Research Article
Research on Optimization of Aircraft Climb Trajectory considering Environmental Impact
Table 3
Different weight combinations and optimization results.
| | | | Fitness | Optimization results | CO2 (kg) | NOx (kg) | V_var (kt) | Fuel (kg) | TE (°C) |
| 0.5 | 0.5 | 0 | 1.0111 | 14.5705 | 1245.8700 | 1.83391E − 12 | 3880.8850 | 27.2005 | 0.45 | 0.45 | 0.1 | 1.1166 | 3.7499 | 1243.8161 | 1.82226E − 12 | 3874.4873 | 27.3247 | 0.4 | 0.4 | 0.2 | 1.3247 | 1.7042 | 1249.4549 | 1.82663E − 12 | 3892.0520 | 27.5250 | 0.35 | 0.35 | 0.3 | 1.4347 | 0.8521 | 1247.0179 | 1.82473E − 12 | 3884.4609 | 27.4387 | 0.3 | 0.3 | 0.4 | 1.6726 | 0.5625 | 1253.0039 | 1.83254E − 12 | 3903.1073 | 27.5890 | 0.25 | 0.25 | 0.5 | 1.9890 | 1.4219 | 1251.0381 | 1.83032E − 12 | 3896.9838 | 27.5329 | 0.2 | 0.2 | 0.6 | 2.4717 | 1.4198 | 1246.6654 | 1.82466E − 12 | 3883.3627 | 27.4223 | 0.15 | 0.15 | 0.7 | 3.1743 | 2.7656 | 1250.4562 | 1.82972E − 12 | 3895.1711 | 27.5152 | 0.1 | 0.1 | 0.8 | 4.8133 | 1.2761 | 1263.3120 | 1.84806E − 12 | 3935.2170 | 27.8072 | 0.05 | 0.05 | 0.9 | 9.3217 | 1.0717 | 1254.1837 | 1.83389E − 12 | 3906.7823 | 27.6224 | 0 | 0 | 1 | 201.4523 | 0.5625 | 1245.7658 | 1.82241E − 12 | 3880.5604 | 27.4208 |
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