Multiobjective Mission Planning for Multiple Geosynchronous Spacecraft Refueling

Table 2

Pareto-optimal solutions of cases 1-4.

(a)

Case	Outer-loop optimization variables
			(day)	(deg)	(deg)	(deg)
1	(1, 7, 3, 10, 9, 2, 4, 8, 6, 5)	/	(8, 13, 11, 8, 11, 9, 10, 10)	3.67	119.39	59.64
2	(10, 3, 1, 7, 8, 2, 4, 5, 6, 9)	/	(8, 10, 8, 12, 10, 11, 9, 12)	(6.88, 2.01)	(121.84, 240.95)	(199.97, 154.15)
3	(3, 10, 9, 8, 2, 4, 1, 7, 5, 6)	(4, 4)	(14, 9, 13, 9, 11, 12, 11, 11)	3.71	115.59	101.73
4	(7, 1, 3, 10, 2, 4, 5, 8, 6, 9)	(4, 4)	(10, 12, 12, 11, 11, 10, 13, 11)	(5.57, 1.54)	(105.12, 242.19)	(141.06, 179.48)

(b)

Case	Inner-loop optimization variable	Objective values
		(day)	(kg)
1	(0, 1, 0, 0, 1, 0, 1, 1)	80	2360.8
2	(1, 0, 0, 2, 2, 0, 0, 2)	80	2210.6
3	(0, 0, 1, 1, 0, 1, 0, 1)	45	2357.4
4	(1, 0, 0, 1, 0, 0, 2, 2)	45	2162.8