Multiaircraft Optimal 4D Trajectory Planning Using Logical Constraints

Table 1

Boundary conditions for Experiment 1 and Experiment 3.

Symbol	Unit	Aircraft 1	Aircraft 2	Aircraft 3
	m	7400	7000	7200
	m	3350	3350	3350
	deg	39.526	39.116	39.000
	deg	40.575	40.575	40.575
	deg	-5.327	-4.448	-3.325
	deg	-3.422	-3.422	-3.422
	m/s	130	130	130
	m/s	110	110	110
	deg	0	0	0
	deg	0	0	0
	deg	356	294	24
	kg	65000	65000	65000