Asteroid Rendezvous Mission Design Using Multiobjective Particle Swarm Optimization

Table 3

MOPSO performance with different boundary constraint optimization.

Test problem	Algorithm	Epsilon			Hybervolume
		Mean	std	P value	Mean	std	P value
Asteroid 1,; two-impulse	MOPSO-I	0.011987	0.008378	0.1620	0.972618	0.006829	0.0257
	MOPSO-II	0.006833	0.004066		0.977958	0.001301
Asteroid 2,; three-impulse	MOPSO-I	0.025630	0.0278051	0.1620	0.87509	0.308357	0.6232
	MOPSO-II	0.0399274	0.026254		0.968537	0.016548