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Vertical motion requirements for landing simulationTests were conducted to determine the significance of vertical acceleration cues in the simulation of the visual approach and landing maneuver. Landing performance measures were obtained for four subject pilots operating a visual landing simulation device which provides up to plus or minus 40 feet of vertical motion. Test results indicate that vertical motion cues are utilized in the landing task, and that they are particularly important in the simulation of aircraft with marginal longitudinal handling qualities. To assure vertical motion cues of the desired fidelity in the landing tasks, it appears that a simulator must have excursion capabilities of at least plus or minus 20 feet.
Document ID
19730008293
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bray, R. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62236
Report Number: NASA-TM-X-62236
Accession Number
73N17020
Funding Number(s)
PROJECT: RTOP 760-74-04-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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