• DocumentCode
    2961500
  • Title

    Phase research of no-drive structure silicon micromachined gyroscope

  • Author

    Xu, X.S. ; Liu, H.L. ; Zhang, F.X.

  • Author_Institution
    Res. Centre of Sensor Technol., Beijing Inf. Sci. & Technol. Univ., Beijing
  • fYear
    2008
  • fDate
    5-8 Aug. 2008
  • Firstpage
    939
  • Lastpage
    942
  • Abstract
    The phase picking up technique of silicon micromachined gyroscope used for rotating carrier is introduced. When the sensitivity axis is parallel to the deflexion plane, silicon pendulum will get the biggest Coriolis force, and the outputs are the peak value of the sine wave. However, when the sensitivity axis is perpendicularity to the deflexion plane, the outputs are the zero value of the sine wave. The self-rotated signal of the carrier (accelerometer) as benchmark, comparing to the output signal phase of the carrier and the gyroscope, then subtract the lagged value from the phase difference of the accelerometer and the gyroscope, we can confirm the real deflecting direction of the carrier in the space.
  • Keywords
    Coriolis force; gyroscopes; micromachining; micromechanical devices; sensitivity analysis; Coriolis force; deflexion plane; no-drive structure silicon micromachined gyroscope; rotating carrier; sensitivity axis; silicon pendulum; Accelerometers; Angular velocity; Ceramics; Gas detectors; Gyroscopes; Information science; Signal processing; Silicon; Space technology; Structural beams;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation, 2008. ICMA 2008. IEEE International Conference on
  • Conference_Location
    Takamatsu
  • Print_ISBN
    978-1-4244-2631-7
  • Electronic_ISBN
    978-1-4244-2632-4
  • Type

    conf

  • DOI
    10.1109/ICMA.2008.4798884
  • Filename
    4798884