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Use of Piloted Simulation for High-Angle-of-Attack Agility Research and Design Criteria DevelopmentThis paper reviews the use of piloted simulation at Langley Research Center as part of the NASA High-Angle-of-Attack Technology Program (HAATP) program to provide methods and concepts for the design of advanced fighter aircraft. A major focus of this program is to develop the design process required to fully exploit the benefits from advanced control concept for high-angle-of-attack agility. Important methodologies associated with the effective us of piloted simulation of the research are described, particularly those relating to the test techniques, validation of the test results, and design guidelines/criteria development.
Document ID
19910063214
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Marilyn E Ogburn ORCID
(Langley Research Center Hampton, Virginia, United States)
John V Foster
(Langley Research Center Hampton, Virginia, United States)
Keith D Hoffler
(ViGYAN (United States) Hampton, Virginia, United States)
Date Acquired
August 14, 2013
Publication Date
August 12, 1991
Publication Information
Publication: Flight Simulation Technologies Conference
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA-91-2954
Meeting Information
Meeting: AIAA Flight Simulation Technologies Conference
Location: New Orleans, LA
Country: US
Start Date: August 12, 1991
End Date: August 14, 1991
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
91A47837
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Angle of attack
National Aeronautics and Space Administration
Agile combat aircraft
Langley Research Center
Flight test programme
Test pilots
High performance aircraft
Cooper Harper Handling Qualities rating scale
Thrust to weight ratio
Handling qualities

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