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Cockpit simulation study of use of flight path angle for instrument approachesThe results of a piloted simulation experiment to evaluate the effect of integrating flight path angle information into a typical transport electronic attitude director indicator display format for flight director instrument landing system approaches are presented. Three electronic display formats are evaluated during 3 deg straight-in approaches with wind shear and turbulence conditions. Flight path tracking data and pilot subjective comments are analyzed with regard to the pilot's tracking performance and workload for all three display formats.
Document ID
19810015505
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hanisch, B. (Bendix Corp. Teterboro, NJ, United States)
Ernst, H. (Bendix Corp. Teterboro, NJ, United States)
Johnston, R. (Bendix Corp. Teterboro, NJ, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1981
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
FSD-7511-81-06
NASA-CR-165708
Accession Number
81N24040
Funding Number(s)
CONTRACT_GRANT: NAS1-16144
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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