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兵工学报 ›› 2014, Vol. 35 ›› Issue (7): 1003-1008.doi: 10.3969/j.issn.1000-1093.2014.07.010

• 论文 • 上一篇    下一篇

双柔性空间机械臂动力学建模与控制

杨永泰1, 荣吉利1, 李健2, 刘宾3, 胡成威3   

  1. (1.北京理工大学 宇航学院, 北京 100081; 2.广西科技大学 汽车与交通学院, 广西 柳州 545006;
  • 收稿日期:2013-08-19 修回日期:2013-08-19 上线日期:2014-09-05
  • 通讯作者: 杨永泰 E-mail:yangyongtai_bit@163.com
  • 作者简介:杨永泰(1985—),男,博士研究生
  • 基金资助:
    国家自然科学基金项目(10972033);中国空间技术研究院创新基金项目(CAST20100141107)

Dynamic Modeling and Control of Space Manipulator with Flexible Joints and Links

YANG Yong-tai1, RONG Ji-li1, LI Jian2, LIU Bin3, HU Cheng-wei3   

  1. (1.School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;2.Automotive and Transportation Engineering Institute, Guangxi University of Science and Technology,Liuzhou 545006, Guangxi, China; 3.China Academy of Space Technology, Beijing 100094, China)
  • Received:2013-08-19 Revised:2013-08-19 Online:2014-09-05
  • Contact: YANG Yong-tai E-mail:yangyongtai_bit@163.com

摘要: 大多数研究者在空间机械臂动力学建模时,只考虑了关节柔性或者臂杆柔性,并且通常采用假设模态法对臂杆的变形进行描述,但该方法仅适用于小变形情况。基于这种情况,采用自然坐标法对柔性关节进行建模和绝对节点坐标法对柔性臂杆进行建模,得到了既包含关节柔性又包含臂杆柔性的空间机械臂动力学方程,并能精确地描述臂杆的小变形以及大变形。利用5次多项式对关节轨迹进行规划,通过逆动力学得到关节的前馈驱动力矩;采用PID控制策略,作为反馈输入。在二连杆柔性关节柔性杆机械臂上进行数值仿真。仿真结果表明:该控制策略在实现关节轨迹跟踪控制的同时,也能有效减弱机械臂的振动。

关键词: 航空航天科学技术基础学科, 空间机械臂, 柔性关节, 柔性杆, 自然坐标法, 绝对节点坐标法, 轨迹跟踪

Abstract: Only joint flexibility or link flexibility is considered in the dynamic modeling of the space manipulator by most researchers, and the assumed mode method, only suitable for small deformation, is usually utilized to describe the flexible deformation of link. Both nature coordinate formulation (NCF) to model the flexible joint and absolute nodal coordinate formulation (ANCF) to model the flexible link are used to obtain the dynamic equations of the space manipulator, which include both joint flexibility and link flexibility and are able to precisely describe both small and large deformations. The joint trajectory is developed by quintic polynomial function, and then the actuator torque is obtained by the inverse dynamics as feedforward. PID control scheme is used as feedback input. The two-link flexible manipulator is used to evaluate this method. Results show that the proposed control scheme is effective in both the tracking of joint trajectory and suppressing of vibration.

Key words: basic disciplines of aerospace science and technology, space manipulator, flexible joint, flexible link, nature coordinate formulation, absolute nodal coordinate formulation, trajectory tracking

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