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Periodic Error Compensation for Quartz MEMS Gyroscope Drift of INS

机译:惯导的石英MEMS陀螺仪漂移的周期性误差补偿

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摘要

In order to improve the navigation accuracy of an inertial navigation system (INS), composed of quartz gyroscopes, the existing real-time compensation methods for periodic errors in quartz gyroscope drift and the periodic error term relationship between sampled original data and smoothed data are reviewed. On the base of the results, a new compensation method called using former period characteristics to compensate latter smoothness data (UFCL for short) method is proposed considering the INS working characteristics. This new method uses the original data without smoothing to work out an error conversion formula at the INS initial alignment time and then compensate the smoothed data errors by way of the formula at the navigation time. Both theoretical analysis and experimental results demonstrate that this method is able to cut down on computational time and raise the accuracy which makes it a better real-time compensation approach for periodic error terms of quartz micro electronic mechanical system (MEMS) gyroscope’s zero drift.

著录项

  • 来源
    《中国航空学报:英文版》 |2007年第6期|P.539-545|共7页
  • 作者单位

    College;

    of;

    Energy;

    and;

    Power;

    Engineering,;

    Huazhong;

    University;

    of;

    Science;

    and;

    Technology,;

    Wuhan;

    430074,;

    China;

    School;

    of;

    Instrument;

    Science;

    and;

    Opto-electronics;

    Engineering,;

    Beijing;

    University;

    of;

    Aeronautics;

    and;

    Astronautics,;

    Beijing;

    100083,;

    China;

    Mechanical;

    and;

    Electrical;

    Equipment;

    Research;

    Institute,;

    Qingdao;

    Navy;

    Submarine;

    Academe,;

    Qingdao;

    266071,;

    China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 CHI
  • 中图分类 航空;
  • 关键词

    时间补偿系统; 石英陀螺仪; 周期特性; 惯性导航系统;

    机译:时间补偿系统;石英陀螺仪;周期特性;惯性导航系统;
  • 入库时间 2022-08-19 04:18:17
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