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
Link To Document :
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