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Expansion of flight simulator capability for study and solution of aircraft directional control problems on runwaysThe development, evaluation, and evaluation results of a DC-9-10 runway directional control simulator are described. An existing wide bodied flight simulator was modified to this aircraft configuration. The simulator was structured to use either two of antiskid simulations; (1) an analog mechanization that used aircraft hardware; or (2) a digital software simulation. After the simulation was developed it was evaluated by 14 pilots who made 818 simulated flights. These evaluations involved landings, rejected takeoffs, and various ground maneuvers. Qualitatively most pilots evaluated the simulator as realistic with good potential especially for pilot training for adverse runway conditions.
Document ID
19780012175
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kibbee, G. W.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-2970
MDC-J7727
Report Number: NASA-CR-2970
Report Number: MDC-J7727
Accession Number
78N20118
Funding Number(s)
CONTRACT_GRANT: NAS1-13981
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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