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    Thermal Design Optimization Method of Mesh Reflector Antennas Considering Deformation Compatibility Conditions

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 004::page 04022048
    Author:
    Shunji Zhang
    ,
    Shuxin Zhang
    ,
    Wang Zhong
    ,
    Zihan Sun
    DOI: 10.1061/(ASCE)AS.1943-5525.0001442
    Publisher: ASCE
    Abstract: Cable-network structures are an important part of mesh reflector antennas. The performance of antennas depends greatly on the surface accuracy and tension distribution. However, there are periodic temperature changes in the space environment where the mesh antenna is located. The traditional form-finding and optimization design methods can only guarantee good performance at room temperature, while active adjustment technology is limited by on-orbit measurement technology and control technology. Therefore, it is critical to carefully design the cable-network configuration to reduce the influence of space thermal loads. In this study, a thermal design optimization method for mesh reflector antennas was proposed by considering the deformation compatibility conditions. The length variation of the cable element under thermal loads was analyzed accurately. With the combination of the force density sensitivity matrix and temperature deformation equation, the force density increment equation of the whole cable net was established. By constraining the reflector nodes to the paraboloid and selecting the quadratic sum of the node thermal deformation as the objective function, we obtained a cable-network configuration with better surface shape stability than traditional design methods. Finally, a numerical example is presented to illustrate the effectiveness of the proposed method.
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      Thermal Design Optimization Method of Mesh Reflector Antennas Considering Deformation Compatibility Conditions

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4286176
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    • Journal of Aerospace Engineering

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    contributor authorShunji Zhang
    contributor authorShuxin Zhang
    contributor authorWang Zhong
    contributor authorZihan Sun
    date accessioned2022-08-18T12:11:39Z
    date available2022-08-18T12:11:39Z
    date issued2022/04/26
    identifier other%28ASCE%29AS.1943-5525.0001442.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4286176
    description abstractCable-network structures are an important part of mesh reflector antennas. The performance of antennas depends greatly on the surface accuracy and tension distribution. However, there are periodic temperature changes in the space environment where the mesh antenna is located. The traditional form-finding and optimization design methods can only guarantee good performance at room temperature, while active adjustment technology is limited by on-orbit measurement technology and control technology. Therefore, it is critical to carefully design the cable-network configuration to reduce the influence of space thermal loads. In this study, a thermal design optimization method for mesh reflector antennas was proposed by considering the deformation compatibility conditions. The length variation of the cable element under thermal loads was analyzed accurately. With the combination of the force density sensitivity matrix and temperature deformation equation, the force density increment equation of the whole cable net was established. By constraining the reflector nodes to the paraboloid and selecting the quadratic sum of the node thermal deformation as the objective function, we obtained a cable-network configuration with better surface shape stability than traditional design methods. Finally, a numerical example is presented to illustrate the effectiveness of the proposed method.
    publisherASCE
    titleThermal Design Optimization Method of Mesh Reflector Antennas Considering Deformation Compatibility Conditions
    typeJournal Article
    journal volume35
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001442
    journal fristpage04022048
    journal lastpage04022048-10
    page10
    treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 004
    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