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    On Nonlinear Dynamics and an Optimal Control Design to a Longitudinal Flight

    Source: Journal of Computational and Nonlinear Dynamics:;2008:;volume( 003 ):;issue: 001::page 11012
    Author:
    Danilo Carlos Pereira
    ,
    Fábio Roberto Chavarette
    ,
    Marat Rafikov
    ,
    José Manoel Balthazar
    DOI: 10.1115/1.2802111
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In 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.
    keyword(s): Design , Optimal control , Aircraft , Bifurcation , Flight , Nonlinear dynamics , Equilibrium (Physics) , Equations of motion AND Stability ,
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      On Nonlinear Dynamics and an Optimal Control Design to a Longitudinal Flight

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/137585
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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