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Wavelet Analyses of F/A-18 Aeroelastic and Aeroservoelastic Flight Test DataTime-frequency signal representations combined with subspace identification methods were used to analyze aeroelastic flight data from the F/A-18 Systems Research Aircraft (SRA) and aeroservoelastic data from the F/A-18 High Alpha Research Vehicle (HARV). The F/A-18 SRA data were produced from a wingtip excitation system that generated linear frequency chirps and logarithmic sweeps. HARV data were acquired from digital Schroeder-phased and sinc pulse excitation signals to actuator commands. Nondilated continuous Morlet wavelets implemented as a filter bank were chosen for the time-frequency analysis to eliminate phase distortion as it occurs with sliding window discrete Fourier transform techniques. Wavelet coefficients were filtered to reduce effects of noise and nonlinear distortions identically in all inputs and outputs. Cleaned reconstructed time domain signals were used to compute improved transfer functions. Time and frequency domain subspace identification methods were applied to enhanced reconstructed time domain data and improved transfer functions, respectively. Time domain subspace performed poorly, even with the enhanced data, compared with frequency domain techniques. A frequency domain subspace method is shown to produce better results with the data processed using the Morlet time-frequency technique.
Document ID
19970016826
Acquisition Source
Armstrong Flight Research Center
Document Type
Technical Memorandum (TM)
Authors
Martin J Brenner
(Armstrong Flight Research Center Rosamond, California, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-4793
NAS 1.15:4793
H-2164
Report Number: NASA-TM-4793
Report Number: NAS 1.15:4793
Report Number: H-2164
Meeting Information
Meeting: Structure, Structural Dynamics and Materials Conference Exhibit
Location: Kissimmee, FL
Country: US
Start Date: April 7, 1997
End Date: April 10, 1997
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
97N19223
Funding Number(s)
PROJECT: RTOP 522-32-34
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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