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contributor authorDanilo Carlos Pereira
contributor authorFábio Roberto Chavarette
contributor authorMarat Rafikov
contributor authorJosé Manoel Balthazar
date accessioned2017-05-09T00:27:13Z
date available2017-05-09T00:27:13Z
date copyrightJanuary, 2008
date issued2008
identifier issn1555-1415
identifier otherJCNDDM-25643#011012_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137585
description abstractIn this work, we analyzed a bifurcational behavior of a longitudinal flight nonlinear dynamics, taking as an example the F-8 aircraft “Crusader.” We deal with an analysis of high angles of attack in order to stabilize the oscillations; those were close to the critical angle of the aircraft, in the flight conditions, established. We proposed a linear optimal control design applied to the considered nonlinear aircraft model below angle of stall, taking into account regions of Hopf and saddled noddle bifurcations.
publisherThe American Society of Mechanical Engineers (ASME)
titleOn Nonlinear Dynamics and an Optimal Control Design to a Longitudinal Flight
typeJournal Paper
journal volume3
journal issue1
journal titleJournal of Computational and Nonlinear Dynamics
identifier doi10.1115/1.2802111
journal fristpage11012
identifier eissn1555-1423
keywordsDesign
keywordsOptimal control
keywordsAircraft
keywordsBifurcation
keywordsFlight
keywordsNonlinear dynamics
keywordsEquilibrium (Physics)
keywordsEquations of motion AND Stability
treeJournal of Computational and Nonlinear Dynamics:;2008:;volume( 003 ):;issue: 001
contenttypeFulltext


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