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    Nonlinear Control of a Quadrotor With Deviated Center of Gravity

    Source: Journal of Dynamic Systems, Measurement, and Control:;2017:;volume( 139 ):;issue: 001::page 11003
    Author:
    Xian, Bin
    ,
    Zhao, Bo
    ,
    Zhang, Yao
    ,
    Zhang, Xu
    DOI: 10.1115/1.4034366
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, a new adaptive tracking controller is developed for a quadrotor unmanned aerial vehicle (UAV) via immersion and invariance (I&I) approach. The controller is able to compensate parametric uncertainties such as the unmeasurable effects of the deviated center-of-gravity (CoG), as well as the aerodynamic coefficients. The globally asymptotic tracking of the desired attitude trajectories is proven via the Lyapunov-based stability analysis and LaSalle's invariance theorem. Real-time experiment results performed on a quadrotor attitude control testbed are given to show the good control performance of the proposed scheme.
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      Nonlinear Control of a Quadrotor With Deviated Center of Gravity

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4236561
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    contributor authorXian, Bin
    contributor authorZhao, Bo
    contributor authorZhang, Yao
    contributor authorZhang, Xu
    date accessioned2017-11-25T07:20:36Z
    date available2017-11-25T07:20:36Z
    date copyright2016/9/9
    date issued2017
    identifier issn0022-0434
    identifier otherds_139_01_011003.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4236561
    description abstractIn this paper, a new adaptive tracking controller is developed for a quadrotor unmanned aerial vehicle (UAV) via immersion and invariance (I&I) approach. The controller is able to compensate parametric uncertainties such as the unmeasurable effects of the deviated center-of-gravity (CoG), as well as the aerodynamic coefficients. The globally asymptotic tracking of the desired attitude trajectories is proven via the Lyapunov-based stability analysis and LaSalle's invariance theorem. Real-time experiment results performed on a quadrotor attitude control testbed are given to show the good control performance of the proposed scheme.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNonlinear Control of a Quadrotor With Deviated Center of Gravity
    typeJournal Paper
    journal volume139
    journal issue1
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.4034366
    journal fristpage11003
    journal lastpage011003-8
    treeJournal of Dynamic Systems, Measurement, and Control:;2017:;volume( 139 ):;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
    yabeshDSpacePersian