DocumentCode
3020179
Title
Quadrature control principle of hemispherical resonator gyro
Author
Zhao Hongbo ; Ren Shunqing ; Wang Changhong
Author_Institution
Space Control & Inertial Technol. Res. Center, Harbin Inst. of Technol., Harbin, China
fYear
2013
fDate
20-22 Dec. 2013
Firstpage
479
Lastpage
482
Abstract
The dynamics equations of resonator were established and the solutions of the dynamics equations under quadrature control mode and quasi quadrature control mode were achieved, then the relations between the excitation and the input angular rate were derived under both modes. By comparing and analyzing, the simplicity and the practicability of the quasi quadrature control mode were better than that of the quadrature control mode. Finally, the method of greatly improving HRG´s accuracy under quasi quadrature control was achieved.
Keywords
gyroscopes; motion control; physical instrumentation control; resonators; HRG accuracy; hemispherical resonator gyro; quadrature control principle; quasiquadrature control mode; resonator dynamics equations; Accuracy; Electrodes; Equations; Force; Harmonic analysis; Market research; Vibrations; density distribution nonuniformity; hemispherical resonator gyro; quadrature control;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on
Conference_Location
Shengyang
Print_ISBN
978-1-4799-2564-3
Type
conf
DOI
10.1109/MEC.2013.6885115
Filename
6885115
Link To Document