Journals Articles Conferences News About CLP
Submit a paper Email Alert
Search
Search
Articles
Journals
News
Advanced Search
Top Searches
2D MaterialsTransformation opticsQuantum PhotonicsSmall lasersSemiconductor UV PhotonicsSupersymmetric microring laser arrays

Laser & Optoelectronics Progress, Volume. 56, Issue 18, 180301(2019)

Minor Damage Location Method for Aircraft Skins Based on Marked Honeycomb Model

Zhijing Yu1, Xin Li1, Yanling Li1, Zechuan Li2, and Jingchang Zhuge1、*
Author Affiliations
  • 1 Electronic Information and Automation College, Civil Aviation University of China, Tianjin 300300, China
  • 2 Aeronautical Engineering College, Civil Aviation University of China, Tianjin 300300, China
    • show less
    AbstractGet PDF(in Chinese)
    Figures&Tables (14)
    Equations (0)
    References (16)
    Cited By (1)
    Tools
    Paper Information
    Topics
    Figures & Tables(14)
    Basic point transfer model of honeycomb model

    Fig. 1. Basic point transfer model of honeycomb model

    Download full size
    RRT reflective marks

    Fig. 2. RRT reflective marks

    Download full size
    Pixel edge of feature control point

    Fig. 3. Pixel edge of feature control point

    Download full size
    Radial grayscale gradient

    Fig. 4. Radial grayscale gradient

    Download full size
    Subpixel edge point

    Fig. 5. Subpixel edge point

    Download full size
    Diagram of projection of circular inscribed hexagon

    Fig. 6. Diagram of projection of circular inscribed hexagon

    Download full size
    Cross ratio invariance principle in hexagon

    Fig. 7. Cross ratio invariance principle in hexagon

    Download full size
    Diagram of experimental device

    Fig. 8. Diagram of experimental device

    Download full size
    Schematic of experimental process

    Fig. 9. Schematic of experimental process

    Download full size
    Control point layout model of damaged skin

    Fig. 10. Control point layout model of damaged skin

    Download full size
    Damage to surface of aircraft skin. (a) Normal skin; (b) crack; (c) corrosion; (d) strike; (e) scratch

    Fig. 11. Damage to surface of aircraft skin. (a) Normal skin; (b) crack; (c) corrosion; (d) strike; (e) scratch

    Download full size
    3×3 template images after adaptive median filtering. (a) Normal; (b) crack; (c) corrosion; (d) strike; (e) scratch

    Fig. 12. 3×3 template images after adaptive median filtering. (a) Normal; (b) crack; (c) corrosion; (d) strike; (e) scratch

    Download full size
    Error values and time consumptions of three algorithms. (a) Error in image; (b) time consumption; (c) relative truth error

    Fig. 13. Error values and time consumptions of three algorithms. (a) Error in image; (b) time consumption; (c) relative truth error

    Download full size

    • Table 1. Center coordinate results of four groups of control points under three different methodspixel

      View table

      Table 1. Center coordinate results of four groups of control points under three different methodspixel

      Experimental groupPositioning methodData resultTheoretical optimal value
      1Honeycomb model location method(1157.38,1349.27)(1156.95,1348.94)(1157.73,1350.12)(1158.08,1349.23)(1157.64,1348.75)
      Method in Ref. [11](581.82,349.36)(582.24,350.03)(581.43,348.97)(581.12,348.62)(582.42,350.37)
      Method in Ref. [9](217.60,145.39)(216.92,144.88)(217.05,144.98)(217.83,145.64)(218.85,146.38)
      2Honeycomb model location method(597.60,344.36)(597.82,344.57)(598.05,343.98)(596.89,345.35)(597.64,344.25)
      Method in Ref. [11](1851.03,1247.87)(1851.37,1248.24)(1850.72,1247.48)(1851.65,1248.56)(1852.76,1241.28)
      Method in Ref. [9](654.78,864.63)(655.21,865.02)(655.68,865.43)(654.38,864.19)(665.68,875.13)
      3Honeycomb model location method(800.16,675.26)(799.89,675.03)(799.60,674.69)(801.75,675.57)(800.37,674.96)
      Method in Ref. [11](514.76,483.87)(515.09,484.23)(515.46,484.61)(515.78,484.97)(525.09,481.23)
      Method in Ref. [9](1264.53,1027.86)(1264.87,1028.22)(1265.33,1028.76)(1265.69,1029.14)(1267.74,1030.12)
      4Honeycomb model location method(1697.61,1144.36)(1698.10,1144.77)(1697.32,1145.16)(1696.95,1143.84)(1697.43,1144.27)
      Method in Ref. [11](1456.47,987.39)(1456.68,987.63)(1456.89,987.87)(1457.12,988.23)(1466.18,980.63)
      Method in Ref. [9](1733.64,1368.59)(1734.12,1368.93)(1734.44,1369.29)(1733.23,1368.27)(1745.22,1370.47)
    Tools

    Get Citation

    Copy Citation Text

    Zhijing Yu, Xin Li, Yanling Li, Zechuan Li, Jingchang Zhuge. Minor Damage Location Method for Aircraft Skins Based on Marked Honeycomb Model[J]. Laser & Optoelectronics Progress, 2019, 56(18): 180301

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Set citation alerts for article
    Save article for my favorites
    Paper Information

    Category: COHERENCE OPTICS AND STATISTICAL OPTICS

    Received: Jan. 21, 2019

    Accepted: Apr. 9, 2019

    Published Online: Sep. 9, 2019

    The Author Email: Zhuge Jingchang (12315414@qq.com)

    DOI:10.3788/LOP56.180301

    Topics

    laser devices and laser physics
    Lasers and Laser Optics
    Laser physics
    laser manufacturing
    Instrumentation, Measurement and Metrology