Fully working mbh for two phase missions!
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@@ -6,7 +6,7 @@
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# Test the optimizer for a one-phase mission
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# The lambert's solver said this should be pretty valid
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launch_window = [DateTime(1992,11,1), DateTime(1992,12,1)]
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launch_window = DateTime(1992,11,1), DateTime(1992,12,1)
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latest_arrival = DateTime(1993,6,1)
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leave, arrive = DateTime(1992,11,19), DateTime(1993,4,1)
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test_leave = DateTime(1992,11,12)
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@@ -25,7 +25,7 @@
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# Now we can look at a slightly more complicated trajectory
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flybys = [Earth, Venus, Mars]
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launch_window = [DateTime(2021,10,1), DateTime(2021,12,1)]
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launch_window = DateTime(2021,10,1), DateTime(2021,12,1)
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latest_arrival = DateTime(2023,1,1)
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dates = [DateTime(2021,11,1), DateTime(2022,3,27), DateTime(2022,8,28)]
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phases = Vector{Phase}()
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@@ -45,7 +45,7 @@
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# Here is the final, most complicated, trajectory to test
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flybys = [Earth, Venus, Earth, Mars, Earth, Jupiter]
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launch_window = [DateTime(2023,1,1), DateTime(2024,1,1)]
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launch_window = DateTime(2023,1,1), DateTime(2024,1,1)
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latest_arrival = DateTime(2031,1,1)
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dates = [DateTime(2023,5,23),
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DateTime(2023,10,21),
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