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Mathematical Problems in Engineering
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2015
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Article
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Tab 2
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Research Article
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