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Effect of vertical active vibration isolation on tracking performance and on ride qualitiesAn investigation to determine the effect on pilot performance and comfort of an active vibration isolation system for a commercial transport pilot seat is reported. The test setup consisted of: a hydraulic shaker which produced random vertical vibration inputs; the active vibration isolation system; the pilot seat; the pilot control wheel and column; the side-arm controller; and a two-axis compensatory tracking task. The effects of various degrees of pilot isolation on short-term (two-minute) tracking performance and comfort were determined.
Document ID
19730003382
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dimasi, F. P.
(Barry Wright Corp. Watertown, MA, United States)
Allen, R. E.
(Barry Wright Corp. Watertown, MA, United States)
Calcaterra, P. C.
(Barry Wright Corp. Watertown, MA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Publication Information
Publisher: NASA
Subject Category
Biotechnology
Report/Patent Number
NASA-CR-2146
Report Number: NASA-CR-2146
Accession Number
73N12109
Funding Number(s)
PROJECT: RTOP 133-61-13-02
CONTRACT_GRANT: NAS1-9919
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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