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Research of impact dynamic modeling of flexible probe-cone docking mechanism based on Kane method

机译:基于凯恩方法的柔性探锥对接机构冲击动力学建模研究

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摘要

Considered in this investigation is the dynamic behavior of space flexible probe-cone docking mechanism, in which the soft cone technology is applied. Kane method and Hertz contact theory are used to obtain the governing equations describing the response of the flexible docking mechanism. These equations are then coded into a computer program and solved using fourth-order Runge-Kutta methods. Results of the theoretical mode are found to be in good agreement with the experimental results, and the numerical results obtained from ANSYS/LS-DYNA software. Furthermore, the influence of soft cone parameters on impact process is discussed based on theoretical model systemically.
机译:在这项研究中考虑的是空间柔性探针锥对接机构的动态行为,其中应用了软锥技术。凯恩方法和赫兹接触理论用于获得描述柔性对接机构响应的控制方程。然后将这些方程式编码到计算机程序中,并使用四阶Runge-Kutta方法求解。理论模式的结果与实验结果吻合良好,数值结果可从ANSYS / LS-DYNA软件获得。此外,基于理论模型系统地讨论了软锥参数对冲击过程的影响。

著录项

  • 来源
    《Archive of Applied Mechanics》 |2015年第2期|205-221|共17页
  • 作者单位

    College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;

    College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;

    College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Probe-cone docking mechanism; Soft cone; Simulation; Impact dynamics; Kane method;

    机译:探锥对接机制;软锥模拟;冲击动力学;凯恩法;

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