NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Dynamic Modeling from Flight Data with Unknown Time SkewsA method for estimating dynamic model parameters from flight data with unknown time skews is described and demonstrated. The method combines data reconstruction, nonlinear optimization, and equation-error parameter estimation in the frequency domain to accurately estimate both dynamic model parameters and the relative time skews in the data. Data from a nonlinear F-16 aircraft simulation with realistic noise, instrumentation errors, and arbitrary time skews were used to demonstrate the approach. The approach was further evaluated using flight data from a subscale jet transport aircraft, where the measured data were known to have relative time skews. Comparison of modeling results obtained from time-skewed and time-synchronized data showed that the method accurately estimates both dynamic model parameters and relative time skew parameters from flight data with unknown time skews.
Document ID
20160007723
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Morelli, Eugene A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 20, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Stability And Control
Report/Patent Number
NF1676L-21730
Report Number: NF1676L-21730
Meeting Information
Meeting: 2016 AIAA SciTech Forum and Exposition
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 109492.02.07.02.10.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available