International Journal of Aerospace Engineering / 2016 / Article / Tab 3

Research Article

Multiple Gravity Assist Spacecraft Trajectories Design Based on BFS and EP_DE Algorithm

Table 3

Value range of each variable in GTOC1.

(MJD2000) (d) (d) (d) (d) (d) (d) (d)

Min300014141414100366300
Max100002000200020002000900090009000

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