A Two-Step Approach for Airborne Delay Minimization Using Pretactical Conflict Resolution in Free-Route Airspace

Table 10

The delayed aircraft vector deflection model fuel consumption (kg).

Scenario Number	20 Aircraft			25 Aircraft
	Baseline	GA-based	TS-based	Baseline	GA-based	TS-based
1	182.28	0	0	439.03	11.9	11.9
2	638.64	1.9	1.9	354.47	10.7	10.7
3	170.69	0.6	0.6	8.23	0	0
4	53.12	0	0	384.05	91	105.5
5	16.78	0	0	11.41	0	0
6	0	0	0	152.33	17	17
7	18.3	0	0	452.02	24.6	24.6
8	403.88	83.6	83.6	211.66	31.4	31.4
9	95.19	0	0	127.42	5.4	5.4
10	64.43	0	0	16.42	0	0
11	90.57	0	0	331.98	0	0
12	103.62	20.9	20.9	170.02	12.58	12.58
13	473.5	20.1	20.1	197.55	15.7	15.7
14	498.86	15.2	15.3	699.73	138	158.9
15	568.93	7.1	7.1	235.45	50.4	50.4
16	106.74	0	0	439.81	14.5	14.5
17	50.96	0	0	430.29	32.4	35.8
18	618.74	12.6	12.6	86.38	0	0
19	39.42	8.3	8.3	367.17	40.9	55.01
20	0	0	0	270.53	0	0
21	444.4	25.2	25.2	260.96	0	0
22	141.64	0	0	198.04	15.7	15.7
23	11.76	0	0	74.39	0	0
24	60.5	0	0	398.77	0	0
25	276.37	47.9	49.3	105.24	16.2	8.8
26	66.59	12.5	12.5	188.11	0	0
27	146.51	9.3	9.3	564.78	89.8	94.4
28	261.83	9.4	9.4	600.61	115.6	115.6
29	437.79	4.7	4.7	7.09	0	0
30	0	0	0	249.33	0	0