Asteroid Rendezvous Mission Design Using Multiobjective Particle Swarm Optimization

Table 5

MOPSO-II performance with different parameters (Cases  2 and  4).

Test problem	Algorithm	Epsilon			Hybervolume
		Mean	std	P value	Mean	std	P value
Asteroid 1,; three-impulse	Case  2	0.010692	0.006797	0.6776	0.984063	0.002738	0.1405
	Case  4	0.012918	0.012848		0.985643	0.002736