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A describing-function analysis of the stability of a launch vehicle with nonlinear thrust vectoringDescribing-function analysis of launch vehicle stability with nonlinear thrust vectoring
Document ID
19650026236
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Lester, H. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3064
Accession Number
65N35837
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LAUNCH VEHICLE
STABILITY AND CONTROL
AERODYNAMIC STABILITY
NONLINEAR SYSTEM

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