空间近距离金属碎片的无接触式减旋机构研究

微特电机 ›› 2021, Vol. 49 ›› Issue (6): 17-21.

空间近距离金属碎片的无接触式减旋机构研究

王骞, 陈津灏, 孙全浩, 姜在临, 李勇

哈尔滨工业大学电气工程与自动化学院,哈尔滨 150001

收稿日期:2021-01-18 出版日期:2021-06-28 发布日期:2021-06-22
作者简介:王骞(1982—),男,副教授,博士生导师,主要从事航空航天电机系统、直线电机系统等方面的研究。
基金资助:
机器人技术与系统国家重点实验室自主课题资助项目(SKLRS201812B)

Research on Non-Contact Derotation Mechanism to Metal Fragments Closely in Space

WANG Qian, CHEN Jin-hao, SUN Quan-hao, JIANG Zai-lin, LI Yong

School of Electrical Engineering and Automation, Harbin Institute of Technology, Harbin 150001, China

Received:2021-01-18 Online:2021-06-28 Published:2021-06-22

摘要/Abstract

摘要： 太空金属碎片需要先被减旋,才能进行回收或销毁。对捕捉金属碎片的无接触式减旋机构的工作原理进行了理论分析,以数学模型为基础,有限元计算为辅助,对其结构参数影响和集肤效应进行了对比研究。结合被捕捉目标自身属性,设计了一种非接触式双轭圆环式线圈减旋机构,仿真分析结果证明了该减旋机构的减旋效率高。

关键词: 无接触式减旋机构, 集肤效应, 电磁线圈, 金属碎片

Abstract: The metal fragments in space need to be reduced before they can be recycled or destroyed. The working principle of the non-contact derotation mechanism to metal fragments was analyzed. Based on the mathematical model, with the aid of finite element calculation, the influence of its structural parameters and the skin effect were compared. A non-contact double yoke toroidal coil reduction mechanism was designed based on the properties of the captured target. The simulation analysis results proved that the reduction effect is good.

Key words: non-contact derotation mechanism, skin effect, electromagnetic coil, metal fragment

中图分类号:

TM351

王骞, 陈津灏, 孙全浩, 姜在临, 李勇. 空间近距离金属碎片的无接触式减旋机构研究[J]. 微特电机, 2021, 49(6): 17-21.

WANG Qian, CHEN Jin-hao, SUN Quan-hao, JIANG Zai-lin, LI Yong. Research on Non-Contact Derotation Mechanism to Metal Fragments Closely in Space[J]. Small & Special Electrical Machines, 2021, 49(6): 17-21.

参考文献

[1] SHAN M H, GUO J, EBERHARD G.Review and comparison of active space debris capturing and removal methods[J].Progress in Aerospace Sciences,2016(80):18-32.
[2] 马广富,郭延宁,邱爽,等.空间非合作目标消旋技术研究现状总结与展望[J].飞控与探测,2018,1(1):26-33.
[3] ANSELMO L,PARDINI C.Compliance of the Italian satellites in low Earth orbit with the end-of-life disposal guidelines for Space Debris Mitigation and ranking of their long-term criticality for the environment [J].ActaAstronautica,2015(114):93-10.
[4] HUANG P F, ZHANG F, MENG Z J, et al.Adaptive control for space debris removal with uncertain kinematics,dynamics and states[J].ActaAstronautica,2016(128):416-430.
[5] WORMNES K,DE JONG J H,KRAG H,et al.Throw-nets and tethersfor robust space debris capture [C]//64th International Astronautical Congress,2013:23-27.
[6] PAPUSHEV P,KARAVAEV Y,MISHINA M.Investigations of the evolution of optical characteristics and dynamics of proper rotation of uncontrolled geostationary artificial satellites [J].Advances in Space Research,2009,43(9):1416-1422.
[7] AN X Y,REN Z, LU W.Terminal sliding mode control of attitude synchronization for autonomous docking to a tumbling satellite[C]//International Conferenceon Mechatronic Sciences,Electric Engineering and Computer (MEC),2013:2760-2763.
[8] SUGAI F,ABIKO S,TSUJITA T,et al.Development of an eddy current brake system for detumbling malfunctioning satellites[C]//IEEE/SICE International Symposium on System Integration (SII),2012:325-330.
[9] 孙晟昕,吴昊,魏承,等.基于柔性毛刷的自旋卫星的消旋动力学分析[J].中国科学:物理学力学天文学,2019,49(2):139-146.
[10] 张帆,黄攀峰.空间绳系机器人抓捕非合作目标的质量特性参数辨识[J].宇航学报,2015,36(6):630-639.
[11] 王哲.面向大型旋转空间碎片捕获的接触式消旋技术研究[D].哈尔滨:哈尔滨工业大学,2018.
[12] 石永康,杨乐平,朱彦伟,等.空间旋转目标涡流消旋概念与仿真分析[J].宇航学报,2018,39(10):1089-1096.
[13] 孙全浩.空间非磁化金属体的近距离无接触式减旋机构研究[D].哈尔滨:哈尔滨工业大学,2020.