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Models of subjective response to in-flight motion dataMathematical relationships between subjective comfort and environmental variables in an air transportation system are investigated. As a first step in model building, only the motion variables are incorporated and sensitivities are obtained using stepwise multiple regression analysis. The data for these models have been collected from commercial passenger flights. Two models are considered. In the first, subjective comfort is assumed to depend on rms values of the six-degrees-of-freedom accelerations. The second assumes a Rustenburg type human response function in obtaining frequency weighted rms accelerations, which are used in a linear model. The form of the human response function is examined and the results yield a human response weighting function for different degrees of freedom.
Document ID
19750002636
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rudrapatna, A. N.
(Virginia Univ. Charlottesville, VA, United States)
Jacobson, I. D.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1973
Subject Category
Man/System Technology And Life Support
Report/Patent Number
TR-403209
NASA-CR-140675
Report Number: TR-403209
Report Number: NASA-CR-140675
Accession Number
75N10708
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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