空间站三指末端执行机构建模与操作验证
CSTR:
作者:
作者单位:

1.南京航空航天大学宇航空间机构全国重点实验室,南京 210016;2.南京航空航天大学深空探测星表机构 技术工信部重点实验室,南京 210016;3.上海宇航系统工程研究所,上海 201109

作者简介:

通讯作者:

王宸,男,副研究员,E-mail:nuaawangchen@nuaa.edu.cn。

中图分类号:

V528

基金项目:

国家自然科学基金(U21B6002, 52075242);江苏省自然科学基金(BK20210297);江苏省研究生科研创新计划(KYCX22_0382); 宇航空间机构全国重点实验室自研课题(2024ASM-ZY08)。


Modeling and Operation Verification of Three-Finger Manipulator of Space Stations
Author:
Affiliation:

1.National Key Laboratory of Aerospace Mechanism, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China;2.Key Laboratory of Exploration Mechanism of Deep Space Planet Surface, Ministry of Industry and Information Technology, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China;3.Shanghai Institute of Aerospace System Engineering, Shanghai 201109, China

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    为满足航天器在轨维护等高风险任务对高可靠操作工具的迫切需求,针对多指机械手在非结构化环境中面临的稳定性与适应性难题,本文提出了一种涵盖静力学、运动学与动力学的多层次耦合建模方法。通过拓扑优化与变刚度原理构建欠驱动手指构型,采用D-H(Denavit-Hartenberg)参数法建立精确捏取与包络抓取的位姿变换模型,并结合牛顿-欧拉方程与拉格朗日动力学理论推导多体耦合动力学方程。仿真与平台实验验证表明:在400 N·mm驱动力矩下,三指接触力稳定于5~6 N范围,旋拧阶段末端速度收敛至0.332 m/s,验证了所提方法的动态稳定性与抗干扰能力。本研究成果为精密操作领域提供了理论支撑,并可拓展至月面手术机器人操作等场景。

    Abstract:

    To meet the urgent need for highly reliable operation tools in high-risk tasks like in-orbit maintenance of spacecraft, a multi-level coupled modeling method is proposed covering statics, kinematics, and dynamics to address the stability and adaptability issues faced by multi-finger manipulators in unstructured environments. The underdriven finger configuration is constructed through topological optimization and the principle of variable stiffness. The pose transformation model for precise pinching and envelope grasping is established by using the D-H (Denavit-Hartenberg) parameter method, and the multi-body coupling dynamic equation is derived by combining the Newton-Euler equation and the Lagrange dynamics theory. Simulation and platform test show that under a driving torque of 400 N·mm, the three-finger contact force stabilizes within the range of 5—6 N, and the speed at the end of the twisting stage converges to 0.332 m/s, verifying the dynamic stability and anti-interference ability of the proposed method. Research results provide theoretical support for the field of precision operation and can be extended to scenarios such as the operation of surgical robots on the lunar surface.

    参考文献
    相似文献
    引证文献
引用本文

任蒙飞,席笑天,张崇峰,侯祺禹,王宸,陈金宝,马嘉,陈萌.空间站三指末端执行机构建模与操作验证[J].南京航空航天大学学报,2025,57(6):1229-1241

复制
分享
相关视频

文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2025-02-27
  • 最后修改日期:2025-10-09
  • 录用日期:
  • 在线发布日期: 2025-12-18
  • 出版日期:
文章二维码
您是第位访问者
网站版权 © 南京航空航天大学学报
技术支持:北京勤云科技发展有限公司