摘要
空间对接是在航天领域内倍受关注的研究热点和难点问题。由于空间对接的最后阶段推力器是关闭的,依靠惯性使两航天器实现"刚对接",因此缺乏有效应对突发情况的预知能力。为了有效解决依靠惯性使两航天器实现空间刚对接所固有的问题,设计出一种新型电磁对接锁紧机构,并针对该机构的工作原理及在不同工况下的对接过程进行了动力学分析。
Space docking is a space service technology,which has attracted more and more attention in the field of aerospace.Since the thruster is closed in the last stage of space docking,and the docking of two spacecrafts relies on the inertia of the spacecrafts,which is called rigid space docking,it is short of emergency measures.To effectively solve the problem in rigid space docking,a new type of electromagnetic locking mechanism is designed,and a series of research on the working principle and the process of the mechanism is conducted.
作者
孙朋
解志坚
高碧祥
武国梁
SUN Peng;XIE Zhi-jian;GAO Bi-xiang;WU Guo-liang(School of Mechanical and Electrical Engineering,North University of China,Taiyuan 030051,China)
出处
《机械工程与自动化》
2019年第2期30-32,共3页
Mechanical Engineering & Automation
关键词
空间对接技术
新型电磁对接机构
动力学分析
space docking technology
new type of electromagnetic docking mechanism
dynami analysis
作者简介
孙朋(1993-),男,山西运城人,在读硕士研究生,主要研究方向:结构与仿真、自动武器发射技术。
