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
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