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The influence of response feedback loops on the lateral-directional dynamics of a variable-stability transport aircraftResponse feedback control loops effects on lateral-directional dynamics of variable stability transport aircraft
Document ID
19670017216
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Szalai, K. J. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3966
Accession Number
67N26545
Funding Number(s)
CONTRACT_GRANT: 720-04-00-01-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRANSPORT AIRCRAFT
AERODYNAMIC STABILITY
FEEDBACK CONTROL SYSTEM
DYNAMICS

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