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Motion/visual cueing requirements for vortex encounters during simulated transport visual approach and landingThis paper addresses the issues of motion/visual cueing fidelity requirements for vortex encounters during simulated transport visual approaches and landings. Four simulator configurations were utilized to provide objective performance measures during simulated vortex penetrations, and subjective comments from pilots were collected. The configurations used were as follows: fixed base with visual degradation (delay), fixed base with no visual degradation, moving base with visual degradation (delay), and moving base with no visual degradation. The statistical comparisons of the objective measures and the subjective pilot opinions indicated that although both minimum visual delay and motion cueing are recommended for the vortex penetration task, the visual-scene delay characteristics were not as significant a fidelity factor as was the presence of motion cues. However, this indication was applicable to a restricted task, and to transport aircraft. Although they were statistically significant, the effects of visual delay and motion cueing on the touchdown-related measures were considered to be of no practical consequence.
Document ID
19830013921
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Parrish, R. V.
(NASA Langley Research Center Hampton, VA, United States)
Bowles, R. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-15544
NAS 1.60:2136
NASA-TP-2136
Report Number: L-15544
Report Number: NAS 1.60:2136
Report Number: NASA-TP-2136
Accession Number
83N22192
Funding Number(s)
PROJECT: RTOP 505-35-33-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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