Mathematical Problems in Engineering

Research Article

Improved Reliability-Based Optimization with Support Vector Machines and Its Application in Aircraft Wing Design

Table 1

Results of the mathematical example.
 ErrorSORAErrorSVM
SORA−0.6380−0.63801.2763.45 × 10−41.00 × 10−33.48 × 10−4189.9%0.8%
SORA + SVM10.15900.1590−0.3181.01 × 10−32.78 × 10−39.74 × 10−4177.2%3.5%
SORA + SVM20.16150.1615−0.32301.02 × 10−32.79 × 10−31.00 × 10−3173.53%−1.96%
SORA + SVM30.17030.1703−0.34071.05 × 10−32.89 × 10−31.01 × 10−3175.24%−3.81%
SORA + SVM40.14370.1437−0.28740.94 × 10−32.58 × 10−31.00 × 10−3174.47%6.38%
SORA + SVM50.15090.1509−0.30170.97 × 10−32.66 × 10−31.00 × 10−3173.10%2.67%