'Studies in stability and control analysis of airframes having nonlinear aerodynamic characteristics'

dc.contributor.authorChristopher, P. A. T.
dc.date.accessioned2017-07-28T10:37:32Z
dc.date.available2017-07-28T10:37:32Z
dc.date.issued1966-06
dc.description.abstractThe problem of longitudinal stability and control of an airframe, having nonlinearity in its principal aerodynamic characteristics, is considered. It is shown that the equation describing the response in w, and thus the incidence, is a nonlinear differential equation of the fourth order. This equation, and its degenerate forms, is used as an example to demonstrate various nonlinear techniques and their shortcomings.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/12245
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N/AERO-171en_UK
dc.relation.ispartofseries171en_UK
dc.title'Studies in stability and control analysis of airframes having nonlinear aerodynamic characteristics'en_UK
dc.typeReporten_UK

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