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    Disturbance Observer–Based Backstepping Control for Hypersonic Vehicles with Input Constraints

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 001::page 04023092-1
    Author:
    Qin Zhong
    ,
    Jiaqi Zhao
    ,
    Ruifan Liu
    ,
    Wei Du
    ,
    Pei Dai
    DOI: 10.1061/JAEEEZ.ASENG-5038
    Publisher: ASCE
    Abstract: A super-twisting disturbance observer–based adaptive fixed-time antisaturation backstepping control algorithm is designed for hypersonic vehicles with input constraints. First, super-twisting disturbance observers are developed to estimate the lumped disturbances comprising model uncertainties, aerodynamic uncertainties, and external disturbances, which will enhance the robustness of the backstepping controller. To address the problem of explosion of complexity in the backstepping approach, hyperbolic sine tracking differentiators are used and which can achieve a higher tracking accuracy than that of the command filtered backstepping control algorithm. Furthermore, an adaptive fixed-time antisaturation compensator (AFAC) is used to suppress the influence of actuator saturation. AFAC can shorten the saturation duration, and the auxiliary variable of AFAC rapidly converges to zero after the saturation disappears. In this case, the controller degenerates to the former backstepping controller. Finally, the effectiveness of the proposed controller is verified by numerical simulation results.
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      Disturbance Observer–Based Backstepping Control for Hypersonic Vehicles with Input Constraints

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4297180
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    contributor authorQin Zhong
    contributor authorJiaqi Zhao
    contributor authorRuifan Liu
    contributor authorWei Du
    contributor authorPei Dai
    date accessioned2024-04-27T22:39:22Z
    date available2024-04-27T22:39:22Z
    date issued2024/01/01
    identifier other10.1061-JAEEEZ.ASENG-5038.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4297180
    description abstractA super-twisting disturbance observer–based adaptive fixed-time antisaturation backstepping control algorithm is designed for hypersonic vehicles with input constraints. First, super-twisting disturbance observers are developed to estimate the lumped disturbances comprising model uncertainties, aerodynamic uncertainties, and external disturbances, which will enhance the robustness of the backstepping controller. To address the problem of explosion of complexity in the backstepping approach, hyperbolic sine tracking differentiators are used and which can achieve a higher tracking accuracy than that of the command filtered backstepping control algorithm. Furthermore, an adaptive fixed-time antisaturation compensator (AFAC) is used to suppress the influence of actuator saturation. AFAC can shorten the saturation duration, and the auxiliary variable of AFAC rapidly converges to zero after the saturation disappears. In this case, the controller degenerates to the former backstepping controller. Finally, the effectiveness of the proposed controller is verified by numerical simulation results.
    publisherASCE
    titleDisturbance Observer–Based Backstepping Control for Hypersonic Vehicles with Input Constraints
    typeJournal Article
    journal volume37
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5038
    journal fristpage04023092-1
    journal lastpage04023092-12
    page12
    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
    yabeshDSpacePersian