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    Vibration Suppression of an Underactuated Dynamic System Using Virtual Actuators

    Source: Journal of Vibration and Acoustics:;2016:;volume( 138 ):;issue: 006::page 61006
    Author:
    Khoshnood, A. M.
    ,
    Azad, I.
    ,
    Hasani, S. M.
    DOI: 10.1115/1.4034082
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Sloshing is one of the critical problems in aerospace vehicles with liquid containers. Motion of the liquid in resonance situations can degrade the stability and performance of attitude control systems. Two important characteristics of this time varying phenomenon are sensorless and underactuated properties which lead to difficulty of attitude control system design. In this paper, a new technique based on soft sensor and virtual actuator is used to suppress the effects of fuel sloshing in an aerospace launch vehicle (ALV). For this purpose, a nonlinear dynamic model of the vehicle with mechanical model of the fuel sloshing is considered as a multibody dynamic system. The preliminary attitude control system of the vehicle is extended using the new vibration suppression technique and a numerical simulation of the nonlinear model is carried out. Results of the simulation show that the undesired effects of the fuel sloshing are effectively decreased using the proposed vibration suppression technique.
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      Vibration Suppression of an Underactuated Dynamic System Using Virtual Actuators

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    https://yetl.yabesh.ir/yetl1/handle/yetl/162974
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    contributor authorKhoshnood, A. M.
    contributor authorAzad, I.
    contributor authorHasani, S. M.
    date accessioned2017-05-09T01:34:56Z
    date available2017-05-09T01:34:56Z
    date issued2016
    identifier issn1048-9002
    identifier othervib_138_06_061006.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162974
    description abstractSloshing is one of the critical problems in aerospace vehicles with liquid containers. Motion of the liquid in resonance situations can degrade the stability and performance of attitude control systems. Two important characteristics of this time varying phenomenon are sensorless and underactuated properties which lead to difficulty of attitude control system design. In this paper, a new technique based on soft sensor and virtual actuator is used to suppress the effects of fuel sloshing in an aerospace launch vehicle (ALV). For this purpose, a nonlinear dynamic model of the vehicle with mechanical model of the fuel sloshing is considered as a multibody dynamic system. The preliminary attitude control system of the vehicle is extended using the new vibration suppression technique and a numerical simulation of the nonlinear model is carried out. Results of the simulation show that the undesired effects of the fuel sloshing are effectively decreased using the proposed vibration suppression technique.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleVibration Suppression of an Underactuated Dynamic System Using Virtual Actuators
    typeJournal Paper
    journal volume138
    journal issue6
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.4034082
    journal fristpage61006
    journal lastpage61006
    identifier eissn1528-8927
    treeJournal of Vibration and Acoustics:;2016:;volume( 138 ):;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