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基于激励-校准法的硅微陀螺仪模态匹配控制电路研究

吴磊 杨波 王刚

传感技术学报2018,Vol.31Issue(3):363-367,5.
传感技术学报2018,Vol.31Issue(3):363-367,5.DOI:10.3969/j.issn.1004-1699.2018.03.008

基于激励-校准法的硅微陀螺仪模态匹配控制电路研究

Research on Mode-Matching Control Circuit for Micromechanical Silicon Gyroscope Based on Excitation-Calibration Alibration Technology

吴磊 1杨波 2王刚1

作者信息

  • 1. 东南大学仪器科学与工程学院,南京210096
  • 2. 东南大学微惯性仪表与先进导航技术教育部重点实验室,南京210096
  • 折叠

摘要

Abstract

A real-time mode-matching control circuit for micromechanical silicon gyroscope based on excitation-cali-bration method is presented in this paper.The symmetry characteristic of sense mode response is exploited by injecting excitation signals mixed with two pilot tones having specific frequencies into sense mode. The tuning voltage is ac-quired by calculating the amplitude difference between two response signals of pilot tones. The principle of frequency tuning technology based on electrostatic negative stiffness is reported at first.Then,the proposed mode-matching meth-od is presented and the introduced tuning error is analyzed. The mode-matching model built in Simulink verifies the feasibility of the proposed frequency tuning technology.The automatic mode-matching control circuit is designed based on FPGA. Experimental results indicate that zero bias stability decreases from 1.69°/h to 0.42°/h and the static per-formance is improved by 4.02 times. Angular random walk decreases from 0.046 °/ h to0.0195 °/ h and the static performance is improved by 2.36 times.

关键词

硅微陀螺仪/模态匹配/激励-校准/静电负刚度/零偏

Key words

micromechanical silicon gyroscope/mode-matching/excitation-calibration/electrostatic negative stiffness/zero bias

分类

航空航天

引用本文复制引用

吴磊,杨波,王刚..基于激励-校准法的硅微陀螺仪模态匹配控制电路研究[J].传感技术学报,2018,31(3):363-367,5.

基金项目

航空科学基金项目(20150869005) (20150869005)

传感技术学报

OA北大核心CSCDCSTPCD

1004-1699

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