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In-flight simulation studies at the NASA Dryden Flight Research FacilitySince the late 1950's, the National Aeronautics and Space Administration's Dryden Flight Research Facility has found in-flight simulation to be an invaluable tool. In-flight simulation has been used to address a wide variety of flying qualities questions, including low-lift-to-drag ratio approach characteristics for vehicles like the X-15, the lifting bodies, and the Space Shuttle; the effects of time delays on controllability of aircraft with digital flight-control systems, the causes and cures of pilot-induced oscillation in a variety of aircraft, and flight-control systems for such diverse aircraft as the X-15 and the X-29. In-flight simulation has also been used to anticipate problems and to avoid them and to solve problems once they appear. Presented here is an account of the in-flight simulation at the Dryden Flight Research Facility and some discussion. An extensive bibliography is included.
Document ID
19920019867
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shafer, Mary F.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1833
NASA-TM-4396
NAS 1.15:4396
Meeting Information
Meeting: AIAA Simulation Technology Conference
Location: New Orleans, LA
Country: United States
Start Date: August 12, 1991
End Date: August 14, 1991
Accession Number
92N29110
Funding Number(s)
PROJECT: RTOP 505-64-30
Distribution Limits
Public
Copyright
Public Use Permitted.
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