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Generation and Calibration of Linear Models of Aircraft with Highly Coupled Aeroelastic and Flight DynamicsThis presentation is a refinement of an earlier presentation describing the methods of generating models used for designing control laws for use in vehicles with significant structural effects.
Document ID
20200000422
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Ouellette, Jeffrey (NASA Armstrong Flight Research Center Edwards, CA, United States)
Valdez, Felipe D. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
January 16, 2020
Publication Date
January 8, 2020
Subject Category
Aircraft Stability And Control
Report/Patent Number
AFRC-E-DAA-TN76537
Meeting Information
Meeting: AIAA SciTech Forum 2020
Location: Orlando, FL
Country: United States
Start Date: January 6, 2020
End Date: January 10, 2020
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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