引用本文:李利亮,牛睿,邵志杰,沈毅.基于专用卡尔曼滤波器思想的陀螺故障诊断[J].控制理论与应用,2019,36(9):1501~1508.[点击复制]
LI Li-liang,NIU Rui,SHAO Zhi-jie,SHEN Yi.Gyroscope fault diagnosis based on dedicated Kalman filter scheme[J].Control Theory and Technology,2019,36(9):1501~1508.[点击复制]
基于专用卡尔曼滤波器思想的陀螺故障诊断
Gyroscope fault diagnosis based on dedicated Kalman filter scheme
摘要点击 1958  全文点击 875  投稿时间:2018-03-19  修订日期:2019-01-22
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DOI编号  10.7641/CTA.2019.80192
  2019,36(9):1501-1508
中文关键词  姿态确定系统  陀螺  故障检测与分离  卡尔曼滤波器
英文关键词  Attitude determination system  Gyroscope  Fault detection  Kalman filter
基金项目  国家自然科学基金
作者单位E-mail
李利亮 哈尔滨工业大学 lll163@yeah.net 
牛睿 上海航天控制技术研究所  
邵志杰 上海航天控制技术研究所  
沈毅* 哈尔滨工业大学 yishen_hit@126.com 
中文摘要
      本文针对卫星姿态确定系统, 提出了一种基于专用卡尔曼滤波器思想的陀螺故障诊断方法. 利用卫星姿态 运动方程设计了一种加性卡尔曼滤波器, 用于生成作为故障征兆信号的残差. 结合专用观测器思想和卡尔曼滤波 器, 提出了利用卡尔曼滤波器组的故障检测与分离律. 另外, 给出了一种基于3-σ的阈值计算方法, 用于设计故障诊 断中所用的检测阈值. 仿真结果验证了所提出方法的有效性.
英文摘要
      A gyroscope fault diagnosis method based on dedicated Kalman filter scheme is proposed for satellite attitude determination systems. Based on the attitude kinematics, an additive Kalman filter is designed to generate residuals, which are used as the symptom of fault. By integrating dedicated observer scheme and Kalman filter, a fault detection and isolation method using a bank of Kalman filters is proposed. In addition, a 3-σ based method is presented to generate the threshold used in fault diagnosis. Simulation results are given to verify the effectiveness of the proposed method.