Spacecraft Multiple-Impulse Trajectory Optimization Using Differential Evolution Algorithm with Combined Mutation Strategies and Boundary-Handling Schemes

Table 2

Impulse time and characteristic velocity of the best solution.

Algorithm	Impulses ( (s), (m/s))				(m/s)
	= 1	= 2	= 3	= 4
PSASM	(0, 391.48)	(2648.94, 236.51)	(10130.13, 235.83)	(12772.96, 392.50)	1256.32
DE_CMSBHS	(0, 392.55)	(2648.09, 235.59)	(10124.87, 235.59)	(12772.96, 392.55)	1256.27