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VTOL control system studies on a 6-degree-of- freedom motion simulator.Optimization of VTOL control concepts with and without stabilization compared with six degree of freedom motion simulator, noting system failure effects and nonlinear concepts
Document ID
19660061385
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fry, E. B.
Gerdes, R. M.
Gossett, T. D.
Greif, R. K.
Date Acquired
August 3, 2013
Publication Date
September 1, 1966
Subject Category
Aircraft
Report/Patent Number
ICAS PAPER 66-9
Report Number: ICAS PAPER 66-9
Accession Number
66A40675
Distribution Limits
Public
Copyright
Other
Keywords
SYSTEM FAILURE
CONTROL SIMULATOR
VTOL AIRCRAFT
NONLINEAR SYSTEM
OPTIMIZATION
DEGREE OF FREEDOM
AIRCRAFT CONTROL

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