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2022-04-18 10:59:25 -06:00
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LaTeX/conclusion.tex
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parameters. This makes the mission designer's job significantly simpler in that they can
simply explore a number of different flyby selection options in order to get a good
understanding of the mission scope and search space for a given spacecraft, launch window,
and target.
and target. The aim of this exploration was to examine whether a Monotonic Basin Hopping
algorithm utilizing an inner-loop NLP solver would be an appropriate choice for the
particular problem of low-thrust interplanetary trajectory optimization.
In performing this examination, two results were selected for further analysis. These
results are outlined in Table~\ref{results_table}. As can be seen in the table, both