Modeling of Acceleration Influence on Hemispherical Resonator Gyro Forcing System

Author:

Yi Guoxing1,Xie Yangguang2,Qi Ziyang1,Xi Boqi1

Affiliation:

1. Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin 150001, China

2. Flight Automatic Control Research Institute, Aviation Industry Corporation of China, Xi’an 710065, China

Abstract

Acceleration adds negative effect to Hemispherical Resonator Gyro (HRG) output; therefore, it is important to model the influence and then make necessary compensations, accordingly. Based on the elastic thin-shell theory under the Kirchhoff-Love assumption, the acceleration influence on HRG forcing system is modeled and then schemes for incentive are suggested. Firstly, the dynamic model of resonator is introduced. Then, inertial load and electrostatic force are calculated to obtain the deformation of resonator. At last, schemes for pickoff incentive are proposed to weaken the effect of acceleration on HRG forcer. The simulation results illustrate that acceleration has negative effects on the exciting confidents of forcers and the proposed scheme can eliminate the acceleration influence on forcing system.

Publisher

Hindawi Limited

Subject

General Engineering,General Mathematics

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