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

Table 5

The best result of each velocity increment from impulse/gravity assist.

Time (MJD2000)	Impulse/gravity assist	(km/s)
−780.150849	Departure impulse	3.275103
−649.698113	1st impulse	0.463213
−611.660883	Gravity assist by Venus	6.275954
−385.531004	2nd impulse	0.397884
−187.662661	Gravity assist by Venus	6.951561
−166.669404	3rd impulse	0.000000
−134.355766	Gravity assist by Earth	5.108686
−99.8160349	4th impulse	0.000000
455.4159571	Gravity assist by Jupiter	4.442469
2410.306944	5th impulse	0.000001
2655.415957	Rendezvous impulse	4.246699