DocumentCode :
1721607
Title :
Research on the control loop for Solid Vibratory Gyroscope
Author :
Liu Ning ; Su Zhong ; Liu Hong
Author_Institution :
Sch. of Autom., Beijing Inst. of Technol., Beijing, China
fYear :
2013
Firstpage :
4963
Lastpage :
4968
Abstract :
This work presents the design, analysis, simulation of the control loop of Solid Vibratory Gyroscope (SVG). It can be used to measure the angular velocity of a rotating body based on the inertia effect of the standing wave in two vibration modes of the axisymmetric resonator. In order to reduce the response time, increase the response bandwidth and improve the sensitivity, it is necessary to design the gyroscope control loop and control strategy. A theoretical analysis on the traditional SVG is performed based on the ring model. To realize easily, the implementation modal is given. The typical structure of SVG control includes eight elements which are equally distributed around the circumference. The novel control loop based on the liner demodulator is introduced. It achieves the mode shape stability vibration used the control loop throughout the phase and amplitude of x and y. The numerical simulation is presented to verify the effectiveness of the proposed control scheme using the HRG parameters.
Keywords :
gyroscopes; numerical analysis; physical instrumentation control; vibrations; HRG parameters; SVG control loop analysis; SVG control loop simulation; angular velocity measure; axisymmetric resonator; inertia effect; liner demodulator; mode shape stability vibration; numerical simulation; response bandwidth; response time reduction; ring model; rotating body; solid vibratory gyroscope control loop; standing wave; vibration modes; Angular velocity; Demodulation; Force; Frequency control; Gyroscopes; Shape; Solids; Axisymmetric Resonator; Solid Vibratory Gyroscope; standing wave; vibratory gyroscope control loop;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6640301
Link To Document :
بازگشت