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Evaluation of a linear washout for simulator motion cue presentation during landing approachThe comparison of a fixed-base versus a five-degree-of-freedom motion base simulation of a 737 conventional take-off and landing (CTOL) aircraft performing instrument landing system (ILS) landing approaches was used to evaluate a linear motion washout technique. The fact that the pilots felt that the addition of motion increased the pilot workload and this increase was not reflected in the objective data results, indicates that motion cues, as presented, are not a contributing factor to root-mean-square (rms) performance during the landing approach task. Subjective results from standard maneuvering about straight-and-level flight for specific motion cue evaluation revealed that the longitudinal channels (pitch and surge) possibly the yaw channel produce acceptable motions. The roll cue representation, involving both roll and sway channels, was found to be inadequate for large roll inputs, as used for example, in turn entries.
Document ID
19750024959
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Parrish, R. V.
(NASA Langley Research Center Hampton, VA, United States)
Martin, D. J., Jr.
(Electronic Assoc., Inc., Hampton Va., United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-9984
NASA-TN-D-8036
Report Number: L-9984
Report Number: NASA-TN-D-8036
Accession Number
75N33032
Funding Number(s)
PROJECT: RTOP 504-09-41-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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