Multiaircraft Optimal 4D Trajectory Planning Using Logical Constraints

Table 3

Boundary conditions for Experiment 2.

Symbol	Unit	Aircraft 1	Aircraft 2	Aircraft 3
	m	7400	7400	7400
	m	3350	3350	3350
	deg	39.000	39.000	38.701
	deg	40.575	40.575	40.848
	deg	-5.327	-3.325	-4.320
	deg	-3.430	-5.215	-4.320
	m/s	130	130	130
	m/s	110	110	110
	deg	0	0	0
	deg	0	0	0
	deg	356	294	294
	kg	65000	65000	65000