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Frequency-Domain Deconvolution for Flight Dynamics ApplicationsA deconvolution method is presented for estimating input data from measured output data and a model of the dynamic process involved. The method uses an optimal Wiener filter for separating the measured data into signal and noise components, and a high-accuracy Fourier transform for inverting the model dynamics in the frequency domain. The method is an extension of optimal Fourier smoothing, and uses a technique to enhance the contrast between the signal and noise spectra in designing the Wiener filter. The deconvolution method was applied to simulation and flight test data for the purposes of removing unwanted distortions introduced by signal-conditioning filters and sensor dynamics, and for reconstructing turbulence inputs from measured sensor data. Results indicated hat the method performs well given good signal-to-noise levels and accurate models of the dynamic process.
Document ID
20190001864
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Grauer, Jared A.
(NASA Langley Research Center Hampton, VA, United States)
Boucher, Matthew J.
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
March 26, 2019
Publication Date
June 26, 2018
Subject Category
Aircraft Stability And Control
Report/Patent Number
NF1676L-28783
Report Number: NF1676L-28783
Meeting Information
Meeting: AIAA Aviation and Aeronautics Forum and Exposition
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: WBS 081876.02.07.02.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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