首页 /研究 /Design of an End-effector for Spacecraft Automatic Assembly Robot
OTHER

Design of an End-effector for Spacecraft Automatic Assembly Robot

Bin Zhang, Chengli Zhang, Fugui Xie, Wangmin Yi, Shaohua Meng, Wei Wang

发表年份
2019
引用次数
2

摘要

Abstract With the increasing of large-weight equipment on spacecraft, the traditional assembly method using hoisting manual guidance has some shortcomings, such as poor flexibility, high risk of bumping, low assembly efficiency, etc. [1]. In recent years, robot assembly system has been widely used in spacecraft assembly process. End-effector is an important part of automatic assembly robot. In this paper, an end-effector for batch equipment installation with fast connection and fast release function was designed. Through simulation analysis and experimental verification, it proves that the end-effector has good performance and can meet the application requirements. It helps to raise efficiency and reduce cost for spacecraft assembly.

关键词

Robot end effectorSpacecraftFlexibility (engineering)RobotBumpingProcess (computing)EngineeringComputer scienceControl engineeringMechanical engineering

相关论文

查看 OTHER 分类全部论文