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Effects of aircraft design on STOL ride quality: A simulator studyTo improve the ride quality in short takeoff aircraft, several means have been investigated. In general, these methods consist of placing sensors in the aircraft which sense aircraft motion, usually linear accelerations and angular rates. These signals are then used to deflect control surfaces which generate aerodynamic forces and moments which tend to minimize the motion which the passenger feels. One of the disadvantages of some of these systems is that they may tend to degrade the handling qualities or controllability of the airplane, making it more difficult or annoying for the pilot to fly. Rather than using active control systems to control ride quality, one might possibly design aircraft so that they are inherently pleasant to ride. The purpose of this study is to determine the relationship between characteristic aircraft motions and aircraft ride quality.
Document ID
19740024330
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jacobson, I. D.
(Virginia Univ. Charlottesville, VA, United States)
Jones, C. R.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Aircraft
Report/Patent Number
NASA-CR-140059
ESS-4035-102-74
MEMO-403502
Report Number: NASA-CR-140059
Report Number: ESS-4035-102-74
Report Number: MEMO-403502
Accession Number
74N32443
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-208
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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