• DocumentCode
    3589843
  • Title

    The research on three axis-six DOF disturbance force test technology and its application

  • Author

    Wei Han ; Jianyong Sun ; Dapeng Li ; Zhixian Chen

  • Author_Institution
    China Aero-Polytechnology Establ., Beijing, China
  • fYear
    2014
  • Firstpage
    674
  • Lastpage
    677
  • Abstract
    The spacecraft micro-vibration mechanical environment will have significant effect on the spacecraft performance. To research the micro-vibration influence, a new disturbance test technology is proposed based on FRF inverse theory. The technology can be used to measure three axis-six DOF disturbance forces of any moving parts on the satellite, so it can be applied to evaluate the vibration influence to the satellite environment. An application of the technology is given in the paper as an example. The technology will have broad application prospects in the field of space.
  • Keywords
    artificial satellites; dynamic testing; inverse problems; micromechanics; space vehicles; vibrations; FRF inverse theory; disturbance test technology; frequency response function inverse method; satellite environment; spacecraft microvibration mechanical environment; spacecraft performance; three axis-six DOF disturbance force test technology; three axis-six DOF disturbance forces; Calibration; Force; Force measurement; Satellites; Sensors; Space vehicles; Vibrations; disturbance force; mechanical environment; micro-vibration; test technology; three axis-six DOF;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability, Maintainability and Safety (ICRMS), 2014 International Conference on
  • Print_ISBN
    978-1-4799-6631-8
  • Type

    conf

  • DOI
    10.1109/ICRMS.2014.7107282
  • Filename
    7107282