Laser & Optoelectronics Progress, Volume. 62, Issue 6, 0615003(2025)

Feature Vector-Based Coarse Registration Algorithm for Aircraft Blades

Zechuan Wang1、*, Zhenhua Zhang1, jin Liu1, and Haima Yang2
Author Affiliations
  • 1College of Electronic and Electrical Engineering, Shanghai University of Engineering Science, Shanghai 201620, China
  • 2School of Optical-Electrical and Computer Engineering, University of Shanghai for Science and Technology, Shanghai 200093, China
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    Figures & Tables(13)
    Rotation of feature vectors. (a) Initial position; (b) decentralization; (c) alignment of feature vectors
    Rotation of feature points. (a) Alignment of feature vectors; (b) alignment of feature points
    Point cloud scanning system
    Coarse registration results of rocket turbopump blades. (a) Initial blades; (b) proposed algorithm; (c) FPFH; (d) PCA; (e) 3DSC
    Precise registration results of rocket turbopump blades by ICP algorithm. (a) Proposed algorithm; (b) FPFH; (c) PCA; (d) 3DSC
    Coarse registration results of damaged compressor blades. (a) Initial blades; (b) proposed algorithm; (c) FPFH; (d) PCA; (e) 3DSC
    Precise registration results of damaged compressor blades by ICP algorithm. (a) Proposed algorithm; (b) FPFH; (c) PCA; (d) 3DSC
    Coarse registration results of different algorithms. (a) Time; (b) RMSE
    Precise registration results of different algorithms. (a) ICP Iterations; (b) RMSE
    • Table 1. Comparison of coarse registration results for rocket turbopump blades by different algorithms

      View table

      Table 1. Comparison of coarse registration results for rocket turbopump blades by different algorithms

      AlgorithmRMSE /mmTime /sDown sampling
      Proposed0.52178.66
      FPFH0.762652.7510000
      PCA0.505078.62160000
      3DSC1.8370250.8950000
    • Table 2. Comparison of precise registration results for rocket turbopump blades by different algorithms

      View table

      Table 2. Comparison of precise registration results for rocket turbopump blades by different algorithms

      AlgorithmRMSE /(10-3 mm)Time /sICP iterations
      Proposed algorithm+ICP2.226403.5820
      FPFH+ICP3.345596.4629
      PCA+ICP1.853380.2418
      3DSC+ICP33.540709.1535
    • Table 3. Comparison of coarse registration results for damaged compressor blades by different algorithms

      View table

      Table 3. Comparison of coarse registration results for damaged compressor blades by different algorithms

      AlgorithmRMSE /mmTime /sDown sampling
      Proposed0.523110.87
      FPFH0.793669.7512000
      PCA0.573885.72170000
      3DSC2.2750245.4850000
    • Table 4. Comparison of precise registration results for damaged compressor blades by different algorithms

      View table

      Table 4. Comparison of precise registration results for damaged compressor blades by different algorithms

      AlgorithmRMSE /(10-3 mm)Time /sICP iterations
      Proposed algorithm+ICP3.109464.5819
      FPFH+ICP4.065723.4629
      PCA+ICP3.784489.2420
      3DSC+ICP24.180857.1535
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    Zechuan Wang, Zhenhua Zhang, jin Liu, Haima Yang. Feature Vector-Based Coarse Registration Algorithm for Aircraft Blades[J]. Laser & Optoelectronics Progress, 2025, 62(6): 0615003

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    Paper Information

    Category: Machine Vision

    Received: Jun. 17, 2024

    Accepted: Aug. 20, 2024

    Published Online: Mar. 3, 2025

    The Author Email:

    DOI:10.3788/LOP241494

    CSTR:32186.14.LOP241494

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