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A SINS/BDS Integrated Navigation Method Based on Classified Weighted Adaptive Filtering

机译:基于分类加权自适应滤波的SINS / BDS集成导航方法

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摘要

Aiming at the problem that the accuracy and stability of SINS/BDS integrated navigation system decrease due to uncertain model and observation anomalies, a SINS/BDS integrated navigation method based on classified weighted adaptive filtering is proposed. Firstly, the innovation covariance matching technology is used to detect whether there is any abnormality in the system as a whole. Then the types of anomalies are distinguished by hypothesis test. Different types of anomalies have different effects on state estimation. Based on the dynamic changes of innovation, different adaptive weighting methods are adopted to correct navigation information. The simulation results show that this method can effectively improve the fault-tolerant performance of integrated navigation system in complex environment with unknown anomaly types. When both model anomalies and observation anomalies exist, the speed and position accuracy are increased by 42% and 24% compared with the standard KF, 38% and 22% compared with the innovation orthogonal adaptive filtering, which has higher navigation accuracy.
机译:旨在解决SINS / BDS综合导航系统由于不确定的模型和观察异常而降低的问题,提出了基于分类加权自适应滤波的SINS / BDS集成导航方法。首先,创新协方差匹配技术用于检测系统中是否存在异常。然后通过假设试验来区分异常类型。不同类型的异常对状态估计有不同的影响。基于创新的动态变化,采用了不同的自适应加权方法来纠正导航信息。仿真结果表明,该方法可以有效地提高综合导航系统在复杂环境中的容错性能,具有未知异常类型。当存在模型异常和观察异常时,与标准KF相比,速度和位置精度增加了42%和24%,与创新正交自适应滤波相比,38%和22%,具有更高的导航精度。

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  • 来源
    《Mathematical Problems in Engineering》 |2019年第15期|23.1-23.6|共6页
  • 作者单位

    Air Force Engn Univ Grad Coll Xian Shaanxi Peoples R China;

    Air Force Engn Univ Air & Missile Def Coll Xian Shaanxi Peoples R China;

    Air Force Engn Univ Grad Coll Xian Shaanxi Peoples R China;

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