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基于递归Gibbs-Appell的柔性空间机器人建模与特性分析

张福礼 袁朝辉

张福礼, 袁朝辉. 基于递归Gibbs-Appell的柔性空间机器人建模与特性分析[J]. 航空动力学报, 2023, 38(10):2545-2560 doi: 10.13224/j.cnki.jasp.20220052
引用本文: 张福礼, 袁朝辉. 基于递归Gibbs-Appell的柔性空间机器人建模与特性分析[J]. 航空动力学报, 2023, 38(10):2545-2560 doi: 10.13224/j.cnki.jasp.20220052
ZHANG Fuli, YUAN Zhaohui. Flexible space robot modeling and characteristic analysis based on recursive Gibbs-Appell[J]. Journal of Aerospace Power, 2023, 38(10):2545-2560 doi: 10.13224/j.cnki.jasp.20220052
Citation: ZHANG Fuli, YUAN Zhaohui. Flexible space robot modeling and characteristic analysis based on recursive Gibbs-Appell[J]. Journal of Aerospace Power, 2023, 38(10):2545-2560 doi: 10.13224/j.cnki.jasp.20220052

基于递归Gibbs-Appell的柔性空间机器人建模与特性分析

doi: 10.13224/j.cnki.jasp.20220052
基金项目: 国家自然科学基金(51505381)
详细信息
    作者简介:

    张福礼(1986-),男,博士生,主要从事空间机器人动力学建模与控制方法研究。E-mail:zhangfuli2007@sina.com

  • 中图分类号: V414.2

Flexible space robot modeling and characteristic analysis based on recursive Gibbs-Appell

  • 摘要:

    利用递归Gibbs-Appell方法研究了多重柔性的空间机器人动力学建模与特性分析。首先,根据Timoshenko beam theory与集中刚度分别对连杆与关节进行柔性描述,其次,利用旋转矩阵R3×3与平移向量L1×3的简化了齐次变换矩阵T4×4以降低递推运动学难度,利用递归Gibbs函数与势能函数推导了柔性空间机器人的逆向动力学模型,再次,利用反向递归法获取了惯量矩阵与耦合矩阵,并构建了正向动力学模型。最后数值仿真结果表明,Matlab与Adams的仿真结果相对偏差不超过0.1%,Z弯曲变形相对于X剪切变形与Y扭转变形数量级超过了103,这验证所建模型的正确性。在一定范围内,关节刚度增加50 N·m/rad时,连杆最大变形增量不超过1.5×10−3 m,关节摩擦成5倍增长时,连杆最大变形增量不超过2×10−3 m,帆板的增量变形具有相同变化趋势。

     

  • 图 1  柔性空间机器人的结构与变形描述

    Figure 1.  Structure and deformation description of flexible space robot

    图 2  空间柔性机器人整体系统结构

    Figure 2.  The system structure of space flexible robot

    图 3  基于Gibbs-Appell的递归动力学计算流程

    Figure 3.  Recursive dynamics calculation flow based on Gibbs-Appell

    图 4  载体的位姿变化

    Figure 4.  Pose change of carrier

    图 5  机械臂关节角度变化

    Figure 5.  Changes of joint angles

    图 6  机械臂关节柔性变化

    Figure 6.  Changes of joint flexibilit

    图 7  机械臂末端变形

    Figure 7.  Deformation at the end of the manipulator

    图 8  帆板中心点变形

    Figure 8.  Deformation of solar panel center point

    图 9  机械臂末端变形(不同关节刚度)

    Figure 9.  End deformation of manipulator (different joint stiffnesses)

    图 10  帆板中心点变形(不同关节刚度)

    Figure 10.  Deformation of solar panel center point (different joint stiffnesses)

    图 11  机械臂末端变形(不同关节摩擦因数)

    Figure 11.  End deformation of manipulator (different joint friction coefficients)

    图 12  帆板中心点变形(不同关节摩擦因数)

    Figure 12.  Deformation of solar panel center point (different joint friction coefficients)

    表  1  坐标系的意义

    Table  1.   Significance of coordinate systems

    名称实际坐标xiyizi浮动坐标$ {\hat x_i} $、$ {\hat y_i} $、${\hat {\textit{z} }_i}$
    说明X与关节轮毂平行,并与(i+1)关节轮毂方向平行;
    Z轴与平行电动机轴转动关节;Y轴由右手定律决定
    轴$ \hat X $与变形连杆平行,并与(i+1)关节的轮毂方向平行;$ \hat Z $轴与平行电动机轴转动关节;$ \hat Y $轴由右手定律决定
    下载: 导出CSV

    表  2  空间柔性机器人关节机构物理参数

    Table  2.   Physical parameters of joint mechanism of space flexible robot

    关节质量/kg尺寸/m 惯量/(kg·m2阻尼系数/
    (N·m·s/rad)
    刚度系数/
    (N·m/rad)
    长度半径IxxIyyIzz
    J1J22.30.060.07 0.07450.07450.01000.051000
    J3J4J5, J62.30.060.070.07450.07450.01000.05800
    下载: 导出CSV

    表  3  空间柔性机器人机构物理参数

    Table  3.   Physical parameters of spatial flexible robot mechanism

    机械臂质量/kg尺寸/m 惯量/(kg·m2弹性模量/
    109 Pa
    长度宽或半径IxxIyyIzz
    B01.58×1031.51.51.5 1.481×1031.481×1030.592×103210
    B1100.2560.0630.07450.07450.0397210
    B2171.7740.0634.4920.06754.49270
    B3, B550.1280.0630.03310.03310.0397210
    B4161.6040.0633.4620.06353.46270
    B670.2940.0630.06430.06430.0278210
    Bp162410.029.00056.45647.6270.37
    下载: 导出CSV
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  • 收稿日期:  2022-01-31
  • 网络出版日期:  2023-08-29

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