• DocumentCode
    2630724
  • Title

    Vibration Analysis of Circle Truss of the Astromesh Deployable Antenna

  • Author

    Heping, Liu ; Ani, Luo ; Tongming, Zhang ; Yang, Li

  • Author_Institution
    Sch. of Mech. & Electr. Eng., Harbin Eng. Univ., Harbin, China
  • Volume
    3
  • fYear
    2011
  • fDate
    6-7 Jan. 2011
  • Firstpage
    1116
  • Lastpage
    1119
  • Abstract
    Characteristics vibration and stiffness of astromesh deployable antenna is mainly decided by circle truss. So vibration of circle truss is necessary to be analyzed. At first, analyze the structure of the astromesh deployable antenna, and set up mass matrix, stiffness matrix and force vector of link ending points with the method of finite unit. Then transforming-coordinate matrixes and expanding-coordinate matrixes are used to transform the matrixes and vectors. The repeated addition method is adopted to found the vibration equations of the whole system. The program in the software Matlab and simulation in the software Ansys are used to get the numerical results of theory analysis and check the correctness of theory analysis. The analysis makes the structure more reasonable.
  • Keywords
    matrix algebra; reflector antennas; supports; astromesh deployable antenna; circle truss; expanding-coordinate matrix; finite unit method; link ending points force vector; set up mass matrix; software Ansys; software Matlab; stiffness matrix; transforming-coordinate matrix; vibration analysis; Analytical models; Antennas; Equations; Force; Mathematical model; Shape; Vibrations; Deployable antenna; Mode shape; Natural frequency; Vibration;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Measuring Technology and Mechatronics Automation (ICMTMA), 2011 Third International Conference on
  • Conference_Location
    Shangshai
  • Print_ISBN
    978-1-4244-9010-3
  • Type

    conf

  • DOI
    10.1109/ICMTMA.2011.847
  • Filename
    5721684