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半球谐振陀螺零偏温度漂移的自补偿

刘吉利 李建朋 武志忠 李恺

空间控制技术与应用2018,Vol.44Issue(1):69-73,5.
空间控制技术与应用2018,Vol.44Issue(1):69-73,5.DOI:10.3969/j.issn.1674-1579.2018.01.010

半球谐振陀螺零偏温度漂移的自补偿

Self-Compensation of Bias Temperature Drift in Hemispherical Resonator Gyro

刘吉利 1李建朋 1武志忠 1李恺1

作者信息

  • 1. 北京控制工程研究所,北京100190
  • 折叠

摘要

Abstract

Variation of temperature has a strong effect on Hemispherical Resonator Gyro(HRG) output.In this paper,we propose a self-compensation scheme based on the drive-mode resonant frequency.The analysis of relationship between resonant frequency and temperature is used to illustrate the feasibility of frequency used as temperature.The bias temperature drift mode is established and the drive-mode resonant frequency is used to compensate the bias drift real timely.The resolution of the resonant frequency is 0.03 Hz which means a resolution of 0.075 ℃ for temperature.The self-compensation yielded a total bias error of 2.8 (o)/h over temperature range of-10 ℃ ~60 ℃,corresponding to a 30(°)/h bias error before compensation.These results show that the scheme is valid.

关键词

半球谐振陀螺/零偏漂移/自补偿

Key words

hemispherical resonator gyro/bias drift/self-compensation

分类

航空航天

引用本文复制引用

刘吉利,李建朋,武志忠,李恺..半球谐振陀螺零偏温度漂移的自补偿[J].空间控制技术与应用,2018,44(1):69-73,5.

基金项目

十三五核高基专项资助项目(2017ZX01013101-003).Supported by the 13th National Five Plan of CCS (2017ZX01013101-003). (2017ZX01013101-003)

空间控制技术与应用

OA北大核心CSCDCSTPCD

1674-1579

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