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
Link To Document :
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