YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Analysis and Optimization of Transmission Performance of Low-Impact Docking Mechanism

    Source: Journal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005::page 04023048-1
    Author:
    Jia-Yu Dong
    ,
    Jin-Bao Chen
    ,
    Jie Wang
    ,
    Chuan-Zhi Chen
    ,
    Zhi-Cheng Song
    ,
    Jia-Qi Li
    DOI: 10.1061/JAEEEZ.ASENG-4519
    Publisher: ASCE
    Abstract: Compared with the traditional docking mechanism, a low-impact docking mechanism (LIDM) has a big advantage, that is, LIDMs can realize low-impact docking by controlling the movement of the driving rods in real-time. In this process, the load sensing ring (LSR) of the chaser spacecraft is adjusted in real-time according to the position and attitude of the target spacecraft, which requires that the LIDM has high transmission efficiency, so that the position and attitude of the LSR can be changed rapidly under the motion of the driving rods and respond to the position and attitude requirements of the docking control system to the LSR as soon as possible. In this paper, a transmission efficiency solution and an optimization method suitable for LIDMs are proposed. The LIDM dynamic model and transmission efficiency model are established, and an improved genetic algorithm with better convergence effect is proposed and used to optimize the transfer efficiency. The results of numerical examples in this paper show that the improved genetic algorithm has stronger global optimization ability when calculating high-complexity optimization problems. In the optimized LIDM configuration parameters, the size of LSR and the bottom reference circle are close to the lower limit and upper limit of the given size limit, respectively, and the instantaneous transmission force ratio is increased from 0.6477 to 0.9160. The reliability of the optimized results is verified in dynamic simulation software. This study provides ideas and methods for the design and optimization of subsequent high transmission efficiency mechanisms.
    • Download: (1.770Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Analysis and Optimization of Transmission Performance of Low-Impact Docking Mechanism

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4293245
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    contributor authorJia-Yu Dong
    contributor authorJin-Bao Chen
    contributor authorJie Wang
    contributor authorChuan-Zhi Chen
    contributor authorZhi-Cheng Song
    contributor authorJia-Qi Li
    date accessioned2023-11-27T23:02:52Z
    date available2023-11-27T23:02:52Z
    date issued6/21/2023 12:00:00 AM
    date issued2023-06-21
    identifier otherJAEEEZ.ASENG-4519.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4293245
    description abstractCompared with the traditional docking mechanism, a low-impact docking mechanism (LIDM) has a big advantage, that is, LIDMs can realize low-impact docking by controlling the movement of the driving rods in real-time. In this process, the load sensing ring (LSR) of the chaser spacecraft is adjusted in real-time according to the position and attitude of the target spacecraft, which requires that the LIDM has high transmission efficiency, so that the position and attitude of the LSR can be changed rapidly under the motion of the driving rods and respond to the position and attitude requirements of the docking control system to the LSR as soon as possible. In this paper, a transmission efficiency solution and an optimization method suitable for LIDMs are proposed. The LIDM dynamic model and transmission efficiency model are established, and an improved genetic algorithm with better convergence effect is proposed and used to optimize the transfer efficiency. The results of numerical examples in this paper show that the improved genetic algorithm has stronger global optimization ability when calculating high-complexity optimization problems. In the optimized LIDM configuration parameters, the size of LSR and the bottom reference circle are close to the lower limit and upper limit of the given size limit, respectively, and the instantaneous transmission force ratio is increased from 0.6477 to 0.9160. The reliability of the optimized results is verified in dynamic simulation software. This study provides ideas and methods for the design and optimization of subsequent high transmission efficiency mechanisms.
    publisherASCE
    titleAnalysis and Optimization of Transmission Performance of Low-Impact Docking Mechanism
    typeJournal Article
    journal volume36
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-4519
    journal fristpage04023048-1
    journal lastpage04023048-13
    page13
    treeJournal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005
    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