1U-Sized Deployable Space Manipulator for Future On-Orbit Servicing, Assembly, and Manufacturing

Jinguo Liu, Pengyu Zhao, Keli Chen, Xin Zhang, Xiang Zhang
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引用次数: 1

Abstract

Miniaturized, multifunctional, and economical on-orbit service satellites have been increasingly used with the continuous increase of space exploration missions. In this paper, an innovative deployable manipulator is designed, named Cubot, which can be stowed in 1 U-sized (10 cm×10 cm×10 cm) space. With CubeSat as the carrier, the deployable Cubot aims to achieve a variety of on-orbit operation tasks including space debris removal and space station on-orbit maintenance, for future on-orbit servicing, assembly, and manufacturing (OSAM). A kinematics modeling method of a space manipulator with passive joints is proposed, and the motion equation of the manipulator is derived. Considered the elastic potential energy stored in the passive joint during deployment, the momentum change of Cubot is simulated and analyzed. As the main forced element, the end effector is analyzed using FEA. Dynamic stress response with respect to the force distribution and the clamping angle is analyzed to evaluate mechanical performances of the end-effector component. Deployment tests are conducted to verify the feasibility of Cubot based on a principled prototype, which aims to provide engineering and practical experience for the development of this field.
面向未来在轨服务、装配和制造的1u尺寸可展开空间机械臂
随着空间探索任务的不断增加,在轨服务卫星的小型化、多功能化和经济化得到了越来越多的应用。本文设计了一种新型的可展开机械手Cubot,可放置在1u大小(10 cm×10 cm×10 cm)的空间内。以CubeSat为载体,可部署Cubot旨在实现各种在轨操作任务,包括空间碎片清除和空间站在轨维护,为未来的在轨服务、组装和制造(OSAM)服务。提出了一种具有被动关节的空间机械臂的运动学建模方法,推导了该机械臂的运动方程。考虑被动关节在展开过程中储存的弹性势能,对Cubot的动量变化进行了仿真分析。末端执行器作为主要受力单元,采用有限元法对其进行了分析。分析了与力分布和夹持角有关的动应力响应,评价了末端执行器部件的力学性能。基于原理样机进行部署测试,验证Cubot的可行性,旨在为该领域的发展提供工程和实践经验。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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