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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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