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    Robust Flight Control Design Using Sensor-Based Backstepping Control for Unmanned Aerial Vehicles

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 006
    Author:
    Lijia Cao
    ,
    Xiaoxiang Hu
    ,
    Shengxiu Zhang
    ,
    Yunfeng Liu
    DOI: 10.1061/(ASCE)AS.1943-5525.0000783
    Publisher: American Society of Civil Engineers
    Abstract: The sensor-based backstepping control law, which is not sensitive to model uncertainty, uses less model knowledge and the measurements of state derivatives. A flight control law based on a sensor-based backstepping method for unmanned aerial vehicles (UAVs) is proposed in this paper. The nonlinear model uncertainties of a UAV and sensor noise are concerning. Moreover, command filters are used to handle dynamics and saturation effects of the actuators for carrying out the flight control law. The simulation results show the proposed flight control law can guarantee the closed-loop system stability and has better tracking control performance than the block backstepping control law with model uncertainty.
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      Robust Flight Control Design Using Sensor-Based Backstepping Control for Unmanned Aerial Vehicles

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4241964
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    contributor authorLijia Cao
    contributor authorXiaoxiang Hu
    contributor authorShengxiu Zhang
    contributor authorYunfeng Liu
    date accessioned2017-12-16T09:22:14Z
    date available2017-12-16T09:22:14Z
    date issued2017
    identifier other%28ASCE%29AS.1943-5525.0000783.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4241964
    description abstractThe sensor-based backstepping control law, which is not sensitive to model uncertainty, uses less model knowledge and the measurements of state derivatives. A flight control law based on a sensor-based backstepping method for unmanned aerial vehicles (UAVs) is proposed in this paper. The nonlinear model uncertainties of a UAV and sensor noise are concerning. Moreover, command filters are used to handle dynamics and saturation effects of the actuators for carrying out the flight control law. The simulation results show the proposed flight control law can guarantee the closed-loop system stability and has better tracking control performance than the block backstepping control law with model uncertainty.
    publisherAmerican Society of Civil Engineers
    titleRobust Flight Control Design Using Sensor-Based Backstepping Control for Unmanned Aerial Vehicles
    typeJournal Paper
    journal volume30
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000783
    treeJournal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 006
    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