Asteroid Rendezvous Mission Design Using Multiobjective Particle Swarm Optimization

Table 7

MOPSO-II performance with different parameters (Cases  3,  5, and  7).

Test problem	Algorithm	Epsilon		Hybervolume
		Mean	std	Mean	std
Asteroid 1,; three-impulse	Case  3	0.00583413	0.0036399	0.994062	0.00135846
	Case  5	0.00438474	0.00129004	0.994755	0.00100777
	Case  7	0.00564449	0.00274183	0.994917	0.00119178