Low-Thrust interplanetary trajectory

This forum is for discussing the implementation of low thrust optimization.

Low-Thrust interplanetary trajectory

Postby Albertillo » Tue Jul 31, 2018 1:30 pm


I am conducting a graduation thesis about mission analysis, and I thought about doing an interplanetary trajectory from Earth to Jupiter using low-thrust. I would like to optimize this trajectory's Delta V, but I don't really know how low-thrust optimization works in GMAT. Is there any type of guide or tutorial for this type of optimization? I searched on the internet but didn't find anything.
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