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Practical Aspects of the Frequency Domain Approach for Aircraft System IdentificationPractical aspects of the frequency-domain approach for aircraft system identification are explained and demonstrated. Topics related to experiment design, flight data analysis, and dynamic modeling are included. For demonstration purposes, simulated time series data and simulated flight data from an F-16 nonlinear simulation with realistic noise are used. This approach enables detailed evaluations of the techniques and results, because the true characteristics of the data and aircraft dynamics are known for the simulated data. Analytical techniques and practical considerations are examined for the finite Fourier transform, nonparametric frequency response estimation, parametric modeling in the frequency domain, experiment design for frequency-domain modeling, data analysis and modeling in the frequency domain, and real-time calculations. Flight data from a subscale jet transport aircraft are used to demonstrate some of the techniques and technical issues.
Document ID
20190001862
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Morelli, Eugene A.
(NASA Langley Research Center Hampton, VA, United States)
Grauer, Jared A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
March 26, 2019
Publication Date
June 8, 2018
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-28745
Report Number: NF1676L-28745
Meeting Information
Meeting: AIAA Aviation Forum 2018
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 109492.02.07.02.10.05
Distribution Limits
Public
Copyright
Public Use Permitted.
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