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Comparison of two head-up displays in simulated standard and noise abatement night visual approachesSituation and command head-up displays were evaluated for both standard and two segment noise abatement night visual approaches in a fixed base simulation of a DC-8 transport aircraft. The situation display provided glide slope and pitch attitude information. The command display provided glide slope information and flight path commands to capture a 3 deg glide slope. Landing approaches were flown in both zero wind and wind shear conditions. For both standard and noise abatement approaches, the situation display provided greater glidepath accuracy in the initial phase of the landing approaches, whereas the command display was more effective in the final approach phase. Glidepath accuracy was greater for the standard approaches than for the noise abatement approaches in all phases of the landing approach. Most of the pilots preferred the command display and the standard approach. Substantial agreement was found between each pilot's judgment of his performance and his actual performance.
Document ID
19750018923
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cronn, F.
(San Jose State Univ. Moffett Field, CA, United States)
Palmer, E. A., III
(NASA Ames Research Center)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-3264
A-5993
Report Number: NASA-TM-X-3264
Report Number: A-5993
Accession Number
75N26995
Funding Number(s)
PROJECT: RTOP 504-09-33
CONTRACT_GRANT: NGL-05-046-002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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