Research on Optimization of Aircraft Climb Trajectory considering Environmental Impact

Table 4

optimized result.

			Fitness	Optimized result			CO2 (kg)	NOx (kg)
				V_var (kt)	Fuel (kg)	TE (°C)
0	0.9	0.1	1.1398	0.0668	1247.5096	1.82E − 12	3885.9925	27.4615
0.1	0.8	0.1	1.1335	1.2812	1246.7496	1.82E − 12	3883.6251	27.4262
0.2	0.7	0.1	1.1302	0.4219	1247.2836	1.82E − 12	3885.2884	27.4511
0.3	0.6	0.1	1.1253	0.9063	1246.9776	1.82E − 12	3884.3351	27.4370
0.4	0.5	0.1	1.1208	0.9375	1246.9701	1.82E − 12	3884.3118	27.4363
0.45	0.45	0.1	1.1178	1.9359	1247.6833	1.83E − 12	3886.5336	27.4366
0.5	0.4	0.1	1.1151	2.9005	1245.4382	1.82E − 12	3879.5401	27.3727
0.6	0.3	0.1	1.1101	4.0345	1248.9455	1.83E − 12	3890.4653	27.4317
0.7	0.2	0.1	1.1062	4.0313	1248.6045	1.83E − 12	3889.4030	27.4239
0.8	0.1	0.1	1.1021	3.2396	1261.9236	1.85E − 12	3930.8919	27.7258