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    Twist Suppression Method of Tethered Towing for Spinning Space Debris

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 004
    Author:
    Zhongjie Meng
    ,
    Bingheng Wang
    ,
    Panfeng Huang
    DOI: 10.1061/(ASCE)AS.1943-5525.0000708
    Publisher: American Society of Civil Engineers
    Abstract: Towing spinning debris in space is subjected to the risk of twist, increasing the likelihood of collision. To reduce the twist potential, a twist suppression method is proposed for the viscoelastic tether in this paper. The system two-dimensional model is explored taking into account the attitude of the two end bodies and the tether slackness. The twist model describing the twist length is established to investigate the tension change during twist. The impedance based tension controller is designed to regulate tension actively by altering the tether unstretched length. Three cases where the thrust is 1 N, 2 N, and 5 N are studied to validate the feasibility of the method. It is shown that without tension control, towing removal is challenging for the system owing to the twist potential and large tension induced. However, the twist length is reduced dramatically and the relative distance of the two bodies is maintained under the tension control. It is also shown that the controller is robust to the measurement noise, and its performance is better for the lager thrust.
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      Twist Suppression Method of Tethered Towing for Spinning Space Debris

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4245035
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    contributor authorZhongjie Meng
    contributor authorBingheng Wang
    contributor authorPanfeng Huang
    date accessioned2017-12-30T13:03:04Z
    date available2017-12-30T13:03:04Z
    date issued2017
    identifier other%28ASCE%29AS.1943-5525.0000708.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4245035
    description abstractTowing spinning debris in space is subjected to the risk of twist, increasing the likelihood of collision. To reduce the twist potential, a twist suppression method is proposed for the viscoelastic tether in this paper. The system two-dimensional model is explored taking into account the attitude of the two end bodies and the tether slackness. The twist model describing the twist length is established to investigate the tension change during twist. The impedance based tension controller is designed to regulate tension actively by altering the tether unstretched length. Three cases where the thrust is 1 N, 2 N, and 5 N are studied to validate the feasibility of the method. It is shown that without tension control, towing removal is challenging for the system owing to the twist potential and large tension induced. However, the twist length is reduced dramatically and the relative distance of the two bodies is maintained under the tension control. It is also shown that the controller is robust to the measurement noise, and its performance is better for the lager thrust.
    publisherAmerican Society of Civil Engineers
    titleTwist Suppression Method of Tethered Towing for Spinning Space Debris
    typeJournal Paper
    journal volume30
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000708
    page04017012
    treeJournal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 004
    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