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Real-Time Global Nonlinear Aerodynamic Modeling for Learn-To-FlyFlight testing and modeling techniques were developed to accurately identify global nonlinear aerodynamic models for aircraft in real time. The techniques were developed and demonstrated during flight testing of a remotely-piloted subscale propeller-driven fixed-wing aircraft using flight test maneuvers designed to simulate a Learn-To-Fly scenario. Prediction testing was used to evaluate the quality of the global models identified in real time. The real-time global nonlinear aerodynamic modeling algorithm will be integrated and further tested with learning adaptive control and guidance for NASA Learn-To-Fly concept flight demonstrations.
Document ID
20160007737
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-21688
Report Number: NF1676L-21688
Meeting Information
Meeting: 2016 AIAA SciTech Conference
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.
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