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基于ASTSMO和UIO的故障估计方法

秦玉峰 史贤俊 翟禹尧 韩露 龙玉峰

秦玉峰, 史贤俊, 翟禹尧, 等 . 基于ASTSMO和UIO的故障估计方法[J]. 北京航空航天大学学报, 2020, 46(12): 2253-2263. doi: 10.13700/j.bh.1001-5965.2019.0631
引用本文: 秦玉峰, 史贤俊, 翟禹尧, 等 . 基于ASTSMO和UIO的故障估计方法[J]. 北京航空航天大学学报, 2020, 46(12): 2253-2263. doi: 10.13700/j.bh.1001-5965.2019.0631
QIN Yufeng, SHI Xianjun, ZHAI Yuyao, et al. Fault estimation method based on adaptive super-twisting sliding mode observer and unknown input observer[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(12): 2253-2263. doi: 10.13700/j.bh.1001-5965.2019.0631(in Chinese)
Citation: QIN Yufeng, SHI Xianjun, ZHAI Yuyao, et al. Fault estimation method based on adaptive super-twisting sliding mode observer and unknown input observer[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(12): 2253-2263. doi: 10.13700/j.bh.1001-5965.2019.0631(in Chinese)

基于ASTSMO和UIO的故障估计方法

doi: 10.13700/j.bh.1001-5965.2019.0631
详细信息
    作者简介:

    秦玉峰  男, 博士研究生。主要研究方向:飞行器检测与故障诊断技术

    史贤俊  男, 博士, 教授, 博士生导师。主要研究方向:飞行器测试性设计、故障检测与诊断

    翟禹尧  男, 博士研究生。主要研究方向:飞行器检测与故障诊断技术

    通讯作者:

    史贤俊, E-mail: sxjaa@sina.com

  • 中图分类号: TP273.2

Fault estimation method based on adaptive super-twisting sliding mode observer and unknown input observer

More Information
  • 摘要:

    针对系统在有未知干扰情况下的故障估计问题,提出一种基于自适应Super-Twisting滑模观测器(ASTSMO)和未知输入观测器(UIO)的故障估计方法。不需要已知故障导数的上界,避免了现有自适应算法存在的滑模增益过估计问题,并且能够处理多执行器同时发生故障的情况。首先,通过非奇异变换将原系统降阶为两个子系统,其中一个子系统只受故障的影响,另一个子系统同时含有故障和不确定干扰。对两个子系统分别设计ASTSMO观测器和UIO观测器,并对误差系统有限时间内收敛的条件进行了证明,同时给出了滑模增益初始值和时变增益的设计方法。然后,基于等效控制的概念对故障进行检测和估计。最后,通过仿真算例验证了所提故障估计方法的有效性。

     

  • 图 1  缓变故障的估计值与真实值

    Figure 1.  Estimated and true values of slow-varying fault

    图 2  发生缓变故障时的子系统1状态观测误差

    Figure 2.  State observation error of subsystem 1 when slow-varying fault occurs

    图 3  子系统2状态观测误差

    Figure 3.  State observation error of subsystem 2

    图 4  发生缓变故障时的k1自适应变化曲线

    Figure 4.  Adaptive change curves of k1 when slow-varying falut occurs

    图 5  发生缓变故障时的k2自适应变化曲线

    Figure 5.  Adaptive change curves of k2 when slow-varying falut occurs

    图 6  突变故障的估计值与真实值

    Figure 6.  Estimated and true values of sudden fault

    图 7  发生突变故障时的子系统1状态观测误差

    Figure 7.  State observation error of subsystem 1 when sudden fault occurs

    图 8  发生突变故障时的k1自适应变化曲线

    Figure 8.  Adaptive change curves of k1 when sudden fault occurs

    图 9  发生突变故障时的k2自适应变化曲线

    Figure 9.  Adaptive change curves of k2 when sudden fault occurs

    图 10  发生缓变故障时采用文献[15-18]方法的k1自适应变化曲线

    Figure 10.  Adaptive change curves of k1 of method in Refs.[15-18] when slow-varying fault occurs

    图 11  发生缓变故障时采用文献[15-18]方法的k2自适应变化曲线

    Figure 11.  Adaptive change curves of k2 of method in Refs.[15-18] when slow-varying fault occurs

    图 12  发生突变故障时采用文献[15-18]方法的k1自适应变化曲线

    Figure 12.  Adaptive change curves of k1 of method in Refs.[15-18] when sudden fault occurs

    图 13  发生突变故障时采用文献[15-18]方法的k2自适应变化曲线

    Figure 13.  Adaptive change curves of k2 of method in Refs.[15-18] when sudden fault occurs

    图 14  执行器同时发生故障时的故障估计结果

    Figure 14.  Fault estimations results for simultaneous actuator failures

    图 15  文献[21]方法的子系统1缓变故障状态观测误差

    Figure 15.  Subsystem 1 state observation error of method in Ref.[21] with slow-varying fault

    图 16  两种方法的缓变故障估计结果

    Figure 16.  Slow-varying fault estimation results of two methods

    图 17  文献[21]方法的子系统1突变故障状态观测误差

    Figure 17.  Subsystem 1 state observation error of method in Ref.[21] with sudden fault

    图 18  两种方法的突变故障估计结果

    Figure 18.  Sudden fault estimation results of two methods

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出版历程
  • 收稿日期:  2019-12-17
  • 录用日期:  2020-04-10
  • 网络出版日期:  2020-12-20

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