Research of the Low Impact Space Docking Mechanism Based on Impedance Control Strategy

被引:0
作者
Xie, Zenghui [1 ]
Liu, Gangfeng [1 ]
Li, Changle [1 ]
Li, Ge [1 ]
Zhao, Jie [1 ]
Li, Liyi [2 ]
机构
[1] Harbin Inst Technol, State Key Lab Robot & Syst, Harbin 150080, Peoples R China
[2] Harbin Inst Technol, Sch Elect Engn & Automat, Harbin 150001, Peoples R China
来源
2016 12TH IEEE/ASME INTERNATIONAL CONFERENCE ON MECHATRONIC AND EMBEDDED SYSTEMS AND APPLICATIONS (MESA) | 2016年
关键词
mechanism configuration; kinematics; force coupling; impedance control; compliant control tests;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In order to solve the violent collision and energy consumption problems of conventional space docking mechanism in the docking process, we developed a set of low impact docking mechanism based on impedance control. The docking mechanism adopts the peripheral docking type, the active end of which is a 6-UPS parallel mechanism which is driven by six electric cylinders installed on the fixed platform. For the purpose of the safety of the docking mechanism in the process of docking buffer, we need to monitor the contact force between the active end and environment, so tension-pressure sensor is installed on the end of each electric cylinder. This paper designed a kind of highly efficient force coupling algorithm to convert the six separate force into a six-dimensional integral contact force and then established the dynamic relationship between the contact force and the adjustment of the position and posture to ensure the contact force in the docking process not appear large overshoot. Finally, we completed the compliant docking experiments, which proved that the scheme of low impact docking mechanism is feasible and that the docking mechanism can finish the expected mission.
引用
收藏
页数:6
相关论文
共 7 条
  • [1] Inaba N, 2000, ROB AUT 2000 P ICRA, V2, P1169
  • [2] Laixing L I N, 2007, SPACECRAFT ENG, V4
  • [3] Liu G, 2015, MULTIAXIS FORCE MEAS
  • [4] Wang X.-G., 2001, ACTA SIMULATA SYSTEM, V4
  • [5] A universal on-orbit servicing system used in the geostationary orbit
    Xu, Wenfu
    Liang, Bin
    Li, Bing
    Xu, Yangsheng
    [J]. ADVANCES IN SPACE RESEARCH, 2011, 48 (01) : 95 - 119
  • [6] Research of flexible beam impact dynamics based on space probe-cone docking mechanism
    Zhang, Xiang
    Huang, Yiyong
    Han, Wei
    Chen, Xiaoqian
    [J]. ADVANCES IN SPACE RESEARCH, 2012, 49 (06) : 1053 - 1061
  • [7] Zimpfer D., 2005, 1st Space Exploration Conference: Continuing the Voyage of Discovery, V1, P234, DOI [DOI 10.2514/6.2005-2523(VERP.7, 10.2514/6.20 05-2523 (ver p. 7]