Table 23 Comparison of the best solution for pressure vessel design found by different methods.
From: Enhancing grasshopper optimization algorithm (GOA) with levy flight for engineering applications
Algorithm | Optimal values for variables | f(x) | |||
|---|---|---|---|---|---|
x1 | x2 | x3 | x4 | ||
LFGOA | 0.7840 | 0.3875 | 40.6220 | 195.8397 | 5895.5481 |
SNS | 0.8125 | 0.4375 | 42.0985 | 176.6366 | 6059.7143 |
MOCoDE | 0.8125 | 0.4375 | 42.0984 | 176.6366 | 6059.7143 |
AHA | 0.7782 | 0.3847 | 40.3197 | 199.9993 | 5885.3537 |
MRFO | 0.7787 | 0.3849 | 40.3447 | 199.6516 | 5987.8131 |
ABC | 0.7782 | 0.3847 | 40.3211 | 199.9802 | 5885.4033 |
CPSOSA | 0.8125 | 0.4375 | 42.0984 | 176.6366 | 6059.7143 |
ADP_GA | 0.8125 | 0.4375 | 42.0968 | 176.6580 | 6059.9384 |
PSO_GRG | 0.8125 | 0.4375 | 42.0984 | 176.6366 | 6059.7144 |
SO | 0.7819 | 0.3857 | 40.5752 | 196.5499 | 5887.5298 |
