Asteroid Rendezvous Mission Design Using Multiobjective Particle Swarm Optimization

Table 6

MOPSO-II performance with different parameters (Cases  6 and  8).

Test problem	Algorithm	Epsilon			Hybervolume
		Mean	std	P value	Mean	std	P value
Asteroid 1,; three-impulse	Case  6	0.006045	0.002645	0.4727	0.99544	0.000816	0.0757
	Case  8	0.007806	0.004042		0.994456	0.001074