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Error outlier with weighted Median Absolute Deviation threshold algorithm and FBG sensor based impact localization on composite wing structure

机译:加权中值绝对偏差阈值算法和基于FBG传感器的冲击定位在复合机翼结构上的异常值

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摘要

In this paper, a low velocity impact localization algorithm based on an error outlier assessment technique with weighted Median Absolute Deviation (MAD) threshold was developed to localize impact on complex composite structures. The error outlier with MAD threshold algorithm was used to localize impacts on a 1000 mm x 1400 mm area of the upper and lower surfaces of a Jabiru UL-D composite wing. Impact monitoring was performed with three multiplexed FBG sensors and the data acquisition was done using SFI-710 high speed interrogator to obtain the impact response signal at a frequency of 100 kHz. The weighted MAD threshold used to filter the likely impact locations from a set of detected locations, and the proposed algorithm was able to localize impacts with consistent overall performance for a varying number of allowed detected locations. A parametric study was also performed to determine the possibility of localizing impact using a single sensor. The feasibility of utilizing the error outlier with weighted MAD threshold algorithm to localize impact with a single sensor was effectively demonstrated. Overall, impacts on the upper and lower surface of the composite wing were predicted and the localization results for three and one FBG sensors were comparable. (C) 2017 Elsevier Ltd. All rights reserved.
机译:本文提出了一种基于误差离群值评估技术的低速冲击定位算法,该算法采用加权中位数绝对偏差(MAD)阈值来定位对复杂复合结构的影响。使用MAD阈值算法的异常值来确定对Jabiru UL-D复合机翼上下表面的1000 mm x 1400 mm区域的影响。使用三个多路FBG传感器进行冲击监测,并使用SFI-710高速询问器完成数据采集,以获取100 kHz频率的冲击响应信号。加权MAD阈值用于从一组检测到的位置中过滤出可能的影响位置,并且所提出的算法能够针对变化数量的允许检测到的位置以一致的整体性能来定位影响。还进行了参数研究,以确定使用单个传感器定位冲击的可能性。有效地证明了使用误差异常值和加权MAD阈值算法通过单个传感器来定位影响的可行性。总体而言,可以预测对复合机翼上,下表面的撞击,并且三个和一个FBG传感器的定位结果具有可比性。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Composite Structures》 |2017年第11期|412-419|共8页
  • 作者单位

    Korea Adv Inst Sci & Technol, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea;

    Korea Adv Inst Sci & Technol, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea;

    Korea Adv Inst Sci & Technol, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea;

    Korea Adv Inst Sci & Technol, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Acoustic emission; Composite wing; FBG; Impact localization; SHM;

    机译:声发射;复合翼;FBG;冲击定位;SHM;

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