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