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
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