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多模型自校准Kalman滤波方法

杨海峰 王金娜 王宇翔

杨海峰, 王金娜, 王宇翔. 多模型自校准Kalman滤波方法[J]. 航空动力学报, 2024, 39(3):20220244 doi: 10.13224/j.cnki.jasp.20220244
引用本文: 杨海峰, 王金娜, 王宇翔. 多模型自校准Kalman滤波方法[J]. 航空动力学报, 2024, 39(3):20220244 doi: 10.13224/j.cnki.jasp.20220244
YANG Haifeng, WANG Jinna, WANG Yuxiang. Multiple-model self-calibration Kalman filter method[J]. Journal of Aerospace Power, 2024, 39(3):20220244 doi: 10.13224/j.cnki.jasp.20220244
Citation: YANG Haifeng, WANG Jinna, WANG Yuxiang. Multiple-model self-calibration Kalman filter method[J]. Journal of Aerospace Power, 2024, 39(3):20220244 doi: 10.13224/j.cnki.jasp.20220244

多模型自校准Kalman滤波方法

doi: 10.13224/j.cnki.jasp.20220244
基金项目: 国家自然科学基金面上项目(61972021)
详细信息
    作者简介:

    杨海峰(1993-),男,博士,主要从事滤波算法、自主导航、深空探测等方面的研究。E-mail:halfyang@buaa.edu.cn

  • 中图分类号: V448;O231

Multiple-model self-calibration Kalman filter method

  • 摘要:

    基于自校准Kalman滤波方法和多模型估计理论,针对工程实际中未知输入(如突风、故障和未知系统误差等)对系统状态方程的影响问题,提出了一种多模型自校准Kalman滤波方法。该方法同时采用自校准Kalman滤波和标准Kalman滤波进行运算,并根据贝叶斯定理自动分配两种方法滤波值的权重,通过加权融合得到最终的滤波结果。与自校准Kalman滤波方法相比,多模型自校准Kalman滤波方法既能有效地补偿非零未知输入的影响,又明显改善了系统在未知输入为零时的滤波精度,大量数值仿真结果表明该方法精度提升可达10%以上,具有更强的适应性和鲁棒性。

     

  • 图 1  状态误差比较

    Figure 1.  Comparison of state errors

    图 2  方均根误差比较

    Figure 2.  Comparison of RMSEs

    图 3  各维度状态误差比较

    Figure 3.  Comparison of state errors in two dimensions

    图 4  各维度方均根误差比较

    Figure 4.  Comparison of RMSEs in two dimensions

    表  1  方均根误差均值

    Table  1.   Mean of RMSEs

    方法方均根误差均值
    MSKF0.0372
    SKF0.0418
    KF0.1169
    下载: 导出CSV

    表  2  各维度方均根误差均值

    Table  2.   Mean of RMSEs in two dimensions

    方法方均根误差均值
    维度一维度二
    MSKF0.03350.0332
    SKF0.03550.0354
    KF0.09150.0920
    下载: 导出CSV
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出版历程
  • 收稿日期:  2022-04-24
  • 网络出版日期:  2023-09-14

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