Nonlinear Stabilization of High Angle-of-Attack Flight Dynamics Using Bifurcation Control

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dc.contributor.authorAbed, Eyad H.en_US
dc.contributor.authorLee, Hsien-Chiarnen_US
dc.contributor.departmentISRen_US
dc.date.accessioned2007-05-23T09:45:30Z
dc.date.available2007-05-23T09:45:30Z
dc.date.issued1990en_US
dc.description.abstractWe consider the problem of designing stabilizing control laws for flight over a broad range of angles-of-attack which also serve to signal the pilot of impending stall. The paper employs bifurcation stabilization coupled with more traditional linear control system design. To focus the discussion, a detailed analysis is given for a model of the longitudinal dynamics of an F-8 Crusader.en_US
dc.format.extent382796 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1903/4980
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; TR 1990-32en_US
dc.subjectIntelligent Servomechanismsen_US
dc.titleNonlinear Stabilization of High Angle-of-Attack Flight Dynamics Using Bifurcation Controlen_US
dc.typeTechnical Reporten_US

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