Fireworks Algorithm Applied to Trajectory Design for Earth to Lunar Halo Orbits

What is it about?

In this paper, a new application of heuristic optimization is applied to calculate the transfer from LEO to lunar halo orbits in a systematic approach. It allows people to design mission in a straightforward way, by simply specifying the altitude of LEO and z-amplitude of halo orbits. Its results are compared with existing methods to ensure its efficiency and accuracy.

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