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    The Control of Fixed-Time Trajectory Tracking for Stratospheric Airships with System Uncertainties and External Disturbances

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006::page 04024078-1
    Author:
    Deping He
    ,
    Zhibin Li
    ,
    Xiangrui Meng
    DOI: 10.1061/JAEEEZ.ASENG-5652
    Publisher: American Society of Civil Engineers
    Abstract: In this study, we address the trajectory tracking control problem for stratospheric airships, characterized by parameter uncertainties and external disturbances. Initially, a mathematical model of the airship is constructed, from which a trajectory tracking error model is derived. Subsequently, a novel sliding mode control law is formulated to enhance control accuracy and accelerate the convergence rate of the sliding mode. Furthermore, radial basis function neural networks are utilized to estimate and compensate for uncertain system parameters and external disturbances, significantly improving the system’s robustness. Lastly, the application of Lyapunov’s theory verifies the fixed-time stability of the closed-loop system and ensures the convergence of trajectory tracking error to a near-zero vicinity within fixed time. Simulation results strongly support the efficacy of the proposed control strategy.
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      The Control of Fixed-Time Trajectory Tracking for Stratospheric Airships with System Uncertainties and External Disturbances

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4298582
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    contributor authorDeping He
    contributor authorZhibin Li
    contributor authorXiangrui Meng
    date accessioned2024-12-24T10:15:25Z
    date available2024-12-24T10:15:25Z
    date copyright11/1/2024 12:00:00 AM
    date issued2024
    identifier otherJAEEEZ.ASENG-5652.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4298582
    description abstractIn this study, we address the trajectory tracking control problem for stratospheric airships, characterized by parameter uncertainties and external disturbances. Initially, a mathematical model of the airship is constructed, from which a trajectory tracking error model is derived. Subsequently, a novel sliding mode control law is formulated to enhance control accuracy and accelerate the convergence rate of the sliding mode. Furthermore, radial basis function neural networks are utilized to estimate and compensate for uncertain system parameters and external disturbances, significantly improving the system’s robustness. Lastly, the application of Lyapunov’s theory verifies the fixed-time stability of the closed-loop system and ensures the convergence of trajectory tracking error to a near-zero vicinity within fixed time. Simulation results strongly support the efficacy of the proposed control strategy.
    publisherAmerican Society of Civil Engineers
    titleThe Control of Fixed-Time Trajectory Tracking for Stratospheric Airships with System Uncertainties and External Disturbances
    typeJournal Article
    journal volume37
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5652
    journal fristpage04024078-1
    journal lastpage04024078-14
    page14
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;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