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    Finite-Time Fault Estimation and Fault-Tolerant Control for Rigid Spacecraft

    Source: Journal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 006
    Author:
    Zhang Xiu-yun;Zong Qun;Tian Bai-ling;Shao Shi-kai;Liu Wen-jing
    DOI: 10.1061/(ASCE)AS.1943-5525.0000915
    Publisher: American Society of Civil Engineers
    Abstract: This paper investigates a fault tolerant problem for the rigid spacecraft in the presence of additive faults and nonlinear disturbances. An adaptive observer and an adaptive terminal sliding mode observer (ATSMO) are presented respectively to distinguish the faults and external disturbances in finite time. Then, we develop a novel finite-time continuous terminal sliding mode controller (CTSMC) to compensate the detected faults. Unlike most of the existing online fault estimation, the proposed approach could achieve finite-time reconstruction of unknown faults and disturbances simultaneously, while the upper bound knowledge is unnecessary. Moreover, the proposed finite-time fault-tolerant controller (FTC) is only based on the information of available output and its first derivative. The effectiveness of the proposed methodology is demonstrated by simulation results.
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      Finite-Time Fault Estimation and Fault-Tolerant Control for Rigid Spacecraft

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4248366
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    contributor authorZhang Xiu-yun;Zong Qun;Tian Bai-ling;Shao Shi-kai;Liu Wen-jing
    date accessioned2019-02-26T07:37:41Z
    date available2019-02-26T07:37:41Z
    date issued2018
    identifier other%28ASCE%29AS.1943-5525.0000915.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4248366
    description abstractThis paper investigates a fault tolerant problem for the rigid spacecraft in the presence of additive faults and nonlinear disturbances. An adaptive observer and an adaptive terminal sliding mode observer (ATSMO) are presented respectively to distinguish the faults and external disturbances in finite time. Then, we develop a novel finite-time continuous terminal sliding mode controller (CTSMC) to compensate the detected faults. Unlike most of the existing online fault estimation, the proposed approach could achieve finite-time reconstruction of unknown faults and disturbances simultaneously, while the upper bound knowledge is unnecessary. Moreover, the proposed finite-time fault-tolerant controller (FTC) is only based on the information of available output and its first derivative. The effectiveness of the proposed methodology is demonstrated by simulation results.
    publisherAmerican Society of Civil Engineers
    titleFinite-Time Fault Estimation and Fault-Tolerant Control for Rigid Spacecraft
    typeJournal Paper
    journal volume31
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000915
    page4018091
    treeJournal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 006
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian