Acta Aeronautica et Astronautica Sinica ›› 2026, Vol. 47 ›› Issue (4): 232349.doi: 10.7527/S1000-6893.2025.32349
• Solid Mechanics and Vehicle Conceptual Design • Previous Articles
Haolei MOU1, Jia ZHANG2, Zhenyu FENG1(
), Chunyu BAI3
Received:2025-05-30
Revised:2025-07-03
Accepted:2025-07-28
Online:2025-07-31
Published:2025-07-30
Contact:
Zhenyu FENG
E-mail:caucstructure@163.com
Supported by:CLC Number:
Haolei MOU, Jia ZHANG, Zhenyu FENG, Chunyu BAI. Prediction of axial crushing response for CFRP thin-walled C-columns based on WOA-BP-LSTM autoencoder[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(4): 232349.
Table 4
Comparison between actual and reconstructed IPCF and EA values for 12 random samples in test set
| 样本 | IPCF/kN | EA/J | ||||
|---|---|---|---|---|---|---|
| 真实值 | 重建值 | 误差/% | 真实值 | 重建值 | 误差/% | |
| 1 | 32.75 | 33.00 | 0.77 | 1 396.33 | 1 388.91 | 0.53 |
| 2 | 27.08 | 27.82 | 2.72 | 1 124.41 | 1 133.20 | 0.78 |
| 3 | 27.51 | 27.62 | 0.42 | 1 092.41 | 1 098.68 | 0.57 |
| 4 | 46.61 | 46.64 | 0.06 | 1 505.54 | 1 488.62 | 1.12 |
| 5 | 29.70 | 29.94 | 0.81 | 1 162.46 | 1 171.61 | 0.79 |
| 6 | 22.85 | 22.68 | 0.73 | 478.99 | 474.58 | 0.92 |
| 7 | 29.29 | 29.15 | 0.49 | 1 122.19 | 1 096.37 | 2.30 |
| 8 | 41.95 | 42.19 | 0.57 | 1 430.47 | 1 434.60 | 0.29 |
| 9 | 33.26 | 33.48 | 0.68 | 1 237.73 | 1 241.88 | 0.34 |
| 10 | 21.58 | 21.99 | 1.89 | 1 097.71 | 1 094.41 | 0.30 |
| 11 | 34.65 | 34.69 | 0.13 | 1 286.87 | 1 311.65 | 1.93 |
| 12 | 20.23 | 20.31 | 0.35 | 511.62 | 509.47 | 0.42 |
Table 5
Comparison between actual and predicted IPCF and EA values for 12 random samples in test set
| 样本 | IPCF/kN | EA/J | ||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 真实值 | BP-LSTM自编码器预测值 | 误差/% | WOA-BP-LSTM自编码器预测值 | 误差/% | 真实值 | BP-LSTM自编码器预测值 | 误差/% | WOA-BP-LSTM自编码器预测值 | 误差/% | |
| 1 | 33.26 | 33.53 | 0.83 | 33.52 | 0.80 | 1 237.73 | 1 278.03 | 3.26 | 1 256.6 | 1.53 |
| 2 | 23.89 | 22.31 | 6.61 | 22.88 | 4.21 | 1 009.58 | 808.18 | 19.95 | 1 021.43 | 1.17 |
| 3 | 28.66 | 26.60 | 7.16 | 27.17 | 5.18 | 1 154.32 | 1 120.60 | 2.92 | 1 143.83 | 0.91 |
| 4 | 22.94 | 24.68 | 7.60 | 23.71 | 3.34 | 1 157.65 | 1 172.38 | 1.27 | 1 154.17 | 0.30 |
| 5 | 33.04 | 34.31 | 3.84 | 33.55 | 1.56 | 1 289.85 | 1 306.47 | 1.29 | 1 299.45 | 0.74 |
| 6 | 27.51 | 26.31 | 4.36 | 26.81 | 2.54 | 1 092.41 | 1 099.62 | 0.66 | 1 090.98 | 0.13 |
| 7 | 33.05 | 33.94 | 2.70 | 33.54 | 1.47 | 1 341.59 | 1 332.72 | 0.66 | 1 342.94 | 0.10 |
| 8 | 20.23 | 20.15 | 0.43 | 21.76 | 7.53 | 511.62 | 586.77 | 14.69 | 534.66 | 4.50 |
| 9 | 46.61 | 45.49 | 2.42 | 45.68 | 2.02 | 1 505.54 | 1 511.12 | 0.37 | 1 509.78 | 0.28 |
| 10 | 24.68 | 22.47 | 8.97 | 22.99 | 6.86 | 450.82 | 526.26 | 16.73 | 453.79 | 0.66 |
| 11 | 34.07 | 33.69 | 1.10 | 33.86 | 0.61 | 1 323.26 | 1 310.19 | 0.99 | 1 302.55 | 1.56 |
| 12 | 41.95 | 43.45 | 3.56 | 43.02 | 2.53 | 1 430.47 | 1 438.79 | 0.58 | 1 435.12 | 0.32 |
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