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Comparison of a linear and a nonlinear washout for motion simulators utilizing objective and subjective data from CTOL transport landing approachesObjective and subjective data gathered in the processes of comparing a linear and a nonlinear washout for motion simulators reveal that there is no difference in the pilot performance measurements used during instrument landing system (ILS) approaches with a Boeing 737 conventional takeoff and landing (CTOL) airplane between fixed base, linear washout, and nonlinear washout operations. However, the subjective opinions of the pilots reveal an important advance in motion cue presentation. The advance is not in the increased cue available over a linear filter for the same amount of motion base travel but rather in the elimination of false rotational rate cues presented by linear filters.
Document ID
19760019106
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.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-10593
NASA-TN-D-8157
Report Number: L-10593
Report Number: NASA-TN-D-8157
Accession Number
76N26194
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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