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    Stability and Performance Analysis of Six-Rotor Unmanned Aerial Vehicles in Wind Disturbance

    Source: Journal of Computational and Nonlinear Dynamics:;2018:;volume( 013 ):;issue: 003::page 31005
    Author:
    Li, Xianying
    ,
    Zhao, Biao
    ,
    Yao, Yu
    ,
    Wu, Hongtao
    ,
    Liu, Yunping
    DOI: 10.1115/1.4038776
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of wind disturbances on the stability of six-rotor unmanned aerial vehicles (UAVs) was investigated, exploring the various disturbances in different directions. The simulation model-based Euler–Poincare equation was established to investigate the spectra of Lyapunov exponents. Next, the value of the Lyapunov exponents was used to evaluate the stability of the systems. The results obtained show that the various speeds of rotors are optimized to keep up the stability after disturbances. In addition, the flight experiment with the hitting gust has been carried out to verify the validity and accuracy of the simulation results.
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      Stability and Performance Analysis of Six-Rotor Unmanned Aerial Vehicles in Wind Disturbance

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4253720
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    contributor authorLi, Xianying
    contributor authorZhao, Biao
    contributor authorYao, Yu
    contributor authorWu, Hongtao
    contributor authorLiu, Yunping
    date accessioned2019-02-28T11:11:52Z
    date available2019-02-28T11:11:52Z
    date copyright1/10/2018 12:00:00 AM
    date issued2018
    identifier issn1555-1415
    identifier othercnd_013_03_031005.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253720
    description abstractThe effect of wind disturbances on the stability of six-rotor unmanned aerial vehicles (UAVs) was investigated, exploring the various disturbances in different directions. The simulation model-based Euler–Poincare equation was established to investigate the spectra of Lyapunov exponents. Next, the value of the Lyapunov exponents was used to evaluate the stability of the systems. The results obtained show that the various speeds of rotors are optimized to keep up the stability after disturbances. In addition, the flight experiment with the hitting gust has been carried out to verify the validity and accuracy of the simulation results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStability and Performance Analysis of Six-Rotor Unmanned Aerial Vehicles in Wind Disturbance
    typeJournal Paper
    journal volume13
    journal issue3
    journal titleJournal of Computational and Nonlinear Dynamics
    identifier doi10.1115/1.4038776
    journal fristpage31005
    journal lastpage031005-11
    treeJournal of Computational and Nonlinear Dynamics:;2018:;volume( 013 ):;issue: 003
    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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