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Application of approach speed criteria derived from closed-loop pilot-vehicle systems analyses to an Ogee wing aircraftApproach speed criteria derived from closed loop pilot-vehicle systems analyses and applied to Ogee wing F-5 aircraft
Document ID
19660026368
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wasicko, R. J. (Systems Technology, Inc. Hawthorne, CA, United States)
Date Acquired
August 3, 2013
Publication Date
September 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-CR-579
Report Number: NASA-CR-579
Accession Number
66N35658
Funding Number(s)
CONTRACT_GRANT: NAS2-1868
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
OGEE WING
APPROACH AND LANDING
CLOSED LOOP SYSTEM
F-5 AIRCRAFT
MAN-MACHINE SYSTEM
PILOTED AIRCRAFT

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