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跨介质航行器旋翼出入水感知及损伤监测

薄夫森 潘登 方子怡 付博玮 李寒阳 刘志海

薄夫森, 潘登, 方子怡, 等. 跨介质航行器旋翼出入水感知及损伤监测[J]. 水下无人系统学报, 2026, 34(5): 1-14 doi: 10.11993/j.issn.2096-3920.2026-0045
引用本文: 薄夫森, 潘登, 方子怡, 等. 跨介质航行器旋翼出入水感知及损伤监测[J]. 水下无人系统学报, 2026, 34(5): 1-14 doi: 10.11993/j.issn.2096-3920.2026-0045
Bo Fusen, Pan Deng, Fang Ziyi, Fu Bowei, Li Hanyang, Liu Zhihai. Entry-Exit Water Perception and Damage Monitoring of Rotors for Cross-Media Vehicle[J]. Journal of Unmanned Undersea Systems. doi: 10.11993/j.issn.2096-3920.2026-0045
Citation: Bo Fusen, Pan Deng, Fang Ziyi, Fu Bowei, Li Hanyang, Liu Zhihai. Entry-Exit Water Perception and Damage Monitoring of Rotors for Cross-Media Vehicle[J]. Journal of Unmanned Undersea Systems. doi: 10.11993/j.issn.2096-3920.2026-0045

跨介质航行器旋翼出入水感知及损伤监测

doi: 10.11993/j.issn.2096-3920.2026-0045
详细信息
    作者简介:

    李寒阳(1982-),男, 副教授, 主要研究方向为跨介质航行器、光学人工智能算法等

  • 中图分类号: TJ630; TB534+.3

Entry-Exit Water Perception and Damage Monitoring of Rotors for Cross-Media Vehicle

  • 摘要: 跨介质航行器旋翼在介质转换过程中, 因介质物理参数突变面临复杂瞬时应变问题, 长期交变载荷易引发桨叶微裂纹萌生、扩展甚至断裂, 严重威胁航行器运行可靠性与任务连续性。为解决旋翼出入水状态感知及损伤监测核心难题, 文中构建“信号采集-处理-特征提取-模型训练-状态感知”的完整技术体系: 实验装置通过导轨控制旋翼驱动结构出入水, 利用光纤光栅解调仪实时采集旋翼出入水全过程信号, 选取奇异点剔除法识别并剔除异常数据点, 完整保留信号入水、水中及出水特征, 通过图像转换保留时间序列的时间戳与幅度信息, 增强时间相关性特征并消除冗余, 而后将特征信号和转换图像用于模型训练。结果表明, 训练模型实现了跨介质航行器旋翼出入水状态的精准识别与实时损伤预警, 为航行器航线调整提供决策支持, 有效提升其智能感知与突防能力, 同时推动光学监测技术在跨介质航行器领域的深入应用。

     

  • 图  1  装置示意图

    Figure  1.  Device schematic

    图  2  非定常扰动

    Figure  2.  Unsteady disturbance

    图  3  中值滤波法处理非定常扰动

    Figure  3.  Median filtering method to deal with unsteady disturbance

    图  4  突变点检测法处理非定常扰动

    Figure  4.  The mutation point detection method deals with unsteady disturbances

    图  5  奇异值剔除法处理非定常扰动

    Figure  5.  Singular value elimination method to deal with unsteady disturbance

    图  6  三种方法定量指标对比

    Figure  6.  Comparison of quantitative indicators of three methods

    图  7  奇异值剔除法处理非定常扰动结果

    Figure  7.  The singular value elimination method is used to deal with the unsteady disturbance results

    图  8  无损伤旋翼特征信号图

    Figure  8.  Four characteristic signal diagrams of non-destructive rotor

    图  9  损伤旋翼四种特征信号图

    Figure  9.  Four characteristic signal diagrams of damaged rotor

    图  10  无损伤旋翼特征信号二维图像转换

    Figure  10.  Two-dimensional image conversion of non-destructive rotor characteristic signal

    图  11  损伤旋翼特征信号二维图像转换

    Figure  11.  Two-dimensional image conversion of damage rotor characteristic signal

    图  12  ResNet18结构图

    Figure  12.  Structure diagram of ResNet18

    图  13  最大池化的处理过程

    Figure  13.  Processing procedure of maximum pooling

    图  14  ResNet-18模型下旋翼训练/验证损失曲线和准确率曲线

    Figure  14.  Rotor training/verification loss curve and accuracy curve under ResNet-18 model

    图  15  VGG16模型下旋翼训练/验证损失曲线和准确率曲线

    Figure  15.  Rotor training/verification loss curve and accuracy curve under VGG16 model

    图  16  290 r/min转速下无损伤旋翼监测结果及数据

    Figure  16.  Monitoring results and data of non-destructive rotor at 290 r/min speed

    图  17  290 r/min转速下损伤旋翼监测结果及数据

    Figure  17.  Monitoring results and data of damaged rotor at 290 r/min speed

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  • 收稿日期:  2026-03-05
  • 修回日期:  2026-04-05
  • 录用日期:  2026-04-14
  • 网络出版日期:  2026-09-02
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