• DocumentCode
    1590503
  • Title

    Quadrature control of Hemispherical Resonator Gyro based on FPGA

  • Author

    Yun, Li ; Bing, Luo ; Xu, Wang ; Wenqi, Wu

  • Author_Institution
    Coll. of Mechatron. Eng. & Autom., Nat. Univ. of Defense Technol., Changsha, China
  • Volume
    3
  • fYear
    2011
  • Firstpage
    369
  • Lastpage
    372
  • Abstract
    The quadrature drift mechanism of the Hemispherical Resonator Gyro is analyzed and its equation is deduced in order to suppress the quadrature drift. The resonator´s two vibration modes which have different frequencies and damping decay rates cause the quadrature drift. Furthermore, the drift caused by different damping decay rates can usually be reduced by calibration, but the drift caused by different frequencies only can be suppressed by the quadrature control loop. The phase error of the 0-degree and 45-degree vibration signals are employed to eliminate frequencies split with quadrature control loop. And the FPGA digital control loop is introduced. Experiments show that the quadrature drift can be suppressed effectively by using the method mentioned before.
  • Keywords
    damping; field programmable gate arrays; gyroscopes; inertial navigation; resonators; vibration control; FPGA; damping decay rates; digital control loop; hemispherical resonator gyro; quadrature control; quadrature drift mechanism; vibration modes; Damping; Electrodes; Field programmable gate arrays; Frequency control; Optical resonators; Resonant frequency; Vibrations; HRG; phase error; quadrature control loop; quadrature drift;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electronic Measurement & Instruments (ICEMI), 2011 10th International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4244-8158-3
  • Type

    conf

  • DOI
    10.1109/ICEMI.2011.6037926
  • Filename
    6037926