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    Adjustable Stiffness CLSM and Its Application in a Gravity Off-Load System

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 003::page 04025015-1
    Author:
    Biaobiao Jiao
    ,
    Baiyan He
    ,
    Yuhang Zhang
    ,
    Lingwei Niu
    ,
    Shilong Yue
    ,
    Jiaming Ma
    DOI: 10.1061/JAEEEZ.ASENG-5956
    Publisher: American Society of Civil Engineers
    Abstract: Gravity offloading technology is crucial in scientific research and engineering, especially when simulating microgravity. Its core is active constant force control, which is a research hotspot in this field. Developing efficient low-stiffness mechanisms improves the force control accuracy of active constant force systems (ACFSs). This paper proposes a novel compliant low-stiffness mechanism (CLSM) that achieves quasi-linear characteristics by superimposing the linear positive stiffness of the tension spring and the negative stiffness of the V-shaped compliant beam. An efficient optimization design method for CLSM is proposed, simplifying the compliant mechanism design. The optimized CLSM can achieve quasi-linear low-stiffness output in a large displacement range with adjustable stiffness and load capacity. In addition, the optimized CLSM is characterized by high load-bearing capacity, low inertia, small volume, and low friction. A new lightweight and miniaturized ACFS based on CLSM is designed to meet the design requirements of the multicable gravity offloading system. The CLSM exhibits excellent dynamic characteristics of low inertia and friction, reducing the system’s internal disturbances while meeting the stiffness and load-bearing capacity requirements of ACFSs. The experimental prototype is established to test the ACFS. The results indicate that the control accuracy of ACFS with CLSM is significantly improved under dynamic excitation.
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      Adjustable Stiffness CLSM and Its Application in a Gravity Off-Load System

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4307061
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    contributor authorBiaobiao Jiao
    contributor authorBaiyan He
    contributor authorYuhang Zhang
    contributor authorLingwei Niu
    contributor authorShilong Yue
    contributor authorJiaming Ma
    date accessioned2025-08-17T22:31:43Z
    date available2025-08-17T22:31:43Z
    date copyright5/1/2025 12:00:00 AM
    date issued2025
    identifier otherJAEEEZ.ASENG-5956.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307061
    description abstractGravity offloading technology is crucial in scientific research and engineering, especially when simulating microgravity. Its core is active constant force control, which is a research hotspot in this field. Developing efficient low-stiffness mechanisms improves the force control accuracy of active constant force systems (ACFSs). This paper proposes a novel compliant low-stiffness mechanism (CLSM) that achieves quasi-linear characteristics by superimposing the linear positive stiffness of the tension spring and the negative stiffness of the V-shaped compliant beam. An efficient optimization design method for CLSM is proposed, simplifying the compliant mechanism design. The optimized CLSM can achieve quasi-linear low-stiffness output in a large displacement range with adjustable stiffness and load capacity. In addition, the optimized CLSM is characterized by high load-bearing capacity, low inertia, small volume, and low friction. A new lightweight and miniaturized ACFS based on CLSM is designed to meet the design requirements of the multicable gravity offloading system. The CLSM exhibits excellent dynamic characteristics of low inertia and friction, reducing the system’s internal disturbances while meeting the stiffness and load-bearing capacity requirements of ACFSs. The experimental prototype is established to test the ACFS. The results indicate that the control accuracy of ACFS with CLSM is significantly improved under dynamic excitation.
    publisherAmerican Society of Civil Engineers
    titleAdjustable Stiffness CLSM and Its Application in a Gravity Off-Load System
    typeJournal Article
    journal volume38
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5956
    journal fristpage04025015-1
    journal lastpage04025015-14
    page14
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 003
    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