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Effects of Coupling Between Pitch and Roll Control Inputs on the Handling Qualities of VTOL AircraftEffects of coupling between pitch and roll control inputs on handling qualities of vtol aircraft
Document ID
19620000276
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Garren, J. F., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
March 1, 1962
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-1233
Report Number: NASA-TN-D-1233
Accession Number
62N10276
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
PITCHING MOMENT
ROLL
CROSS COUPLING
VTOL AIRCRAFT

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