demonstrate modal parameters and stability estimates can be estimated by correlation filtering free decay data with a set of Laplace wavelets.
Document ID
19980018482
Acquisition Source
Armstrong Flight Research Center
Document Type
Contractor Report (CR)
Authors
Freudinger, Lawrence C.
(NASA Dryden Flight Research Center Edwards, CA United States)
Lind, Rick
(NASA Dryden Flight Research Center Edwards, CA United States)
Brenner, Martin J.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:207066
NASA/CR-97-207066
Report Number: NAS 1.26:207066
Report Number: NASA/CR-97-207066
Funding Number(s)
CONTRACT_GRANT: NCC4-111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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