• DocumentCode
    3042161
  • Title

    Resonator fiber optic gyroscope with an all digitalized system

  • Author

    Yu, Xuhui ; Ma, Huilian ; Jin, Zhonghe

  • Author_Institution
    Dept. of Inf. Sci. & Electron. Eng., Zhejiang Univ., Hangzhou, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    815
  • Lastpage
    818
  • Abstract
    Resonator fiber optic gyroscope has the potential to achieve the inertial navigation system requirement with a short sensing coil. An all digitalized system is constructed including the signal modulation/demodulation and a proportional integral (PI) controller in a single field programmable gate array. Under this scheme, the serrodyne phase modulation technique is adopted, which is of benefit to overcome the backscattering induced noise and easy to implement in closed-loop operation. The phase modulation index is optimized to achieve high carrier suppression. The PI controller is adopted in the frequency servo loop to eliminate the residual error at the lock-in frequency. A bias stability of 5.2×10-4 rad/s in 500 seconds is demonstrated experimentally.
  • Keywords
    PI control; fibre optic gyroscopes; inertial navigation; phase modulation; resonators; all digitalized system; frequency servo loop; inertial navigation system requirement; phase modulation index; proportional integral controller; resonator fiber optic gyroscope; serrodyne phase modulation technique; short sensing coil; signal demodulation; signal modulation; single field programmable gate array; Frequency control; Frequency modulation; Optical fibers; Optical ring resonators; Phase modulation; Resonant frequency;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5633090
  • Filename
    5633090