• DocumentCode
    1868772
  • Title

    Error model and vibration analysis of Timoshenko beam subjected to a moving mass

  • Author

    Qu, Zhiyong ; Yao, Yu

  • Author_Institution
    Harbin Inst. of Technol.
  • fYear
    2006
  • fDate
    19-21 Jan. 2006
  • Lastpage
    1281
  • Abstract
    The 6-DOF simulation system has many error factors. To reduce error magnitude and raise simulation precision, the error model is established. By analyzing the basic rules of system with error, the composing method of characteristic matrix can be put forward. Based on characteristic matrix and multi-body kinematics, synthesis error model including static and dynamic errors are obtained. The dynamic response and vibration of beam, which is subjected to a moving table, is chiefly analyzed. Based on Timoshenko´s beam theory and Euler-Lagrange equation, the equations of motion for the beam system, which are composed of translation errors and rotation errors of beam, are obtained. This method can offer academic reference to error synthesis model and compensation for 6-DOF simulation system
  • Keywords
    beams (structures); error analysis; kinematics; motion control; vibrations; 6-DOF simulation system; Euler-Lagrange equation; Timoshenko beam; beam system; beam theory; characteristic matrix; error factors; error synthesis model; motion equations; multibody kinematics; rotation errors; translation errors; vibration analysis; Analytical models; Computational modeling; Computer errors; Computer simulation; Equations; Error analysis; Kinematics; Manufacturing; Missiles; Motion analysis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    0-7803-9395-3
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2006.1627520
  • Filename
    1627520