International Journal of Aerospace Engineering / 2016 / Article / Tab 10

Research Article

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

Table 10

Relationship between width of partition and optimal value.

AlgorithmWidth (days)Optimal value (km/s)Independent runs

EP_DE204.930715
EP_DE164.930715
EP_DE124.930715
EP_DE84.930715

EP_PSO204.975
EP_PSO164.975
EP_PSO124.975
EP_PSO84.9385605

EP_GA205.835
EP_GA165.815
EP_GA125.805
EP_GA85.805

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