NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Passenger ride quality response to an airborne simulator environmentThe present study was done aboard a special aircraft able to effect translations through the center of gravity with a minimum of pitch and roll. The aircraft was driven through controlled motions by an on-board analog computer. The input signal was selectively filtered Gaussian noise whose power spectra approximated that of natural turbulence. This input, combined with the maneuvering capabilities of this aircraft, resulted in an extremely realistic simulation of turbulent flight. The test flights also included varying bank angles during turns. Subjects were chosen from among NASA Flight Research Center personnel. They were all volunteers, were given physical examinations, and were queried about their attitudes toward flying before final selection. In profile, they were representative of the general flying public. Data from this study include (1) a basis for comparison with previous commercial flights, that is, motion dominated by vertical acceleration, (2) extension to motion dominated by lateral acceleration, and (3) evaluation of various bank angles.
Document ID
19760009682
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wolf, T. D.
(NASA Flight Research Center Edwards, CA, United States)
Rezek, T. W.
(NASA Flight Research Center Edwards, CA, United States)
Gee, S. W.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 8, 2013
Publication Date
November 1, 1975
Publication Information
Publication: The 1975 Ride Quality Symp.
Subject Category
Behavioral Sciences
Accession Number
76N16770
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available