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Design of a digital ride quality augmentation system for commuter aircraftCommuter aircraft typically have low wing loadings, and fly at low altitudes, and so they are susceptible to undesirable accelerations caused by random atmospheric turbulence. Larger commercial aircraft typically have higher wing loadings and fly at altitudes where the turbulence level is lower, and so they provide smoother rides. This project was initiated based on the goal of making the ride of the commuter aircraft as smooth as the ride experienced on the major commercial airliners. The objectives of this project were to design a digital, longitudinal mode ride quality augmentation system (RQAS) for a commuter aircraft, and to investigate the effect of selected parameters on those designs.
Document ID
19850001730
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hammond, T. A.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Amin, S. P.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Paduano, J. D.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Downing, D. R.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-172419
NAS 1.26:172419
Accession Number
85N10037
Funding Number(s)
PROJECT: RTOP 505-45-43-02
CONTRACT_GRANT: NAG1-345
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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