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In-flight simulation at the NASA Dryden Flight Research FacilityAn account of the in-flight simulation at the Dryden Flight Research Facility is presented and various aircraft and tests performed are discussed. In-flight simulation has been utilized for a variety of flying quality investigations including low-lift-to-drag ratio approach characteristics for vehicles like the X-15, the lifting bodies, and the Space Shuttle. Consideration is given to the effects of time delays on controllability of aircraft with digital flight-control systems, flight control systems for such aircraft as the X-29, and the causes and cures of pilot-induced oscillation in diverse aircraft.
Document ID
19910063180
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shafer, Mary F.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 91-2916
Report Number: AIAA PAPER 91-2916
Meeting Information
Meeting: AIAA Flight Simulation Technologies Conference
Location: New Orleans, LA
Country: United States
Start Date: August 12, 1991
End Date: August 14, 1991
Accession Number
91A47803
Distribution Limits
Public
Copyright
Other

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