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Aircraft Dynamic Modeling in TurbulenceA method for accurately identifying aircraft dynamic models in turbulence was developed and demonstrated. The method uses orthogonal optimized multisine excitation inputs and an analytic method for enhancing signal-to-noise ratio for dynamic modeling in turbulence. A turbulence metric was developed to accurately characterize the turbulence level using flight measurements. The modeling technique was demonstrated in simulation, then applied to a subscale twin-engine jet transport aircraft in flight. Comparisons of modeling results obtained in turbulent air to results obtained in smooth air were used to demonstrate the effectiveness of the approach.
Document ID
20120014567
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Morelli, Eugene A.
(NASA Langley Research Center Hampton, VA, United States)
Cunninham, Kevin
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 26, 2013
Publication Date
August 13, 2012
Subject Category
Aircraft Stability And Control
Report/Patent Number
NF1676L-14085
Report Number: NF1676L-14085
Meeting Information
Meeting: 2012 AIAA Guidance, Navigation, and Control Conference
Location: Minneapolis, MN
Country: United States
Start Date: August 13, 2012
End Date: August 16, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 284848.02.05.07.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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