• DocumentCode
    3573046
  • Title

    Contact-impact dynamics simulation for space manipulator using equivalent spring-damping model

  • Author

    Houwei Ji ; Min Li ; Xiangcun Wang ; Yang Li ; Lianhang Dou

  • Author_Institution
    Sch. of Mechatron. Eng. & Autom., Shanghai Univ., Shanghai, China
  • fYear
    2014
  • Firstpage
    3186
  • Lastpage
    3191
  • Abstract
    Modelling of contact dynamics is a very essential step in dynamics simulation of robotics operation on space stations, e.g. extravehicular activities, assistances, assembly and maintenance of the station, etc. This paper presents an equivalent spring-damping contact model (ESDCM) to simulate the impacts between the end-effector of space manipulator and its environment, where the contact force is calculated by the model. The ESDCM model is based on the general trend of Hertz contact law in conjunction with a hysteresis damping function. The coefficients in the model have been analyzed. Simulation has been done on multi-body optimization simulation software. The simulations show that the proposed model based on the ESDCM model can reflect the contact phase between space manipulator and free-flying target effectively.
  • Keywords
    aerospace computing; aerospace robotics; control engineering computing; damping; digital simulation; end effectors; hysteresis; manipulator dynamics; optimisation; ESDCM; Hertz contact law; contact-impact dynamics simulation; end-effector; equivalent spring-damping contact model; hysteresis damping function; multibody optimization simulation software; robotics operation; space manipulator; space stations; Analytical models; Dynamics; Force; Manipulator dynamics; Mathematical model; Space vehicles; Contact Dynamics; Impact; Space Manipulator; Spring-Damping Model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation (WCICA), 2014 11th World Congress on
  • Type

    conf

  • DOI
    10.1109/WCICA.2014.7053240
  • Filename
    7053240