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    Prescribed-Time Guidance Law with Approach Angle Constraint and Actuator Faults

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 001::page 04023107-1
    Author:
    Zihao Wu
    ,
    Xiwang Dong
    ,
    Qingdong Li
    ,
    Jianglong Yu
    ,
    Daikai Liu
    DOI: 10.1061/JAEEEZ.ASENG-5049
    Publisher: ASCE
    Abstract: In this paper, a prescribed-time guidance law with approach angle constraint in the presence of an actuator fault is proposed. Firstly, a sliding mode manifold with prescribed-time convergence is given to ensure that the state of the system converges to the equilibrium point in the specified time. Then, in order to suppress the distrubance, an adaptive gain based on adaptive control is designed. Subsequntly, a augmentation term based on the Lyapunov method is presented to meet the prescribed-time convergence prpoperty when an actuator fault occurs. The prescribed-time convergence of the proposed guidance laws is proven. Numerical simulation results validate the effectiveness of the proposed prescribed-time guidance framework.
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      Prescribed-Time Guidance Law with Approach Angle Constraint and Actuator Faults

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4297181
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    • Journal of Aerospace Engineering

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    contributor authorZihao Wu
    contributor authorXiwang Dong
    contributor authorQingdong Li
    contributor authorJianglong Yu
    contributor authorDaikai Liu
    date accessioned2024-04-27T22:39:24Z
    date available2024-04-27T22:39:24Z
    date issued2024/01/01
    identifier other10.1061-JAEEEZ.ASENG-5049.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4297181
    description abstractIn this paper, a prescribed-time guidance law with approach angle constraint in the presence of an actuator fault is proposed. Firstly, a sliding mode manifold with prescribed-time convergence is given to ensure that the state of the system converges to the equilibrium point in the specified time. Then, in order to suppress the distrubance, an adaptive gain based on adaptive control is designed. Subsequntly, a augmentation term based on the Lyapunov method is presented to meet the prescribed-time convergence prpoperty when an actuator fault occurs. The prescribed-time convergence of the proposed guidance laws is proven. Numerical simulation results validate the effectiveness of the proposed prescribed-time guidance framework.
    publisherASCE
    titlePrescribed-Time Guidance Law with Approach Angle Constraint and Actuator Faults
    typeJournal Article
    journal volume37
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5049
    journal fristpage04023107-1
    journal lastpage04023107-11
    page11
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;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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