空间对接电磁锁紧机构研究  

Research on Space Docking Electromagnetic Locking Mechanism

作　　者：楼雨涵 解志坚[1] 杨臻[1] 王昊东 LOU Yuhan;XIE Zhijian;YANG Zhen;WANG Haodong(School of Mechatronics Engineering, North university of China, Taiyuan 030051, China;China Ordnance Industry Test and Research Institute, Huayin 714200, China)

机构地区：[1]中北大学机电工程学院,太原030051 [2]中国兵器工业试验测试研究院,陕西华阴714200

出　　处：《兵器装备工程学报》2020年第12期113-117,148,共6页Journal of Ordnance Equipment Engineering

基　　金：山西省研究生优秀创新项目(20143082)。

摘　　要：以解决空间对接电磁技术中的刚性锁紧连接为研究重点,在调研国内外空间对接机构的基础上,根据相关功能要求和设计指标,对空间电磁柔性对接技术进行研究。为了验证空间电磁柔性对接技术的可行性,使用Maxwell 3D进行电磁力仿真,再结合Matlab、Adams等软件得出运动规律并还原空间对接电磁锁紧与解锁的工作过程。电磁锁紧与解锁机构的计算仿真验证了该机构的可行性,为空间对接研究提供新的思路。Due to the advantages of low fuel consumption,no pollution,miniaturization and no impact,space electromagnetic docking technology has gradually become a hot spot in the development of space docking technology in the world.In order to solve the problem of rigid lock connection in space electromagnetic docking technology as the research focus,on the basis of full investigation of space docking institutions at home and abroad,according to the relevant functional requirements and design indicators,the space electromagnetic flexible docking technology was studied.In order to verify the feasibility of space electromagnetic flexible docking technology,Maxwell 3D was used for electromagnetic force simulation,and then the movement rules were obtained by combining Matlab and Adams,and the working process of space electromagnetic locking and unlocking was restored.The simulation of the electromagnetic lock and unlock structure proves the feasibility of the structure and provides a new idea for the study of space docking.

关 键 词：空间对接 电磁锁紧 电磁力 锁紧机构 电磁分析 

分 类 号：V423.9[航空宇航科学与技术—飞行器设计] TP391.9[自动化与计算机技术—计算机应用技术]