Research Article
Improved Reliability-Based Optimization with Support Vector Machines and Its Application in Aircraft Wing Design
Table 3
Reliability analysis of optimal solution.
| | | | | | | | | |
| | SORA + SVM1 | 0.99870 | 0.99869 | 1.30 × 10−3 | 1.31 × 10−3 | 1.36 × 10−3 | −4.41% | −3.68% | | SORA + SVM2 | 0.99870 | 0.99866 | 1.30 × 10−3 | 1.34 × 10−3 | 1.36 × 10−3 | −4.41% | −1.47% | | SORA + SVM3 | 0.99870 | 0.99871 | 1.30 × 10−3 | 1.29 × 10−3 | 1.36 × 10−3 | −4.41% | −5.15% | | SORA + SVM4 | 0.99870 | 0.99858 | 1.30 × 10−3 | 1.42 × 10−3 | 1.36 × 10−3 | −4.41% | 4.41% | | SORA + SVM5 | 0.99870 | 0.99870 | 1.30 × 10−3 | 1.30 × 10−3 | 1.36 × 10−3 | −4.41% | −4.41% |
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