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USE OF THE VARIABLE STABILITY AND CONTROL X-14A TO DETERMINE ATTITUDE CONTROL POWER AND DAMPING REQUIREMENTS FOR A VISUAL HOVERING TASK IN A VTOL AIRCRAFTControl power and damping requirements for visual hovering tasks in vtol aircraft-bell x-14 testing
Document ID
19620002530
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Drinkwater, F. J., III (NASA Ames Research Center Moffett Field, CA, United States)
Rolls, L. S. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1962
Subject Category
Space Vehicles
Accession Number
62N12530
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DAMPING
STABILITY AND CONTROL
FLIGHT SIMULATOR
VISUAL FLIGHT
X-14 AIRCRAFT
CONTROL
VTOL AIRCRAFT
HOVERING
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