Update for ky
This commit is contained in:
Connor
7
julia/test/genetic_algorithm.jl
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7
julia/test/genetic_algorithm.jl
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@@ -0,0 +1,7 @@
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@testset "Genetic Algorithm" begin
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println("Testing Genetic Algorithm")
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@test true
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end
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@@ -1,73 +0,0 @@
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@testset "Inner Loop" begin
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println("Testing Inner Loop")
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using Dates, SPICE, PlotlyJS
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sc = Sc("test")
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launch_date = DateTime(2016,3,28)
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launch_j2000 = utc2et(Dates.format(launch_date,"yyyy-mm-ddTHH:MM:SS"))
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leg1_tof = 3600*24*30*10.75
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leg2_tof = 3600*24*365*5.5
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v∞s = [ [0.34251772594197877, -2.7344726708862477, -1.1854707164631975],
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[-1.1, -3., -2.6],
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[3.5, 3.5, √(5^2 - 2*3.5^2)],
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[0.3, 1., 0.] ]
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p1 = "Mars"
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p2 = "Saturn"
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start_mass = 10_000.
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phase1 = Phase("Earth", p1, leg1_tof, v∞s[1], v∞s[2])
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phase2 = Phase(p1, p2, leg2_tof, v∞s[3], v∞s[4])
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# For finding the best trajectories
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earth_state = [spkssb(Thesis.ids["Earth"], launch_j2000, "ECLIPJ2000"); start_mass]
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p1_state = [spkssb(Thesis.ids[p1], launch_j2000+leg1_tof, "ECLIPJ2000"); start_mass]
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p2_state = [spkssb(Thesis.ids[p2], launch_j2000+leg1_tof+leg2_tof, "ECLIPJ2000"); start_mass]
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earth = prop(zeros(100,3), earth_state, sc, μs["Sun"], 3600*24*365.)[1]
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p1_path = prop(zeros(100,3), p1_state, sc, μs["Sun"], 3600*24*365*2.)[1]
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p2_path = prop(zeros(100,3), p2_state, sc, μs["Sun"], 3600*24*365*8.)[1]
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leg1, leg1_final = prop(zeros(400,3),
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earth_state+[zeros(3);v∞s[1];start_mass],
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copy(sc),
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μs["Sun"],
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leg1_tof)
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leg2, leg2_final = prop(zeros(400,3),
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p1_state+[zeros(3);v∞s[3];start_mass],
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copy(sc),
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μs["Sun"],
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leg2_tof)
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savefig(plot_orbits( [earth, p1_path, p2_path, leg1, leg2],
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primary="Sun",
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labels=["Earth", p1, p2, "Leg 1", "Leg 2"],
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title="Inner Loop without thrusting",
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colors=["#0000FF", "#FF0000", "#FFFF00", "#FF00FF", "#00FFFF"] ),
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"../plots/inner_loop_before.html")
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# The first leg should be valid
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fresh_sc = copy(sc)
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thrusts = inner_loop( launch_date,
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sc,
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start_mass,
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[phase1],
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verbose=true,
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mbh_specs=(25,50) )
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path, final = prop(thrusts[1], earth_state+[zeros(3);v∞s[1];0.0], Sc("test"), μs["Sun"], leg1_tof)
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@test final[1:6] ≈ p1_state[1:6] + [zeros(3); v∞s[2]]
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savefig(plot_orbits( [earth, p1_path, path],
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primary="Sun",
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labels=["Earth", p1, "Leg 1"],
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title="Inner Loop with thrusting",
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colors=["#0000FF", "#FF0000", "#FF00FF"] ),
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"../plots/inner_loop_after.html")
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# The second one was too hard to figure out on my own, so I'm letting it fail
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@test_throws ErrorException inner_loop( launch_date,
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sc,
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start_mass,
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[phase1, phase2],
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verbose=true,
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mbh_specs=(10,10) )
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end
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@@ -7,19 +7,19 @@ Spacecraft: bepi
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num_thrusters: 2
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duty_cycle: 0.9
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Launch Mass: 4000.0 kg
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Launch Date: 2022-03-06T01:59:18.919
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Launch V∞: [-1.1356413222408823, -4.788069365262547, 2.7000635369246] km/s
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Launch Date: 2024-08-10T04:39:14.851
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Launch V∞: [5.086503138635964, 5.7458326772994415, -0.07148502064229807] km/s
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Phase 1:
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Planet: Jupiter
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V∞_in: [0.606990343209641, 4.407893426470118, 0.9244860672598548] km/s
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V∞_out: [1.2183577357736917, -3.9826645468861925, 2.3687041043301797] km/s
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time of flight: 1.194581479969281e8 seconds
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arrival date: 2025-12-17T16:48:25.919
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thrust profile: [0.2047491180715187 -0.37019469041025893 -0.10453549807669095; 0.4301220091095493 -0.12441963747750297 -0.006770873233015344; 0.43924678986775806 0.1285374874465679 -0.07977271709638968; 0.42297198253230855 0.31380495510861767 -0.07919431310255642; 0.3614168205981836 0.39602843825488454 -0.05704653521018108; 0.2902414389460733 0.4053822027059241 -0.02821739799974643; 0.22430933743909634 0.43938508487263367 -0.00930631106824115; 0.13232647607691467 0.4188738913138919 0.007567873851875307; 0.054141732819826004 0.39551671259361465 0.010428460581952593; -0.012077434841877642 0.3792721276901153 0.0231446451624962; -0.042939891420425445 0.367704668401295 0.04590678245879779; -0.06832185713480624 0.39461571349444186 0.06647905984921844; -0.06871098668169624 0.3943544952193675 0.07996958584990013; -0.043122107121887 0.3236627227698529 0.06434542295394348; 0.0002258095938542581 0.3100245138960139 0.08315646808686966; 0.024384212213495196 0.1820219401839858 0.049878939508001104; 0.014803074731020839 0.09226807883171781 0.03031339291970727; 0.04882521682144194 0.07182823075104046 0.030435679401299; 0.07679479397181303 0.04220157719360384 0.024296177838332548; 0.07770574743624227 0.006328096858830944 0.01324607153162614] %
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V∞_in: [0.036227390916599315, 0.15967408190094506, 0.14767480118449552] km/s
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V∞_out: [0.02010676850789124, 0.050598467400280935, -0.04060341677187609] km/s
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time of flight: 2.2119244577042913e8 seconds
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arrival date: 2031-08-14T06:59:59.851
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thrust profile: [-0.03786142679064034 0.27339859122748333 0.0005726056795561895; -0.1960519532066938 0.1387630677841132 0.004600353091805394; -0.2161656001051881 0.03829454149587224 0.005463035319820266; -0.20722821473665434 -0.02785165286999182 0.00642011251062416; -0.19350969113180666 -0.07336980382318779 0.005798735353253219; -0.17166276097528518 -0.10180245936266212 0.0060229587041231505; -0.14580486341259447 -0.12481013938147219 0.0051907101257523776; -0.10323445301057829 -0.1259218870425957 0.003716732277081773; -0.09355176597918236 -0.130871233294346 0.003306535594834942; -0.07124572651241741 -0.12553468471214665 0.0020108136415145092; -0.0557767268511364 -0.1685959768674539 0.0019437293843202214; -0.021549123169529897 -0.10803755957761324 0.002034600881493311; -0.016013238333261934 -0.09622842770217328 -0.0002741920932820072; -0.004335206653515529 -0.0793719785110731 -0.0008939603722934327; 0.004740346893240406 -0.0607329376874639 -0.001716631473891448; 0.009818095755854734 -0.04491273068933977 -0.0022094281086108515; 0.01312805451032741 -0.027616502567377823 -0.0019177513080552329; 0.011878743159361204 -0.022925058186254264 -0.0022168412947191586; 0.0023818939899512676 -0.018414092946291174 -1.3347743447259673e-5; -0.0031036018027195927 -0.01627946171253065 -0.007426356212648579] %
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Mass Used: 1527.1786215537763 kg
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Launch C3: 31.505632562776483 km²/s²
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||V∞_in||: 4.544517160758207 km/s
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Mass Used: 1077.835193306381 kg
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Launch C3: 58.892217443051806 km²/s²
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||V∞_in||: 0.22049055124520436 km/s
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@@ -7,16 +7,16 @@ Spacecraft: bepi
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num_thrusters: 2
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duty_cycle: 0.9
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Launch Mass: 4000.0 kg
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Launch Date: 2022-03-06T01:59:18.919
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Launch V∞: [-1.1356413222408823, -4.788069365262547, 2.7000635369246] km/s
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Launch Date: 2024-08-10T04:39:14.851
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Launch V∞: [5.086503138635964, 5.7458326772994415, -0.07148502064229807] km/s
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Phase 1:
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Planet: Jupiter
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V∞_in: [0.606990343209641, 4.407893426470118, 0.9244860672598548] km/s
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V∞_out: [1.2183577357736917, -3.9826645468861925, 2.3687041043301797] km/s
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time of flight: 1.194581479969281e8 seconds
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arrival date: 2025-12-17T16:48:25.919
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thrust profile: [0.2047491180715187 -0.37019469041025893 -0.10453549807669095; 0.4301220091095493 -0.12441963747750297 -0.006770873233015344; 0.43924678986775806 0.1285374874465679 -0.07977271709638968; 0.42297198253230855 0.31380495510861767 -0.07919431310255642; 0.3614168205981836 0.39602843825488454 -0.05704653521018108; 0.2902414389460733 0.4053822027059241 -0.02821739799974643; 0.22430933743909634 0.43938508487263367 -0.00930631106824115; 0.13232647607691467 0.4188738913138919 0.007567873851875307; 0.054141732819826004 0.39551671259361465 0.010428460581952593; -0.012077434841877642 0.3792721276901153 0.0231446451624962; -0.042939891420425445 0.367704668401295 0.04590678245879779; -0.06832185713480624 0.39461571349444186 0.06647905984921844; -0.06871098668169624 0.3943544952193675 0.07996958584990013; -0.043122107121887 0.3236627227698529 0.06434542295394348; 0.0002258095938542581 0.3100245138960139 0.08315646808686966; 0.024384212213495196 0.1820219401839858 0.049878939508001104; 0.014803074731020839 0.09226807883171781 0.03031339291970727; 0.04882521682144194 0.07182823075104046 0.030435679401299; 0.07679479397181303 0.04220157719360384 0.024296177838332548; 0.07770574743624227 0.006328096858830944 0.01324607153162614] %
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V∞_in: [0.036227390916599315, 0.15967408190094506, 0.14767480118449552] km/s
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V∞_out: [0.02010676850789124, 0.050598467400280935, -0.04060341677187609] km/s
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time of flight: 2.2119244577042913e8 seconds
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arrival date: 2031-08-14T06:59:59.851
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thrust profile: [-0.03786142679064034 0.27339859122748333 0.0005726056795561895; -0.1960519532066938 0.1387630677841132 0.004600353091805394; -0.2161656001051881 0.03829454149587224 0.005463035319820266; -0.20722821473665434 -0.02785165286999182 0.00642011251062416; -0.19350969113180666 -0.07336980382318779 0.005798735353253219; -0.17166276097528518 -0.10180245936266212 0.0060229587041231505; -0.14580486341259447 -0.12481013938147219 0.0051907101257523776; -0.10323445301057829 -0.1259218870425957 0.003716732277081773; -0.09355176597918236 -0.130871233294346 0.003306535594834942; -0.07124572651241741 -0.12553468471214665 0.0020108136415145092; -0.0557767268511364 -0.1685959768674539 0.0019437293843202214; -0.021549123169529897 -0.10803755957761324 0.002034600881493311; -0.016013238333261934 -0.09622842770217328 -0.0002741920932820072; -0.004335206653515529 -0.0793719785110731 -0.0008939603722934327; 0.004740346893240406 -0.0607329376874639 -0.001716631473891448; 0.009818095755854734 -0.04491273068933977 -0.0022094281086108515; 0.01312805451032741 -0.027616502567377823 -0.0019177513080552329; 0.011878743159361204 -0.022925058186254264 -0.0022168412947191586; 0.0023818939899512676 -0.018414092946291174 -1.3347743447259673e-5; -0.0031036018027195927 -0.01627946171253065 -0.007426356212648579] %
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Mass Used: 1527.1786215537763 kg
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Launch C3: 31.505632562776483 km²/s²
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||V∞_in||: 4.544517160758207 km/s
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Mass Used: 1077.835193306381 kg
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Launch C3: 58.892217443051806 km²/s²
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||V∞_in||: 0.22049055124520436 km/s
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@@ -7,26 +7,26 @@ Spacecraft: bepi
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num_thrusters: 2
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duty_cycle: 0.9
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Launch Mass: 4000.0 kg
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Launch Date: 2024-10-23T01:57:04.645
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Launch V∞: [-2.756658080311089, 5.4981544960382, 1.2354164981485998] km/s
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Launch Date: 2024-03-01T19:28:21.132
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Launch V∞: [-1.4933474839937355, -1.896757005945588, 0.1342176084154792] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-6.97287754424969, 6.962353258098406, 0.0607051347526173] km/s
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V∞_out: [-6.685432199487985, 6.971638091675174, 1.9494641006878624] km/s
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time of flight: 1.16503060035366e7 seconds
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arrival date: 2025-03-06T22:08:50.645
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thrust profile: [0.0007372127333915423 -0.0014732374607987512 -0.0001436849126190515; 0.0015863792714624523 -0.0020954380857885 -3.9222886974518435e-5; 0.0028749200111876953 -0.0029070168117665577 -6.834239668653902e-5; 0.00400664873911032 -0.0036102638724926027 -0.0011534186183358992; 0.003002315886422529 -0.004155862034974375 -0.0019852589032208707; 0.003937369046006624 -0.003292245456470277 -0.00033744520390480056; 0.004022116761090881 -0.0014747882735426667 0.0009925828352185433; 0.0028363477848649932 -0.0006118542455278574 0.0011994525100711487; 0.0010235706279971136 -0.0007807187007764947 0.0007198591227898102; 1.9987192194599394e-5 -0.0011241077612402291 0.00021045682481486607; 0.0007623347096515055 -0.001326552903003275 0.00047334230828265155; -0.0019176703329012404 -0.003664068924494901 -0.0007926699243678642; -0.0034278750339086722 -0.005605775872095162 -0.001640142456026017; -0.003879314794056328 -0.007180423427345347 -0.0021627562917433257; -0.00457576381748711 -0.009085671380846889 -0.0027950147837868416; -0.00496447070432947 -0.011003150581070032 -0.0033564467543545713; -0.005782291476516903 -0.013187396198780097 -0.0040189185350814815; -0.005773642750057005 -0.015126117254672524 -0.00448918463406626; -0.006039589107819558 -0.017206354330223952 -0.00500209304716878; -0.0059712529665976325 -0.019287648124267687 -0.005416379053301935] %
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V∞_in: [-3.139849731672998, -2.3945611648587124, -1.1632748362007634] km/s
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V∞_out: [-4.106939244074457, 0.1211665771442673, -0.25340515321231993] km/s
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time of flight: 1.3574607375499237e8 seconds
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arrival date: 2028-06-19T22:42:54.132
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thrust profile: [-0.0019400973522372704 -0.0007861976680016341 0.0047112570560932255; 0.011634267167378483 0.025735587840716192 0.015153714739090269; 0.04023878204178935 0.0875934946637386 0.007499740159682127; -0.009467277325537368 0.13876616197672662 -0.012524106010789855; -0.10004425231685016 0.12061531322012457 -0.028391166185409118; -0.13327392532361876 0.014962677832168262 -0.03063014336273122; -0.049361915376229575 -0.06085040873226821 -0.01270432841636952; 0.03642870741492757 -0.027538682887140276 0.010604705365215029; 0.07311582311878274 0.038779781029538184 0.025999504078259884; 0.06015230279261901 0.1158643457634677 0.020078516937108694; -0.013284907011255715 0.16994053570631942 0.00015397612701227304; -0.11629264735479383 0.1487421375314807 -0.021401583793150897; -0.1698188059938155 0.045135754639904074 -0.03845221948411285; -0.10895165489995216 -0.06905174529770598 -0.03101882979146279; 0.011677929356157265 -0.0782197824462757 8.240504302237164e-6; 0.08774076836901655 -0.026355447222636122 0.017807315158523546; 0.12797619031639904 0.06837594720414757 0.02080641615928975; 0.09935124388498132 0.1833040558826352 0.0018019410798225937; -0.014862072610943274 0.2643385793887136 -0.021909120364733334; -0.1795798671224834 0.22847319945157946 -0.034527888025767346] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-2.501340292332268, 1.6226626635888894, -0.637397317769162] km/s
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||||
V∞_out: [-0.39137693018363046, -0.6158439855618857, -0.6179155724361174] km/s
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time of flight: 1.634809557285843e8 seconds
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arrival date: 2030-05-12T01:31:25.645
|
||||
thrust profile: [-0.26518247245545706 -0.09071259046697609 -0.06169797323040991; -0.08236380894068383 -0.03242059745452859 -0.0437757891207446; -0.0040559771435419905 -0.006989709543848695 -0.015529763525228361; 0.007774341207249076 -0.008985090840076109 -0.01850530400329914; 0.0012813370577481318 0.0011348539591867289 -0.0155496567606658; -0.007785092497807246 0.05338536306193304 0.019317990985589086; -0.0009728321119441025 0.08815185628620617 0.03949499622566367; 0.04305174658529387 0.2568399121830553 0.055654966170718544; -0.2720351356694226 0.46384420969664153 0.03864258122986833; -0.4887396982520584 0.11774562801231306 0.0008189965640148597; -0.3013298404095551 -0.13014726189273046 -0.05096356023658363; -0.13491430696546597 -0.11875243254479609 -0.04906685950011366; -0.07101074561201698 -0.09571411749724586 -0.04115396467769674; -0.03429442666375736 -0.08608492077264626 -0.032404742164699976; -0.005411454576501817 -0.08226389770332371 -0.021813716609185803; 0.01648826033313751 -0.08220086232228146 0.011531267107186598; -0.0514818142417244 -0.08481514714903496 -0.00037084018174361565; 0.04041503097410506 -0.045097405358868914 -0.044059162529628035; 0.22484925497674185 -0.023660465666373143 -0.05114459775451727; 0.4409715896106006 -0.006503526378072674 -0.04283633117576671] %
|
||||
V∞_in: [-1.9097984490864515, -1.884467804288567, 0.1478655003952606] km/s
|
||||
V∞_out: [0.5920296309381583, 0.5185305548716211, -0.34102424514328644] km/s
|
||||
time of flight: 1.1362938739949062e8 seconds
|
||||
arrival date: 2032-01-26T02:26:01.132
|
||||
thrust profile: [-0.31559923909748794 0.09689755853754745 -0.006919717656144527; -0.30761255565472767 -0.06071900887661422 0.008886404181900506; -0.23940374340653783 -0.15237412731650837 0.01667661369899387; -0.16751972908560994 -0.18821805967249375 0.01986348857730926; -0.10623664248862286 -0.19402685372102804 0.0208771393007191; -0.060042826303610866 -0.18882809282483437 0.021283405055828517; -0.027539940112158413 -0.17483716811234296 0.02049137689324002; -0.0021956619139218967 -0.1584555561559198 0.018984903410624785; 0.016974641677018447 -0.14078038683935779 0.0167485607342253; 0.03155709680599301 -0.122954819538575 0.013916179224635464; 0.042971402866106234 -0.10500259722323473 0.010513311074341624; 0.051634652307553965 -0.08728578079858391 0.006688169997632232; 0.0574625357891749 -0.0697078228574546 0.0023646019984288227; 0.06072929134486919 -0.053286809801298365 -0.0018027124516590476; 0.06007688200669981 -0.037667520940349315 -0.005792135480144473; 0.057800904682763964 -0.027552712555901016 -0.006802209283455497; 0.06140519856479137 -0.020185703984587373 -0.0058901658649188025; 0.06143756674033954 -0.01604342102490885 -0.0053401725681727595; 0.07062559388589974 -8.785146671736722e-5 -0.00863782359632625; 0.07614643902899883 0.016291745427162347 -0.010062236831540575] %
|
||||
|
||||
Mass Used: 1093.7042742756403 kg
|
||||
Launch C3: 39.355120557947245 km²/s²
|
||||
||V∞_in||: 3.0489363257617543 km/s
|
||||
Mass Used: 1283.6554577493703 kg
|
||||
Launch C3: 5.845788213962862 km²/s²
|
||||
||V∞_in||: 2.687082661129041 km/s
|
||||
|
||||
|
||||
|
||||
|
||||
@@ -7,23 +7,23 @@ Spacecraft: bepi
|
||||
num_thrusters: 2
|
||||
duty_cycle: 0.9
|
||||
Launch Mass: 4000.0 kg
|
||||
Launch Date: 2024-10-23T01:57:04.645
|
||||
Launch V∞: [-2.756658080311089, 5.4981544960382, 1.2354164981485998] km/s
|
||||
Launch Date: 2024-03-01T19:28:21.132
|
||||
Launch V∞: [-1.4933474839937355, -1.896757005945588, 0.1342176084154792] km/s
|
||||
Phase 1:
|
||||
Planet: Mars
|
||||
V∞_in: [-6.97287754424969, 6.962353258098406, 0.0607051347526173] km/s
|
||||
V∞_out: [-6.685432199487985, 6.971638091675174, 1.9494641006878624] km/s
|
||||
time of flight: 1.16503060035366e7 seconds
|
||||
arrival date: 2025-03-06T22:08:50.645
|
||||
thrust profile: [0.0007372127333915423 -0.0014732374607987512 -0.0001436849126190515; 0.0015863792714624523 -0.0020954380857885 -3.9222886974518435e-5; 0.0028749200111876953 -0.0029070168117665577 -6.834239668653902e-5; 0.00400664873911032 -0.0036102638724926027 -0.0011534186183358992; 0.003002315886422529 -0.004155862034974375 -0.0019852589032208707; 0.003937369046006624 -0.003292245456470277 -0.00033744520390480056; 0.004022116761090881 -0.0014747882735426667 0.0009925828352185433; 0.0028363477848649932 -0.0006118542455278574 0.0011994525100711487; 0.0010235706279971136 -0.0007807187007764947 0.0007198591227898102; 1.9987192194599394e-5 -0.0011241077612402291 0.00021045682481486607; 0.0007623347096515055 -0.001326552903003275 0.00047334230828265155; -0.0019176703329012404 -0.003664068924494901 -0.0007926699243678642; -0.0034278750339086722 -0.005605775872095162 -0.001640142456026017; -0.003879314794056328 -0.007180423427345347 -0.0021627562917433257; -0.00457576381748711 -0.009085671380846889 -0.0027950147837868416; -0.00496447070432947 -0.011003150581070032 -0.0033564467543545713; -0.005782291476516903 -0.013187396198780097 -0.0040189185350814815; -0.005773642750057005 -0.015126117254672524 -0.00448918463406626; -0.006039589107819558 -0.017206354330223952 -0.00500209304716878; -0.0059712529665976325 -0.019287648124267687 -0.005416379053301935] %
|
||||
V∞_in: [-3.139849731672998, -2.3945611648587124, -1.1632748362007634] km/s
|
||||
V∞_out: [-4.106939244074457, 0.1211665771442673, -0.25340515321231993] km/s
|
||||
time of flight: 1.3574607375499237e8 seconds
|
||||
arrival date: 2028-06-19T22:42:54.132
|
||||
thrust profile: [-0.0019400973522372704 -0.0007861976680016341 0.0047112570560932255; 0.011634267167378483 0.025735587840716192 0.015153714739090269; 0.04023878204178935 0.0875934946637386 0.007499740159682127; -0.009467277325537368 0.13876616197672662 -0.012524106010789855; -0.10004425231685016 0.12061531322012457 -0.028391166185409118; -0.13327392532361876 0.014962677832168262 -0.03063014336273122; -0.049361915376229575 -0.06085040873226821 -0.01270432841636952; 0.03642870741492757 -0.027538682887140276 0.010604705365215029; 0.07311582311878274 0.038779781029538184 0.025999504078259884; 0.06015230279261901 0.1158643457634677 0.020078516937108694; -0.013284907011255715 0.16994053570631942 0.00015397612701227304; -0.11629264735479383 0.1487421375314807 -0.021401583793150897; -0.1698188059938155 0.045135754639904074 -0.03845221948411285; -0.10895165489995216 -0.06905174529770598 -0.03101882979146279; 0.011677929356157265 -0.0782197824462757 8.240504302237164e-6; 0.08774076836901655 -0.026355447222636122 0.017807315158523546; 0.12797619031639904 0.06837594720414757 0.02080641615928975; 0.09935124388498132 0.1833040558826352 0.0018019410798225937; -0.014862072610943274 0.2643385793887136 -0.021909120364733334; -0.1795798671224834 0.22847319945157946 -0.034527888025767346] %
|
||||
Phase 2:
|
||||
Planet: Jupiter
|
||||
V∞_in: [-2.501340292332268, 1.6226626635888894, -0.637397317769162] km/s
|
||||
V∞_out: [-0.39137693018363046, -0.6158439855618857, -0.6179155724361174] km/s
|
||||
time of flight: 1.634809557285843e8 seconds
|
||||
arrival date: 2030-05-12T01:31:25.645
|
||||
thrust profile: [-0.26518247245545706 -0.09071259046697609 -0.06169797323040991; -0.08236380894068383 -0.03242059745452859 -0.0437757891207446; -0.0040559771435419905 -0.006989709543848695 -0.015529763525228361; 0.007774341207249076 -0.008985090840076109 -0.01850530400329914; 0.0012813370577481318 0.0011348539591867289 -0.0155496567606658; -0.007785092497807246 0.05338536306193304 0.019317990985589086; -0.0009728321119441025 0.08815185628620617 0.03949499622566367; 0.04305174658529387 0.2568399121830553 0.055654966170718544; -0.2720351356694226 0.46384420969664153 0.03864258122986833; -0.4887396982520584 0.11774562801231306 0.0008189965640148597; -0.3013298404095551 -0.13014726189273046 -0.05096356023658363; -0.13491430696546597 -0.11875243254479609 -0.04906685950011366; -0.07101074561201698 -0.09571411749724586 -0.04115396467769674; -0.03429442666375736 -0.08608492077264626 -0.032404742164699976; -0.005411454576501817 -0.08226389770332371 -0.021813716609185803; 0.01648826033313751 -0.08220086232228146 0.011531267107186598; -0.0514818142417244 -0.08481514714903496 -0.00037084018174361565; 0.04041503097410506 -0.045097405358868914 -0.044059162529628035; 0.22484925497674185 -0.023660465666373143 -0.05114459775451727; 0.4409715896106006 -0.006503526378072674 -0.04283633117576671] %
|
||||
V∞_in: [-1.9097984490864515, -1.884467804288567, 0.1478655003952606] km/s
|
||||
V∞_out: [0.5920296309381583, 0.5185305548716211, -0.34102424514328644] km/s
|
||||
time of flight: 1.1362938739949062e8 seconds
|
||||
arrival date: 2032-01-26T02:26:01.132
|
||||
thrust profile: [-0.31559923909748794 0.09689755853754745 -0.006919717656144527; -0.30761255565472767 -0.06071900887661422 0.008886404181900506; -0.23940374340653783 -0.15237412731650837 0.01667661369899387; -0.16751972908560994 -0.18821805967249375 0.01986348857730926; -0.10623664248862286 -0.19402685372102804 0.0208771393007191; -0.060042826303610866 -0.18882809282483437 0.021283405055828517; -0.027539940112158413 -0.17483716811234296 0.02049137689324002; -0.0021956619139218967 -0.1584555561559198 0.018984903410624785; 0.016974641677018447 -0.14078038683935779 0.0167485607342253; 0.03155709680599301 -0.122954819538575 0.013916179224635464; 0.042971402866106234 -0.10500259722323473 0.010513311074341624; 0.051634652307553965 -0.08728578079858391 0.006688169997632232; 0.0574625357891749 -0.0697078228574546 0.0023646019984288227; 0.06072929134486919 -0.053286809801298365 -0.0018027124516590476; 0.06007688200669981 -0.037667520940349315 -0.005792135480144473; 0.057800904682763964 -0.027552712555901016 -0.006802209283455497; 0.06140519856479137 -0.020185703984587373 -0.0058901658649188025; 0.06143756674033954 -0.01604342102490885 -0.0053401725681727595; 0.07062559388589974 -8.785146671736722e-5 -0.00863782359632625; 0.07614643902899883 0.016291745427162347 -0.010062236831540575] %
|
||||
|
||||
Mass Used: 1093.7042742756403 kg
|
||||
Launch C3: 39.355120557947245 km²/s²
|
||||
||V∞_in||: 3.0489363257617543 km/s
|
||||
Mass Used: 1283.6554577493703 kg
|
||||
Launch C3: 5.845788213962862 km²/s²
|
||||
||V∞_in||: 2.687082661129041 km/s
|
||||
|
||||
@@ -1,17 +0,0 @@
|
||||
@testset "Outer Loop" begin
|
||||
|
||||
using Dates
|
||||
|
||||
println("Testing Genetic Algorithm")
|
||||
|
||||
launch_range = [ DateTime(2016,3,28), DateTime(2019,3,28) ]
|
||||
target = "Saturn"
|
||||
deadline = DateTime(2028,12,31)
|
||||
|
||||
# First let's just test that we can generate a member of the population
|
||||
member = gen_decision_vector(launch_range, target, deadline)
|
||||
println(member)
|
||||
|
||||
@test typeof(member) == Vector{Phase}
|
||||
|
||||
end
|
||||
@@ -3,7 +3,7 @@ using Random
|
||||
using LinearAlgebra
|
||||
using SPICE
|
||||
using Thesis
|
||||
using Dates: DateTime, Dates
|
||||
using Dates: DateTime, Millisecond, Dates, Second, format, datetime2unix, unix2datetime
|
||||
|
||||
try
|
||||
furnsh("../../spice_files/naif0012.tls")
|
||||
@@ -15,8 +15,9 @@ end
|
||||
|
||||
@testset "All Tests" begin
|
||||
include("plotting.jl")
|
||||
include("inner_loop/laguerre-conway.jl")
|
||||
include("inner_loop/propagator.jl")
|
||||
include("inner_loop/nlp_solver.jl")
|
||||
include("inner_loop/monotonic_basin_hopping.jl")
|
||||
include("laguerre-conway.jl")
|
||||
include("propagator.jl")
|
||||
include("nlp_solver.jl")
|
||||
include("mbh.jl")
|
||||
include("genetic_algorithm.jl")
|
||||
end
|
||||
|
||||
Reference in New Issue
Block a user