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半球谐振陀螺相位不均衡误差快速诊断与补偿方法

陈彤阳 李华 马圣杰 舒航 杨森 王育彬

陈彤阳,李华,马圣杰,等. 半球谐振陀螺相位不均衡误差快速诊断与补偿方法[J]. 北京航空航天大学学报,2026,52(8):2828-2835
引用本文: 陈彤阳,李华,马圣杰,等. 半球谐振陀螺相位不均衡误差快速诊断与补偿方法[J]. 北京航空航天大学学报,2026,52(8):2828-2835
Chen T Y,Li H,Ma S J,et al. A rapid diagnostic and compensation method for phase imbalance errors in hemispherical resonator gyroscopes[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(8):2828-2835 (in Chinese)
Citation: Chen T Y,Li H,Ma S J,et al. A rapid diagnostic and compensation method for phase imbalance errors in hemispherical resonator gyroscopes[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(8):2828-2835 (in Chinese)

半球谐振陀螺相位不均衡误差快速诊断与补偿方法

doi: 10.13700/j.bh.1001-5965.2025.0623
详细信息
    通讯作者:

    E-mail:lih292@avic.com

  • 中图分类号: V241.5;TP212

A rapid diagnostic and compensation method for phase imbalance errors in hemispherical resonator gyroscopes

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  • 摘要:

    针对半球谐振陀螺测控系统中两轴检测回路存在的相位不均衡误差,提出基于驻波自进动的陀螺相位不均衡误差快速诊断与补偿方法。通过观察恒速自进动时的正交控制力常值耦合量,得到共有相位误差补偿值,通过观察不同自进动速率下的正交控制力残差,得到差异相位误差补偿值,调整了两轴检测回路解调量的相位不均衡误差补偿值,消除了检测模态下控制力的相互耦合,使谐振子重新工作于谐振状态,降低了陀螺角度相关性零偏(ADB)峰峰值。实验表明:陀螺ADB峰峰值由15.56 (°)/h减小至0.71 (°)/h,降低了约22倍,验证了所提方法的有效性和正确性。

     

  • 图 1  半球谐振陀螺全角控制模型

    Figure 1.  Full-angle control model of hemispherical resonator gyroscope

    图 2  不同$ {\text{δ}} {\varphi }_{{\mathrm{cmp}}} $下的正交控制力均值

    Figure 2.  Mean value of orthogonal control forces under varying $ {\text{δ}} {\varphi }_{{\mathrm{cmp}}} $

    图 3  不同$ {\varepsilon }_{{\mathrm{p}}\_ {\mathrm{cmp}}} $下的正交控制力

    Figure 3.  Orthogonal control forces at different $ {\varepsilon }_{{\mathrm{p}}\_ {\mathrm{cmp}}} $

    图 4  不同$ {\varepsilon }_{{\mathrm{p}}\_ {\mathrm{cmp}}} $下的正交控制力残差

    Figure 4.  Residuals of orthogonal control forces at different $ {\varepsilon }_{{\mathrm{p}}\_ {\mathrm{cmp}}} $

    图 5  不同$ {\text{δ}} {\varphi }_{{\mathrm{cmp}}} $下陀螺的正交控制力均值

    Figure 5.  Mean of orthogonal control forces of gyroscope at different $ {\text{δ}} {\varphi }_{{\mathrm{cmp}}} $

    图 6  不同$ {\varepsilon }_{{\mathrm{p}}\_ {\mathrm{cmp}}} $下陀螺的正交控制力残差

    Figure 6.  Residuals of gyroscope’s orthogonal control forces at different $ {\varepsilon }_{{\mathrm{p}}\_ {\mathrm{cmp}}} $

    图 7  相位不均衡误差补偿前后ADB

    Figure 7.  Comparison of ADB before and after phase imbalance error compensation

    图 8  相位不均衡误差补偿前后高动态环境下ADB

    Figure 8.  ADB in high-dynamic environments before and after phase imbalance error compensation

    表  1  仿真参数设置

    Table  1.   Configuration of simulation parameters

    参数 数值
    高阻尼轴Q 1.3485×107
    低阻尼轴Q 1.3651×107
    频率裂解值$ \Delta \omega $/ mHz 0.3
    谐振频率$ \omega $ / Hz 7630.7
    采样率/ Hz 100
    x轴相位延迟/(°) 10
    y轴相位延迟/(°) 5
    下载: 导出CSV
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出版历程
  • 收稿日期:  2025-09-05
  • 录用日期:  2025-11-14
  • 网络出版日期:  2025-11-26
  • 整期出版日期:  2026-08-31

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