Research Article
Reconstruction of Wing Structure Deformation Based on Particle Swarm Optimization Ridge Regression
Table 3
Test results of four displacement points (unit: mm).
| Load cases | Displacement measurement point (mm) | 1 | 2 | 3 | 4 |
| 1 | 5.54 | 5.66 | 4.24 | 4.37 | 2 | 11.68 | 11.56 | 8.76 | 8.76 | 3 | 11.72 | 11.98 | 8.46 | 8.19 | 4 | 18.98 | 19.24 | 12.83 | 12.69 | 5 | 26.19 | 25.91 | 16.90 | 17.06 | 6 | 5.64 | 5.78 | 4.35 | 4.11 | 7 | 11.77 | 11.94 | 8.68 | 8.59 | 8 | 11.80 | 11.65 | 8.39 | 8.51 | 9 | 18.93 | 18.90 | 12.72 | 12.72 | 10 | 26.20 | 26.02 | 16.81 | 16.74 | 11 | 5.39 | 5.56 | 4.18 | 4.32 | 12 | 11.82 | 11.84 | 8.73 | 8.99 | 13 | 11.77 | 11.76 | 8.37 | 8.09 | 14 | 18.99 | 18.74 | 12.76 | 12.78 | 15 | 26.13 | 25.98 | 16.84 | 16.69 | 16 | 5.51 | 5.35 | 4.28 | 4.24 | 17 | 17.44 | 17.60 | 12.92 | 12.71 | 18 | 17.66 | 17.44 | 12.55 | 12.37 | 19 | 28.20 | 28.43 | 18.96 | 18.73 | 20 | 38.69 | 38.58 | 25.33 | 25.39 | 21 | 62.32 | 62.05 | 42.22 | 42.50 | 22 | 62.45 | 62.67 | 42.26 | 42.05 | 23 | 62.40 | 62.64 | 42.29 | 42.11 | 24 | 63.41 | 63.23 | 44.02 | 43.94 | 25 | 63.53 | 63.81 | 44.15 | 44.14 | 26 | 63.20 | 63.12 | 43.93 | 44.02 | 27 | -27.08 | -26.68 | -20.07 | -20.14 | 28 | -52.38 | -51.88 | -37.24 | -36.89 | 29 | -17.76 | -17.84 | -12.93 | -12.85 | 30 | -24.17 | -23.62 | -17.05 | -17.42 | 31 | -47.50 | -48.35 | -32.24 | -31.98 | 32 | -37.89 | -38.26 | -25.69 | -25.33 | 33 | -39.71 | -39.53 | -25.53 | -25.55 | 34 | -26.80 | -26.51 | -17.14 | -17.24 |
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