• DocumentCode
    1857949
  • Title

    Design trade-offs of micromachined gyroscope concept allowing interchangeable operation in both robust and precision modes

  • Author

    Schofield, A.R. ; Trusov, A.A. ; Shkel, A.M.

  • Author_Institution
    Dept. of Mech. & Aerosp. Eng., Univ. of California, Irvine, CA, USA
  • fYear
    2009
  • fDate
    21-25 June 2009
  • Firstpage
    1952
  • Lastpage
    1955
  • Abstract
    This paper presents design trade-offs for a z-axis gyroscope allowing interchangeable operation in either precision or robust modes. This is enabled through a complete 2-DOF sense mode which allows the specification of the peak spacing and degree of coupling independent of frequency. Simulated sense mode frequency responses for various coupling amounts indicate that weakly coupled systems are desirable due to the larger precision mode gain increase (over 20 dB) for atmospheric pressure operation. Experimentally measured sense mode frequency responses for strong and weak coupling confirm the simulation results in air while also revealing that strong coupling is desirable at vacuum due to the increased precision mode gain improvement of over 40 dB while leaving the robust mode relatively unaffected.
  • Keywords
    frequency response; gyroscopes; micromechanical devices; atmospheric pressure operation; micromachined gyroscope; sense mode frequency responses; z-axis gyroscope; Atmospheric modeling; Bandwidth; Costs; Equations; Gyroscopes; Laboratories; Resonant frequency; Robustness; Suspensions; Vehicle dynamics; Mode-matching; Robustness; Vibratory gyroscope;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Solid-State Sensors, Actuators and Microsystems Conference, 2009. TRANSDUCERS 2009. International
  • Conference_Location
    Denver, CO
  • Print_ISBN
    978-1-4244-4190-7
  • Electronic_ISBN
    978-1-4244-4193-8
  • Type

    conf

  • DOI
    10.1109/SENSOR.2009.5285672
  • Filename
    5285672