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Turbulence flight director analysis and preliminary simulationA control column and trottle flight director display system is synthesized for use during flight through severe turbulence. The column system is designed to minimize airspeed excursions without overdriving attitude. The throttle system is designed to augment the airspeed regulation and provide an indication of the trim thrust required for any desired flight path angle. Together they form an energy management system to provide harmonious display indications of current aircraft motions and required corrective action, minimize gust upset tendencies, minimize unsafe aircraft excursions, and maintain satisfactory ride qualities. A preliminary fixed-base piloted simulation verified the analysis and provided a shakedown for a more sophisticated moving-base simulation to be accomplished next. This preliminary simulation utilized a flight scenario concept combining piloting tasks, random turbulence, and discrete gusts to create a high but realistic pilot workload conducive to pilot error and potential upset. The turbulence director (energy management) system significantly reduced pilot workload and minimized unsafe aircraft excursions.
Document ID
19740025332
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Johnson, D. E.
(Systems Technology, Inc. Hawthorne, CA, United States)
Klein, R. E.
(Systems Technology, Inc. Hawthorne, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Aircraft
Report/Patent Number
NASA-CR-140487
ITR-1003-2
Report Number: NASA-CR-140487
Report Number: ITR-1003-2
Accession Number
74N33445
Funding Number(s)
CONTRACT_GRANT: NASW-2118
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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