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    Shape Change Analysis and Design of Cylindrical Tensegrity Booms

    Source: Journal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005::page 04023047-1
    Author:
    Kaila M. Roffman
    ,
    George A. Lesieutre
    DOI: 10.1061/JAEEEZ.ASENG-4578
    Publisher: ASCE
    Abstract: In space applications, the pursuit of deployable structures with high packaging efficiency and low mass is essential. Tensegrity structures, prestressed networks of struts and cables, offer a promising approach. In this work, a Class-2 cylindrical triplex tensegrity bay is explored for use in booms, where select cables are allowed to change length in order to modify the overall shape of the structure. A novel approach to characterize the range of equilibrated shapes a triplex can achieve is first presented. The results are then used in combination with consideration of bending stiffness, packaging efficiency, and mass to explore the effects of different configuration parameters, namely the ratio of bay height to circumscribing radius (h/r), the member cross-sectional radii, and the number of bays. This design analysis offers new insight into how triplex tensegrity structures can be modified to achieve specific design objectives. Increasing h/r for a single bay increases the range of achievable active tip motion as well as packaging efficiency. Increasing member radii decreases the range of achievable shapes and packaging efficiency while increasing stiffness and mass. When increasing the number of bays for a fixed overall height, a larger number of bays generally increases the range of achievable shapes and mass while reducing stiffness. Packaging efficiency was found to be discontinuous dependent upon the exact number of bays, but generally decreases with increasing number of bays. An example design study is conducted using the Canadarm2 for comparison and illustrates the potential utility of tensegrities for boom structures.
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      Shape Change Analysis and Design of Cylindrical Tensegrity Booms

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    contributor authorKaila M. Roffman
    contributor authorGeorge A. Lesieutre
    date accessioned2023-11-27T23:03:22Z
    date available2023-11-27T23:03:22Z
    date issued6/20/2023 12:00:00 AM
    date issued2023-06-20
    identifier otherJAEEEZ.ASENG-4578.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4293252
    description abstractIn space applications, the pursuit of deployable structures with high packaging efficiency and low mass is essential. Tensegrity structures, prestressed networks of struts and cables, offer a promising approach. In this work, a Class-2 cylindrical triplex tensegrity bay is explored for use in booms, where select cables are allowed to change length in order to modify the overall shape of the structure. A novel approach to characterize the range of equilibrated shapes a triplex can achieve is first presented. The results are then used in combination with consideration of bending stiffness, packaging efficiency, and mass to explore the effects of different configuration parameters, namely the ratio of bay height to circumscribing radius (h/r), the member cross-sectional radii, and the number of bays. This design analysis offers new insight into how triplex tensegrity structures can be modified to achieve specific design objectives. Increasing h/r for a single bay increases the range of achievable active tip motion as well as packaging efficiency. Increasing member radii decreases the range of achievable shapes and packaging efficiency while increasing stiffness and mass. When increasing the number of bays for a fixed overall height, a larger number of bays generally increases the range of achievable shapes and mass while reducing stiffness. Packaging efficiency was found to be discontinuous dependent upon the exact number of bays, but generally decreases with increasing number of bays. An example design study is conducted using the Canadarm2 for comparison and illustrates the potential utility of tensegrities for boom structures.
    publisherASCE
    titleShape Change Analysis and Design of Cylindrical Tensegrity Booms
    typeJournal Article
    journal volume36
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-4578
    journal fristpage04023047-1
    journal lastpage04023047-14
    page14
    treeJournal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005
    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