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Be sure to mention its uses in many legitimate places. + Reveal the advantages of Sims-Flanagan transcription as an alternative to higher-fidelity propagation models. Be sure to mention its uses in many legitimate places. \section{Interplanetary Trajectory Considerations} Highlight the problems with the 2BP in co-ordinating influences of extra bodies over an interplanetary journey. @@ -87,10 +87,10 @@ Describe the method of patched conics. \subsection{Gravity Assist Maneuvers} - Describe how a gravity assist manuever would work in the framework of patched conics. Also discuss the advantages of such a maneuver. + Describe how a gravity assist maneuver would work in the framework of patched conics. Also discuss the advantages of such a maneuver. \subsection{Multiple Gravity Assist Techniques} - Discuss the advantages of chaining together multiple gravity assists and highlight the difficulties in choosing these assists. Here I can mention porkchop plots, lambert's problem, etc. Here I can also talk about Hybrid Optimal Control Problems. + Discuss the advantages of chaining together multiple gravity assists and highlight the difficulties in choosing these assists. Here I can mention porkchop plots, Lambert's problem, etc. Here I can also talk about Hybrid Optimal Control Problems. \subsection{Ephemeris Considerations} I can quickly mention SPICE here and talk a bit about validation. @@ -102,7 +102,7 @@ Discuss what a decision vector is in the context of an optimization problem. \subsection{Selection and Fitness Evaluation} - Dicuss the costing being used as well as the different types of fitness evaluation that are common. Also discuss the concept of generations and ``survival''. + Discuss the costing being used as well as the different types of fitness evaluation that are common. Also discuss the concept of generations and ``survival''. \subsubsection{Tournament Selection} Dive deeper into the specific selection algorithm being used here. @@ -114,7 +114,7 @@ Discuss specific crossover algorithm used here. \subsubsection{Mutation} - Discuss both the neccessity for mutation and the mutation algorithm being used. + Discuss both the necessity for mutation and the mutation algorithm being used. \section{Algorithm Overview} Highlight the algorithm at a high-level. This is likely where flowcharts and diagrams will go to give a high-level overview. @@ -141,9 +141,9 @@ Overview the outer loop. This may require a final flowchart, but might potentially be too simple to lend itself to one. \subsubsection{Inner Loop Calling Function} - The primary reason for including this section is to dicuss the error handling. + The primary reason for including this section is to discuss the error handling. - \subsubsection{Genetic Algorithm Decription} + \subsubsection{Genetic Algorithm Description} Similar to the MBH section, there are a lot of implementation details to go over here. Many will have already been discussed in the background sections above. But I can step through each of the decisions, similar to Englander's paper on this. \section{Results Analysis} @@ -169,7 +169,7 @@ Talk a bit about why this work is valuable. Missions that could have benefited, missions that this enables, etc. \subsection{Recommendations for Future Work} - Recommend future work, obviously. There are a \emph{ton} of opportunities for improvement including parallellization, cluster computing, etc. + Recommend future work, obviously. There are a \emph{ton} of opportunities for improvement including parallelization, cluster computing, etc. % \bibliography{biblio}{} % \bibliographystyle{plain} diff --git a/archive/EJS_2021-10-18T20:47:50.889/mission b/archive/EJS_2021-10-18T20:47:50.889/mission new file mode 100644 index 0000000..f31b306 --- /dev/null +++ b/archive/EJS_2021-10-18T20:47:50.889/mission @@ -0,0 +1,29 @@ +archive/EJS_2021-10-18T20:47:50.889/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 1978-12-12T22:48:52.804 +Launch V∞: [-6.090674217377611, 1.9365075336539337, 1.0648698904498797] km/s +Phase 1: + Planet: Jupiter + V∞_in: [-8.599568746419632, -3.929372774157513, 0.1598903162745283] km/s + V∞_out: [-6.29056111779008, -7.057496301214243, 0.189430044733671] km/s + time of flight: 1.3001684481349075e8 seconds + arrival date: 1983-01-25T18:36:16.804 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0.15430255903950427 -0.013461557013245747] % + +Mass Used: 254.85590261239986 kg +Launch C3: 79.62133289026262 km²/s² +||V∞_in||: 5.978555952666198 km/s diff --git a/archive/EJU.html b/archive/EJU.html new file mode 100644 index 0000000..fd2cb6c --- /dev/null +++ b/archive/EJU.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EJU_2021-10-20T06:30:07.134/mission b/archive/EJU_2021-10-20T06:30:07.134/mission new file mode 100644 index 0000000..69bd2f1 --- /dev/null +++ b/archive/EJU_2021-10-20T06:30:07.134/mission @@ -0,0 +1,29 @@ +archive/EJU_2021-10-20T06:30:07.134/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1976-08-01T17:52:34.221 +Launch V∞: [7.796110966770354, 4.8982533648856466, 0.17379030255431946] km/s +Phase 1: + Planet: Jupiter + V∞_in: [3.8433311299973627, 5.796528049238326, -0.2817056847145128] km/s + V∞_out: [-1.50322449690382, -5.857435376892681, 3.4467617942706994] km/s + time of flight: 6.162384733838075e7 seconds + arrival date: 1978-07-15T23:36:41.221 + thrust profile: [0.05076636324847266 0.044371172883747347 -0.000466591620230539; 0.04556839732559172 0.04551590000211736 0.026305580765275827; 0.04271388990028329 0.042965827861916495 0.032904618961254566; 0.04125704453812768 0.04399260927643073 0.011906508964846164; 0.037771810990335594 0.045126058811728244 0.017892630651311324; 0.03744914320857412 0.012083627702152488 0.016408253290893425; 0.037727702899229075 0.010853738248166893 0.015148025588847367; 0.005572973923857532 0.007303529249390285 0.011121028124084267; 0.00617297452148193 0.006145429794742058 0.011859116648542195; 0.005049233699504967 0.006452625990674288 0.011772625897474782; 0.004910258402799322 0.006366537658928831 0.0005643550152455212; 0.0025763592102966957 0.003181565085352132 0.010814482610218074; 0.0031947900522401847 0.0029830417754423276 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flight: 2.993961596792109e8 seconds + arrival date: 1988-01-10T05:12:40.221 + thrust profile: [-0.07931776222154702 -0.09715466918867674 -0.026833250451506713; -0.09845323400323117 -0.17879388582940878 -0.04291406251121993; -0.08894254596894183 -0.09528460976651616 -0.054982106035208346; -0.06263720199951707 -0.0878116196248785 -0.05530652171544619; -0.06259005068834375 -0.09717952834183764 -0.06095027382199235; -0.06352579562023707 -0.09929139401807714 -0.07234338457248485; -0.0686236352886369 -0.09800849861144206 -0.08974924433995998; -0.05956649938146661 -0.08337006632048641 -0.1038431051473047; -0.04514195618670204 -0.08203823260227076 -0.10463027094106508; -0.06289461841109399 -0.060085191156628553 -0.10341360065396196; -0.05445769738916689 -0.09997930701298721 -0.09742267375781755; -0.05465737582266164 -0.08439167405860351 -0.09062236126374591; -0.04456643405680078 -0.07331795808665253 -0.09712534152461183; -0.06256760664966003 -0.08549758983692145 -0.12946096634923257; 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b/archive/EJU_2021-10-20T06:30:07.134/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EJU_2021-10-20T06:56:05.706/mission b/archive/EJU_2021-10-20T06:56:05.706/mission new file mode 100644 index 0000000..5e4ac5d --- /dev/null +++ b/archive/EJU_2021-10-20T06:56:05.706/mission @@ -0,0 +1,29 @@ +archive/EJU_2021-10-20T06:56:05.706/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1976-07-29T22:56:52.810 +Launch V∞: [6.949925110063542, 5.51142706678786, 1.1338882248683144] km/s +Phase 1: + Planet: Jupiter + V∞_in: [3.906881971734985, 4.095747067849015, -0.40798750984197163] km/s + V∞_out: [-0.9527557058881729, -3.9759295150204843, -3.9356834360151556] km/s + time of flight: 7.564082964432266e7 seconds + arrival date: 1978-12-22T10:17:21.810 + thrust profile: [0.03782916575140308 0.03740282492642642 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b/archive/EJU_2021-10-20T09:24:50.637/mission @@ -0,0 +1,29 @@ +archive/EJU_2021-10-20T09:24:50.637/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1976-08-03T18:07:52.908 +Launch V∞: [6.299916182319705, 6.240538451377015, -0.9940165103728982] km/s +Phase 1: + Planet: Jupiter + V∞_in: [4.178807865103526, 3.271316108925791, 0.038831033060078735] km/s + V∞_out: [-1.3778027301160083, -5.1110224704243725, -0.38018528529187656] km/s + time of flight: 9.076893335112691e7 seconds + arrival date: 1979-06-20T07:43:25.908 + thrust profile: [0.04513213164333234 0.04346394223048948 0.007180644066023622; 0.023711461445665785 0.04851693214299602 0.03207463889343553; 0.00969082323802968 0.0429167126574647 0.05027917371754633; 0.0006490219093697312 0.03432108495203708 0.05302050429400685; -0.003953708767625976 0.02834092045678569 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-0.007770585754213655; 0.044300010743546385 0.1656092696295884 -0.009813911794334952; 0.04940888045966933 0.15430255903950427 -0.013461557013245747] % + +Mass Used: 254.85590261239986 kg +Launch C3: 79.62133289026262 km²/s² +||V∞_in||: 5.978555952666198 km/s diff --git a/archive/EJU_2021-10-20T09:24:50.637/plot.html b/archive/EJU_2021-10-20T09:24:50.637/plot.html new file mode 100644 index 0000000..1358d89 --- /dev/null +++ b/archive/EJU_2021-10-20T09:24:50.637/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EJU_archive b/archive/EJU_archive new file mode 100644 index 0000000..d9d9426 --- /dev/null +++ b/archive/EJU_archive @@ -0,0 +1,94 @@ +archive/EJU_archive +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1976-08-01T17:52:34.221 +Launch V∞: [7.796110966770354, 4.8982533648856466, 0.17379030255431946] km/s +Phase 1: + Planet: Jupiter + V∞_in: [3.8433311299973627, 5.796528049238326, -0.2817056847145128] km/s + V∞_out: [-1.50322449690382, -5.857435376892681, 3.4467617942706994] km/s + time of flight: 6.162384733838075e7 seconds + arrival date: 1978-07-15T23:36:41.221 + thrust profile: [0.05076636324847266 0.044371172883747347 -0.000466591620230539; 0.04556839732559172 0.04551590000211736 0.026305580765275827; 0.04271388990028329 0.042965827861916495 0.032904618961254566; 0.04125704453812768 0.04399260927643073 0.011906508964846164; 0.037771810990335594 0.045126058811728244 0.017892630651311324; 0.03744914320857412 0.012083627702152488 0.016408253290893425; 0.037727702899229075 0.010853738248166893 0.015148025588847367; 0.005572973923857532 0.007303529249390285 0.011121028124084267; 0.00617297452148193 0.006145429794742058 0.011859116648542195; 0.005049233699504967 0.006452625990674288 0.011772625897474782; 0.004910258402799322 0.006366537658928831 0.0005643550152455212; 0.0025763592102966957 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-0.02009516515935024 -0.007031029808761148 -0.051230718639702445; -0.011470301871887377 -0.004835200281315476 -0.04666627205144148; -0.008153291863800712 -0.009020456383335974 -0.04383434884087585; -0.0014098997805392169 -0.0026298096598901966 -0.03405966422871517; 0.014283781279323941 0.016279866267866545 -0.03609253084131848; 0.05336200053505927 0.03389800040998884 -0.040619525225581585; 0.06527766464651791 0.050216170197614575 -0.042586118795403936; 0.05723451861797406 0.03384400630020884 -0.03901891375575639; 0.08543313326117905 0.08974239510128046 -0.03621120917366133; 0.0630088316034018 0.15678763151906544 -0.005574987167467689; 0.060329780298105595 0.17485309892272635 0.013906868818896528; 0.0637300324111305 0.18467219733664741 0.016407349987587503] % + +Mass Used: 292.79309729930446 kg +Launch C3: 84.80243530207245 km²/s² +||V∞_in||: 7.638468430129195 km/s + + + +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1976-07-29T22:56:52.810 +Launch V∞: [6.949925110063542, 5.51142706678786, 1.1338882248683144] km/s +Phase 1: + Planet: Jupiter + V∞_in: [3.906881971734985, 4.095747067849015, -0.40798750984197163] km/s + V∞_out: [-0.9527557058881729, -3.9759295150204843, -3.9356834360151556] km/s + time of flight: 7.564082964432266e7 seconds + arrival date: 1978-12-22T10:17:21.810 + thrust profile: [0.03782916575140308 0.03740282492642642 -0.002576574442432617; 0.02568719536954076 0.06252477749229525 0.01652454606912066; 0.004225260108780641 0.03649507973713675 0.026304939794628213; 0.008514278978805623 0.005632465170283442 0.028766756627515436; 0.0028553869411493105 0.032931024849802475 0.02858849466203496; -0.00011527850331830502 0.037305718745844846 0.035357183754127365; -0.0020666322700494226 0.024839987547461636 0.04207353968844954; -0.0023476551667392757 0.02636000649838633 0.03519093267459137; 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+Launch C3: 79.96298985450858 km²/s² +||V∞_in||: 6.3733655440922625 km/s + + + +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1976-08-03T18:07:52.908 +Launch V∞: [6.299916182319705, 6.240538451377015, -0.9940165103728982] km/s +Phase 1: + Planet: Jupiter + V∞_in: [4.178807865103526, 3.271316108925791, 0.038831033060078735] km/s + V∞_out: [-1.3778027301160083, -5.1110224704243725, -0.38018528529187656] km/s + time of flight: 9.076893335112691e7 seconds + arrival date: 1979-06-20T07:43:25.908 + thrust profile: [0.04513213164333234 0.04346394223048948 0.007180644066023622; 0.023711461445665785 0.04851693214299602 0.03207463889343553; 0.00969082323802968 0.0429167126574647 0.05027917371754633; 0.0006490219093697312 0.03432108495203708 0.05302050429400685; -0.003953708767625976 0.02834092045678569 0.05567795776724263; -0.007078446275295329 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0.0012758806822037029] km/s + time of flight: 9.72503999711726e7 seconds + arrival date: 2025-09-20T22:59:29.624 + thrust profile: [0.309005048551296 0.18339415892490127 0.0027002374517968134; 0.39038340279454015 -0.08598467958258589 0.010312803693732317; 0.44938940212387873 -0.08807777402752429 0.002785661604362881; 0.4727841039456793 -0.03534032379035236 -0.0018849144811814039; 0.4690712072738283 -0.03960532320766157 -0.004473107597690517; 0.45397991987657443 -0.15486398878325663 -0.005680521852703244; 0.4485788241679923 -0.33567734538476923 -0.005564951845911451; 0.5216248999417937 -0.47975370744057766 -0.005660397120411834; 0.6920392190397051 -0.5005798311516338 -0.005517054932513914; 0.7679838906703794 0.5300520361001183 -0.005384387857015156; 0.512203310002801 0.7194823119304291 -0.0013647498450424262; 0.10514790861349814 0.6588219176238146 -9.159548578737903e-5; -0.049683494944089746 0.566183781136383 -0.0022586868669512107; -0.09075248681288331 0.45610022500744607 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+/home/connor/projects/thesis/archive/EJ_2021-11-07T16:22:00.626/mission--------------------------- + +Spacecraft: bepi + dry_mass: 2000.0 kg + specific impulse: 2800.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 0.9 +Launch Mass: 4000.0 kg +Launch Date: 2027-11-04T12:48:56.123 +Launch V∞: [-8.732498886729314, 4.51787497134938, 0.8120510695970266] km/s +Phase 1: + Planet: Jupiter + V∞_in: [-9.88645331410529, -0.7687768634212618, 0.7151206660880595] km/s + V∞_out: [-0.4049088507623607, 0.17689076088451985, 0.12508940089378756] km/s + time of flight: 4.573440000016084e7 seconds + arrival date: 2029-04-16T20:48:56.123 + thrust profile: [-0.7252261699958953 0.6373188434471561 0.4327846850623052; -0.7899362435001571 0.3285194444697549 0.11446253449938033; -0.7680712363242684 -0.1633173479005095 -0.0753102013115445; -0.5201123290608496 -0.42217681987872474 -0.4647696966643137; -0.6013508181063658 -0.38366831483797026 -0.18445814629025725; -0.4581606987896879 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--git a/archive/EJ_2021-11-07T16:22:00.626/plot.html b/archive/EJ_2021-11-07T16:22:00.626/plot.html new file mode 100644 index 0000000..604e8e6 --- /dev/null +++ b/archive/EJ_2021-11-07T16:22:00.626/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EJ_2021-11-07T16:23:30.327/mission b/archive/EJ_2021-11-07T16:23:30.327/mission new file mode 100644 index 0000000..7e96b04 --- /dev/null +++ b/archive/EJ_2021-11-07T16:23:30.327/mission @@ -0,0 +1,22 @@ +/home/connor/projects/thesis/archive/EJ_2021-11-07T16:23:30.327/mission--------------------------- + +Spacecraft: bepi + dry_mass: 2000.0 kg + specific impulse: 2800.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 0.9 +Launch Mass: 4000.0 kg +Launch Date: 2027-09-12T06:04:50.667 +Launch V∞: [-0.1356894386368732, 5.956064811848478, 0.01939640608336112] km/s +Phase 1: + Planet: Jupiter + V∞_in: [-0.2571115997565001, -0.23716727061524712, 0.1301306668580519] km/s + V∞_out: [-0.014179189011866182, -0.008514489265672389, -0.020254493877991896] km/s + time of flight: 1.8070773341225305e8 seconds + arrival date: 2033-06-03T18:40:23.667 + thrust profile: [-0.28796335426441344 0.2918284262842529 0.004232031537641381; -0.4146826747229724 -0.02204183876659545 0.006463923516828132; -0.3658131284334198 -0.20897490324756807 0.004830213098433344; -0.3009950427607718 -0.29983050286376706 0.0026330364724320627; -0.21226927941652138 -0.31438885498847047 0.00016223993548310865; -0.13803056237326825 -0.31060963133872505 -0.002084476169128304; -0.07968485985716361 -0.29051876651351477 -0.004227991069940268; -0.03393237770799525 -0.2616050729753513 -0.005805065906776818; 0.00010399437044312852 -0.22612386906622065 -0.00723203544008763; 0.02431397619795949 -0.1841020095991609 -0.007967346627807494; 0.03387857848006785 -0.1473548203513266 -0.008904505604898574; 0.0464200796450669 -0.10786650792140276 -0.008591232690818134; 0.05146001248652659 -0.0649385531036076 -0.007930560486331771; 0.05288431148130223 -0.014078912962736419 -0.00441593039414774; 0.0455197215338432 -0.024008992010477768 -0.009803033072905896; 0.05520804599773281 0.0034148633177632287 -0.0036277778862629463; 0.045785853836455455 0.00794833182192021 -0.0217178944298006; 0.04513924118080819 0.05766612276661263 -0.0007249356261771857; 0.0848074300734865 0.06484381201504433 0.010866963214099381; 0.08645863137101507 0.10712102831006817 -0.005895302546374282] % + +Mass Used: 1398.921932467841 kg +Launch C3: 35.493495887266185 km²/s² +||V∞_in||: 0.37321398612237705 km/s diff --git a/archive/EJ_2021-11-07T16:23:30.327/plot.html b/archive/EJ_2021-11-07T16:23:30.327/plot.html new file mode 100644 index 0000000..87816ad --- /dev/null +++ b/archive/EJ_2021-11-07T16:23:30.327/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EJ_2021-11-10T17:36:57.486/mission b/archive/EJ_2021-11-10T17:36:57.486/mission new file mode 100644 index 0000000..f1c270a --- /dev/null +++ b/archive/EJ_2021-11-10T17:36:57.486/mission @@ -0,0 +1,22 @@ +/home/connor/projects/thesis/archive/EJ_2021-11-10T17:36:57.486/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1977-09-23T03:22:48.372 +Launch V∞: [-9.493171911757265, 1.996521857385693, 1.8459560902623946] km/s +Phase 1: + Planet: Jupiter + V∞_in: [-9.543974938238337, -5.087831983949424, -0.35708404363703494] km/s + V∞_out: [-0.129298458647144, 0.15324446409210052, -0.009200490470804264] km/s + time of flight: 1.776357220782331e8 seconds + arrival date: 1983-05-11T02:38:10.372 + thrust profile: [-0.7610489826673982 0.4519575670810889 0.38105436601704845; -0.692182777203481 -0.5430220362690558 -0.19169924364371457; -0.713848909301823 0.5682383712035098 0.21475368591818692; -0.762202012287276 0.6169631842658447 -0.06393276641993992; -0.7682887422768392 0.5658174117175422 -0.356299726756724; -0.7247484323513448 0.615681193372203 -0.3204930084782787; -0.8443101955436311 0.7531829445331782 0.35162106487694683; -0.7361591502293401 -0.7428403909252584 0.054461158094787014; -0.6989134861291908 -0.542824582709043 -0.07047657066876702; -0.7311534977516068 0.308382219231665 -0.2420265209340023; -0.7433256599203858 0.5382732546276702 -0.2395625345263195; -0.7439731882157303 0.6152077332897807 -0.2615422771160056; -0.7183921784988241 0.683166135255115 -0.25632068075573156; -0.6372607269354764 0.7800738376092019 -0.09467864945511045; -0.9264981728556586 0.8626484815884095 0.7406409970321504; -0.6596702419789453 -0.8411615509502441 0.18958949263763294; -0.20841320586198334 -0.7908230728915269 0.12046929919930525; 0.26398550226277 -0.7164725093202939 0.085019685455708; 0.4864448421040628 -0.5765963344719907 0.052561242827218184; 0.6036699781228905 -0.23314430271586686 0.02081945694704924] % + +Mass Used: 1364.498204540083 kg +Launch C3: 97.51396636037275 km²/s² +||V∞_in||: 10.82132158901307 km/s diff --git a/archive/EJ_2021-11-10T17:36:57.486/plot.html b/archive/EJ_2021-11-10T17:36:57.486/plot.html new file mode 100644 index 0000000..0ac38c3 --- /dev/null +++ b/archive/EJ_2021-11-10T17:36:57.486/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJN_2021-11-29T17:22:43.432/mission b/archive/EMJN_2021-11-29T17:22:43.432/mission new file mode 100644 index 0000000..659465d --- /dev/null +++ b/archive/EMJN_2021-11-29T17:22:43.432/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJN_2021-11-29T17:22:43.432/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-12-23T15:19:18.306 +Launch V∞: [3.7246340359905252, -0.7668922286241167, -1.2982795287623152] km/s +Phase 1: + Planet: Mars + V∞_in: [2.494283608647667, 0.4779176399654301, -2.4127945752092663] km/s + V∞_out: [-0.4965998694292626, 2.280726103742723, -2.6122161933665495] km/s + time of flight: 1.1112593378745796e8 seconds + arrival date: 2028-07-01T19:38:11.306 + thrust profile: [0.574314864465574 0.4270452174232693 0.29638159374668793; 0.5446571483586893 0.6545005999072503 0.29885454938460493; -0.6407008818388138 0.6047471705598826 -0.3611107482397214; -0.6090910018886806 0.4086292020353647 -0.3182239029023878; -0.5972700374128047 -0.5925649766181501 -0.1428611882223418; 0.7035933873557789 -0.7374496458897967 0.25856313264181247; 0.6187581048385012 0.71068635783626 -0.05789366680034934; -0.6641950503565809 0.6437898522192934 -0.27526162728737996; -0.7420417902057971 -0.41426865914506017 -0.23642243903474278; -0.6117186284649462 -0.7691378662390483 -0.008551868685930122; 0.9103799821363571 -0.6958464571429571 0.20143430274286617; 0.6949604843307996 0.7921653784196445 -0.06766318190720352; -0.711280843553026 0.7699727320198064 -0.2712015558254371; -0.8157341118174929 0.47411989191797727 -0.25649460581099315; -0.8017585640901678 -0.7742154973052455 -0.037675698291696834; 0.04044429011740304 -0.8663007134481628 0.2032563083072973; 0.854373492928133 -0.7735870663242215 0.19757822091240435; 0.8364988214950911 0.8495507135624523 -0.07245450181745107; -0.17309103497250355 0.8763214931380413 -0.2655879782455708; -0.8411527513899564 0.819160378514693 -0.2586467736093903] % +Phase 2: + Planet: Jupiter + V∞_in: [-5.538205957708029, -2.9054361894143304, 0.33552637947187924] km/s + V∞_out: [0.5046777525076017, 6.240066179835522, -0.1810924190839511] km/s + time of flight: 1.5845886601650202e8 seconds + arrival date: 2033-07-09T19:59:17.306 + thrust profile: [-0.9036543510864951 0.6541143791625612 -0.3222980415291042; -0.8832461130197783 -0.737424683011361 -0.3022522605581414; -0.8209657934438149 -0.855511836631351 -0.2551798333859342; -0.6867673786369394 -0.8683395906979817 -0.2263222463630974; -0.4869220845452508 -0.8445214158833173 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V∞_in: [9.265725092936133, -9.786832491497965, -0.08265318279988049] km/s + V∞_out: [-0.04939156370003244, 7.080398077984083, 0.008343683362610646] km/s + time of flight: 1.1790191001194214e7 seconds + arrival date: 2033-11-23T07:02:28.306 + thrust profile: [-0.03898824639829615 0.16371784077873527 -0.00013552715761737044; -0.03965980066394493 0.16534224208941117 -0.00011383530680316276; -0.0408187339699479 0.16443725546158428 -9.400453754275044e-5; -0.041109678864468216 0.1647205038566749 -8.342084332467601e-5; -0.04174133700362553 0.16664340240392897 -7.006086027666118e-5; -0.0424810737661852 0.1667002978899254 -5.700029092451851e-5; -0.04239207210941273 0.16701251418502575 -4.383623068936747e-5; -0.04652037459029391 0.16804035967999092 -2.978584844002596e-5; -0.04427137548076659 0.16950248273838245 -1.5426422905404063e-5; -0.04508723711412531 0.16561986502047163 -1.3433623473967066e-6; -0.04558502556546034 0.17116968335570643 4.062370321680114e-5; -0.046116752045498706 0.1722075533700207 2.3987312014333166e-5; -0.04709823531387585 0.1715653407790682 3.545164619148473e-5; -0.047773360118737326 0.17247757474396616 5.171911800828078e-5; -0.04877410118731465 0.17444398529369937 6.339628403937785e-5; -0.049033599874160665 0.1739487314179798 7.666428673687004e-5; -0.050091444345239274 0.17443171851273329 8.994289395414832e-5; -0.05049095135560994 0.17620949694675078 0.00010428768262633634; -0.051247933732248764 0.1760232752199048 0.00011912360582272222; -0.052158341276396 0.17808218005608098 0.0001313980216301485] % + +Mass Used: 1726.4616690486366 kg +Launch C3: 16.146552127186432 km²/s² +||V∞_in||: 13.477484307656734 km/s diff --git a/archive/EMJN_2021-11-29T17:22:43.432/plot.html b/archive/EMJN_2021-11-29T17:22:43.432/plot.html new file mode 100644 index 0000000..04d24ef --- /dev/null +++ b/archive/EMJN_2021-11-29T17:22:43.432/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJN_2021-11-29T20:07:38.430/mission b/archive/EMJN_2021-11-29T20:07:38.430/mission new file mode 100644 index 0000000..9de844f --- /dev/null +++ b/archive/EMJN_2021-11-29T20:07:38.430/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJN_2021-11-29T20:07:38.430/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-05-27T23:45:19.477 +Launch V∞: [0.07060914008148668, -4.847892797001834, 0.5290687721885886] km/s +Phase 1: + Planet: Mars + V∞_in: [-2.8376948696397957, -6.866970594886355, -1.1016914014907047] km/s + V∞_out: [-4.226081909733871, -6.202110186999845, -0.3094281797413773] km/s + time of flight: 1.596037143160738e8 seconds + arrival date: 2028-06-17T06:07:13.477 + thrust profile: [-0.08820762853917691 -0.14898517184082533 -0.09820752341370556; -0.16244500639383114 -0.007014189727643575 -0.042114530446779465; -0.11504442623490056 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-0.06358457091065511 0.19606506430779863 -0.061016941617662156; -0.21816429202004126 0.10669767546640854 0.03444638959744015] % +Phase 2: + Planet: Jupiter + V∞_in: [3.7354750271686217, -5.88285076118926, 0.3565930630644914] km/s + V∞_out: [-0.34319042907183317, 6.967067331497001, -0.17523613192719362] km/s + time of flight: 1.599110498440805e8 seconds + arrival date: 2033-07-12T01:51:22.477 + thrust profile: [-0.40987114064695546 -0.3774240932862401 -0.03561424162645277; -0.3658595283634409 -0.649925100592242 -0.03267051158991308; 0.3459098563469254 -0.6438693437660852 -0.04635788737542222; 0.5043654957163684 -0.3232526513194753 -0.01450355602555917; 0.42491000056144884 -0.21802276807884619 0.030992274127171215; 0.34082656017644314 -0.17376917376621892 0.04325816043964533; 0.1376056849711479 -0.12166741048661384 0.05225660923751248; -0.13620705214465267 0.022867431783402784 0.06787427526509686; -0.3502016747280746 0.1254089210892246 -0.03219035055838345; -0.7729039185116515 0.050166197257457634 -0.07418896319497846; -0.8826906384645422 -0.42770154496434787 -0.09066661080452741; -0.8697879488343527 -0.8989912582247904 -0.11292428779799557; -0.3012587410720149 -0.8933703434566561 -0.10271304251295864; 0.7595659924014233 -0.8695220977621636 -0.049116949463447176; 0.7872267924160511 -0.6662320332198877 -0.011350265126440771; 0.7392293426195585 -0.33787052962012654 0.00950541251523341; 0.6603814845566363 -0.005691408214699979 0.01737841943566633; 0.5573136293405954 -0.158764215359649 0.021196329449577604; 0.40957430642093684 0.1915873694381741 0.028239988792705437; 0.18146188186458964 0.1883476561832824 0.03330416774233607] % +Phase 3: + Planet: Neptune + V∞_in: [8.506155596263332, -7.214120420207235, -0.09860913292565265] km/s + V∞_out: [4.053253594386909, 0.1372094566434354, -0.11675704795783998] km/s + time of flight: 4.156831849103214e7 seconds + arrival date: 2034-11-05T04:36:40.477 + thrust profile: [-0.04831977082461104 0.02886785140102746 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4.28282466982456e-5; -0.0598515487471952 0.03219101178897971 -8.932622689143771e-6; -0.060385880377208864 0.03228344074846185 8.425209789811808e-5; -0.06140170323745024 0.03255841183319602 0.0001927115343330996; -0.06185254886048141 0.03268815199448967 0.00029588992432612673] % + +Mass Used: 1125.3822536870607 kg +Launch C3: 23.786963987590454 km²/s² +||V∞_in||: 11.153830742224367 km/s diff --git a/archive/EMJN_2021-11-29T20:07:38.430/plot.html b/archive/EMJN_2021-11-29T20:07:38.430/plot.html new file mode 100644 index 0000000..1d2ba60 --- /dev/null +++ b/archive/EMJN_2021-11-29T20:07:38.430/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJS b/archive/EMJS new file mode 100644 index 0000000..f013054 --- /dev/null +++ b/archive/EMJS @@ -0,0 +1,36 @@ +archive/EMJS--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-11-08T18:47:22.305 +Launch V∞: [-4.451427517503081, 4.380713257243984, 0.9509666906856978] km/s +Phase 1: + Planet: Mars + V∞_in: [-7.503625705871378, 2.9922534516224317, 0.3970744313528344] km/s + V∞_out: [-6.203985495450952, 5.1853077278089845, 0.19685948210225732] km/s + time of flight: 7.692258675246356e7 seconds + arrival date: 2026-04-17T02:10:28.305 + thrust profile: [-0.05747333201815444 0.01458857211306159 0.01661972438571343; -0.07640520733942768 -0.0880498378588422 0.009291396823580423; -0.0642351947881695 -0.14583843433809482 -0.01174256444385774; -0.03591836428259514 -0.19097919421877213 -0.030455634296288725; 0.0014696729268849598 -0.21419745388390338 -0.046332000137257384; 0.043321837437152184 -0.23281386608467833 -0.057269006919827066; 0.08487576000339314 -0.23180733654869165 -0.06400789992534636; 0.12836076596832638 -0.2345880635860211 -0.06663468113711396; 0.16914897842720558 -0.2202670166100522 -0.06608715415000553; 0.20331848204335912 -0.19904198276368773 -0.06263191481516477; 0.23625994800571543 -0.18017227778817843 -0.057302223507679384; 0.26476916718248283 -0.15037417766839517 -0.05026099494873699; 0.28150073209231896 -0.11974625587737671 -0.04226763198923683; 0.2911151952723726 -0.08935809631597122 -0.032922957893997004; 0.29662192049119385 -0.05630987736862665 -0.023018382921682446; 0.3163317621362404 -0.01253021176722935 -0.013235490847343547; 0.25582892879782015 0.03994726547045516 -0.0012262871620623078; 0.20630604157449897 0.09278869993819255 0.011047803244751797; 0.13239326442164706 0.18510472327622382 0.022309378373958296; 0.0678407381537921 0.24416553319280734 0.027187329287448894] % +Phase 2: + Planet: Jupiter + V∞_in: [-2.4066983016171593, 3.60782547580802, -0.0729666504902062] km/s + V∞_out: [2.378938038105792, 3.622859356538288, -0.17162450321036135] km/s + time of flight: 1.0365627669349712e8 seconds + arrival date: 2029-07-29T19:35:04.305 + thrust profile: [-0.08661540144522925 0.5452498417652726 0.01940681405322532; -0.3026836754787113 0.3296518390803253 0.005983402538334351; -0.3406876005629003 0.11833095428025397 0.003356530625833691; -0.2835305485605863 0.05826412825528092 0.02255167620704516; -0.2312925636505238 0.037264277244941184 0.05388961098566991; -0.18711959340793846 0.02248626525242582 0.07873824296078222; -0.1586634246283703 0.009933258699574466 0.0871013968397894; -0.13480225405151802 -0.0016459373751799647 0.08376814481354339; -0.11717491300808694 -0.011644771387652143 0.06591943652720958; -0.12385446642299068 -0.021486105366059834 0.04559099694744897; -0.09388047865743618 -0.028093190404018073 0.021912607207877112; -0.08329274681397837 -0.03442999409177474 0.004671009919336775; -0.074293683492257 -0.039542791582250804 -0.005853738709231158; -0.06633940754759032 -0.044531789384190786 -0.009552210711090501; -0.05819808497253237 -0.047725452096228235 -0.008621886584541672; -0.052136936558275115 -0.0524395749605876 -0.002738982045574738; -0.04346694186008132 -0.0559411143833451 0.005899905372803087; -0.019037945479989642 -0.06356156997525016 0.022900432372144015; 0.03382392128782208 -0.03750155602427737 -0.01509909397132852; 0.0372737888254289 -0.03393228709124474 -0.008856011117644847] % +Phase 3: + Planet: Saturn + V∞_in: [-1.348151617130741, 3.372644961627469, -0.15974064227398158] km/s + V∞_out: [0.5003596890905858, 0.5035022711921476, 0.4902757482488732] km/s + time of flight: 2.6430663321089447e8 seconds + arrival date: 2037-12-13T22:05:37.305 + thrust profile: [0.09042797681998876 0.08185621600988492 -0.005657240382538273; 0.08801730768503421 0.06654785786786777 -0.005370519173262853; 0.08823193892876004 0.06301303625131692 -0.005301669247083464; 0.09786240449059495 0.0767776838916466 -0.005515040644430515; 0.08471215842112331 0.09323975234752191 -0.004395184816667355; 0.06296777251631458 0.13453925938779707 -0.0025772294050847586; -0.0014186632217062752 0.15454606073890062 0.000798883942976955; -0.06382656189096726 0.14369239243391718 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--- /dev/null +++ b/archive/EMJS.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJSU_2021-11-11T04:50:20.773/mission b/archive/EMJSU_2021-11-11T04:50:20.773/mission new file mode 100644 index 0000000..52eb4f9 --- /dev/null +++ b/archive/EMJSU_2021-11-11T04:50:20.773/mission @@ -0,0 +1,43 @@ +/home/connor/projects/thesis/archive/EMJSU_2021-11-11T04:50:20.773/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1977-08-29T00:28:42.235 +Launch V∞: [-5.993015939919875, 2.5730948883971196, 1.0995056788128965] km/s +Phase 1: + Planet: Mars + V∞_in: [-4.912918793015281, -5.749282630615395, 3.500451711966386] km/s + V∞_out: [-3.4658376295259443, -6.128480904546313, 4.458055817928218] km/s + time of flight: 9.655561330465347e7 seconds + arrival date: 1980-09-19T13:28:55.235 + thrust profile: [-0.6848479340229933 -0.6317473532438761 -0.6789410387377113; -0.7283373129568128 -0.6597015909585692 -0.6860291664652663; 0.5143122109172585 -0.7554166841816019 0.6548911297971178; 0.650987105546092 -0.739938250992294 0.686244011796856; -0.567349081163571 -0.7171322204555259 0.7176501535009572; -0.6060664652754209 -0.6881472823274762 0.7152061841403491; -0.6457752364426499 -0.6793453331017747 0.6901800477645527; 0.6373998427205125 -0.6901370973195071 0.6440943571979044; 0.6232981297616063 0.6245585478937647 -0.7042650672249426; -0.7173110561506139 0.47022815205529234 -0.6937264189108627; -0.6298819082617076 -0.7335307650242696 0.6794508601033687; -0.5840798229168693 -0.7117652775560642 0.71673753565496; 0.6518652084909865 -0.679625481136191 0.7150981814535525; 0.6269343446266082 -0.6783434977916609 0.7005711370434008; 0.6192953242902497 -0.6895768905181153 0.66192822798728; 0.6249355751156056 0.6111710277362319 -0.6978924565831346; -0.7127959821946511 0.5739058413985498 -0.7071394367657958; 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0.003803922133384859; 0.19913721147690577 -0.22075888291860724 -0.0002865981573597917; 0.23289402715561758 -0.21456195491530816 -0.00412606331776826; 0.2635970662374559 -0.21101943812025215 -0.007646212949431516; 0.29197382006432404 -0.21013550409926826 -0.010839526103107245] % +Phase 4: + Planet: Uranus + V∞_in: [-0.6121969849040167, -7.150375871374237, -0.13070109116611242] km/s + V∞_out: [0.0007739939100291959, -0.03314950424200176, -7.94754221529655e-5] km/s + time of flight: 1.767996002536118e8 seconds + arrival date: 1995-08-05T05:28:57.235 + thrust profile: [0.06556180290998989 -0.4810097896203703 0.001892764138566078; 0.05798846767670954 -0.45547090983767 0.0021156315191879025; 0.051689770885915726 -0.42832132722472177 0.0022959057542090914; 0.04648700280108465 -0.39928121074291384 0.0024336442919551666; 0.0422028841595979 -0.3680710941209755 0.002508087270289503; 0.03867267523413679 -0.3344021401798511 0.002525995849605425; 0.03572097003592147 -0.29802013051252274 0.0024864926364152923; 0.03318882991262833 -0.2587147803564456 0.0023938091349767227; 0.03090542603076421 -0.2163770501304412 0.0022582652803209927; 0.028677181687678518 -0.17104667286314865 0.002097118557040994; 0.02619154533459498 -0.12299356889209265 0.0019574717120907272; 0.022731235300107018 -0.07291026524510676 0.0019498981886554635; 0.013464668655989014 -0.024663380581525153 0.0024792489578653563; 0.022851842286257088 -0.0034654943191003017 -0.0014195501664108637; 0.01695459135761096 0.042960833303929385 0.00027136301763064255; 0.019109715763285105 0.0939108023750647 -0.0006238697198316213; 0.019041699615714294 0.14424641548655956 -0.001297833776791727; 0.0181625271663931 0.1928667562989665 -0.0018850620022324046; 0.016846067007602567 0.23934680582993179 -0.002459940248822858; 0.015214354318562582 0.2834687949061578 -0.003064218239253031] % + +Mass Used: 2673.1939593971797 kg +Launch C3: 43.74597009857089 km²/s² +||V∞_in||: 7.1777254771611645 km/s diff --git a/archive/EMJSU_2021-11-11T04:50:20.773/plot.html b/archive/EMJSU_2021-11-11T04:50:20.773/plot.html new file mode 100644 index 0000000..6f7b8dd --- /dev/null +++ b/archive/EMJSU_2021-11-11T04:50:20.773/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJS_2021-10-18T22:47:27.423/mission b/archive/EMJS_2021-10-18T22:47:27.423/mission new file mode 100644 index 0000000..1ea6681 --- /dev/null +++ b/archive/EMJS_2021-10-18T22:47:27.423/mission @@ -0,0 +1,36 @@ +archive/EMJS_2021-10-18T22:47:27.423/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 1978-01-03T10:43:56.684 +Launch V∞: [-3.9272284612384682, 1.103272773876818, 0.5261327502187312] km/s +Phase 1: + Planet: Mars + V∞_in: [-4.302171521788235, -0.9224228322302193, -1.14321961684719] km/s + V∞_out: [-3.884897307404638, 2.338666041291152, -0.3214778995965392] km/s + time of flight: 4.342577286549467e7 seconds + arrival date: 1979-05-21T01:26:48.684 + thrust profile: [-0.013447144151271642 -0.03768936107210863 -0.016368572374325367; -0.011844904106064317 -0.02655981602735897 0.04457863849948758; 0.004072854216357777 -0.06638130237888651 0.08240263777419533; 0.02275688493856809 -0.11176740369554655 0.10543301498940685; 0.045760812777573635 -0.1494893115542728 0.13159970546846236; 0.07695648098710427 -0.2178829328468449 0.16954108284269187; 0.13157259005460648 -0.23862770794850882 0.20680275357201225; 0.20764505272897338 -0.2465698722765297 0.20163109585168845; 0.269333209504411 -0.2588680411909609 0.21321916585564238; 0.32998447568721123 -0.2680930176939294 0.21619301937830762; 0.37620045883152436 -0.2724317467650694 0.21675621863459776; 0.4323971239602839 -0.27348332645907797 0.21102218660275301; 0.4703186634081572 -0.2708338296152373 0.2048610047676473; 0.3597048908164455 -0.30168467216940215 0.22271019411557225; 0.5595433516897296 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specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1977-07-15T09:14:38.873 +Launch V∞: [2.5147318268598355, -1.1103623444144004, -6.402642134012201] km/s +Phase 1: + Planet: Mars + V∞_in: [1.4161036678756145, -1.1612060546662615, 2.9720800484503234] km/s + V∞_out: [-0.90804226462538, -3.0734160134493123, 1.3849536778316178] km/s + time of flight: 8.105040003981963e7 seconds + arrival date: 1980-02-08T11:14:38.873 + thrust profile: [0.627838637604648 -0.12503628432096117 0.7855611132388014; -0.5289458287476022 0.6777841575676512 0.7075837038292085; -0.2373838703336668 0.7909345611869171 0.4331633366544985; 0.5432353517595965 0.7768839631178791 -0.783167310773754; 0.5396869301168233 0.7683167946626912 -0.7571970728573518; 0.23588696621684396 0.7769451734643089 -0.7270972946851668; -0.7694041770581667 0.601335658849241 -0.6637596322235111; -0.7921780190588894 -0.600905356962876 -0.44048431937604654; 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-0.08720444491924713; 0.3416336893889104 -0.37382177982174647 -0.05355021694096375; 0.3922447283373164 -0.35961171719778656 -0.03138748595138845; 0.4272895758116155 -0.3267679698520526 -0.017497312957446522; 0.4465876315319068 -0.2826782360645849 -0.008534675888530218; 0.4531265921438839 -0.2323243789797917 -0.002376606148144884; 0.4495616785265872 -0.18074814564085967 0.0023041257879340494; 0.4380764579262854 -0.1330536192097116 0.005943447204693447; 0.42071889349085684 -0.09344905521564274 0.008645824111706685; 0.3990398415062969 -0.06332998130635517 0.011593397065563935; 0.3717084241277894 -0.04056062633087571 0.0157282909739208; 0.33657096418837157 -0.017725329809315477 0.03801942779075905; 0.32630435662337576 0.0002709235371287296 0.033211487884096974] % + +Mass Used: 2627.443374929516 kg +Launch C3: 48.55060699314355 km²/s² +||V∞_in||: 8.548229045965172 km/s diff --git a/archive/EMJS_2021-11-10T17:54:03.858/plot.html b/archive/EMJS_2021-11-10T17:54:03.858/plot.html new file mode 100644 index 0000000..c5db2a2 --- /dev/null +++ b/archive/EMJS_2021-11-10T17:54:03.858/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJS_2021-11-10T18:46:26.719/mission b/archive/EMJS_2021-11-10T18:46:26.719/mission new file mode 100644 index 0000000..8a62363 --- /dev/null +++ b/archive/EMJS_2021-11-10T18:46:26.719/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJS_2021-11-10T18:46:26.719/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 1977-08-28T19:16:48.911 +Launch V∞: [-0.9048124421086198, 1.9143247567671402, 1.0655764532581016] km/s +Phase 1: + Planet: Mars + V∞_in: [-2.4343783407486486, -4.687961859367619, -2.933139307760753] km/s + V∞_out: [-4.790214200771935, -2.8588778216214474, -2.321748592254448] km/s + time of flight: 1.2520840640242675e8 seconds + arrival date: 1981-08-16T23:23:34.911 + thrust profile: [-0.6224581879584439 0.4288059372368617 -0.369846309902295; -0.8456103096731954 -0.5449676132404117 -0.5207697451591612; -0.8002461593492456 -0.855950096213463 -0.3124435417439843; -0.08909026312356522 -0.8654901195188492 0.07012982568146232; 0.680001252515441 -0.7588164444715032 0.36639076258430675; 0.5600241806519821 -0.5524736520531364 0.42732020550718447; 0.16764662042831702 -0.38130964149055036 0.34119753879891973; -0.731954705851045 0.09173304239444241 -0.3217028849043164; -0.8708852593282298 -0.20046295640353465 -0.47555463513488316; -0.8714792916879354 -0.8774730456609726 -0.40411815736943946; -0.7503507155222385 -0.8995426849328464 -0.19904254786993072; -0.21243617845242554 -0.8809796651748026 0.05347795073943726; 0.6472006222755674 -0.8484331643135395 0.11021347676692661; 0.7443657429086448 -0.7955146419656197 0.23886041656554424; 0.7440649663077856 -0.6390085790476502 0.3042575860828415; 0.37484890774561835 -0.37162261741629815 0.19144601961385382; -0.3550450393056071 -0.11435230249867454 -0.07617629787736838; -0.9195229993807225 0.2789170446342234 -0.2615678112840567; -0.9727616469871604 0.3446917247288234 -0.257471197235714; -0.9808492088715268 -0.5477259908772488 -0.44853687745916715] % +Phase 2: + Planet: Jupiter + V∞_in: [-6.701136691962909, -8.599974967150617, 1.3162577103992203] km/s + V∞_out: [-7.466152781006179, -7.773882414996021, -2.1024987830209496] km/s + time of flight: 5.836177608302693e7 seconds + arrival date: 1983-06-23T10:59:50.911 + thrust profile: [-0.9775204977097908 -0.5214058341481157 0.16197437982089447; -0.9681501773489387 -0.7500057879390385 0.22817317938497259; -0.9525762370469925 -0.832426651123316 0.28200011488079785; -0.92761259022897 -0.8555389932740242 0.3222489903321434; -0.8871450236047153 -0.8560245708679001 0.3479490816123863; -0.8195685407028787 -0.8487998122656493 0.3566147862452735; -0.7790460014892773 -0.8311841138895902 0.3582600049182118; -0.6190731426200151 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2.520438083264169e8 seconds + arrival date: 1991-06-18T15:09:58.911 + thrust profile: [-0.09400215473661182 -0.18945521309217062 0.1271918910889239; -0.08607974390576098 -0.15730289401708353 0.1330350509096681; -0.07832275239134029 -0.13478208666438357 0.1351441081454202; -0.07132837621235137 -0.11668356299904072 0.13473290589837142; -0.06422308680008934 -0.10329018345067097 0.13124190941207606; -0.05483219880785128 -0.09065397169544913 0.12875633044650717; -0.04534456797231015 -0.07960292266050767 0.12395016513276043; -0.0352252711827991 -0.07015964172632169 0.11766514477500203; -0.02415557927465716 -0.06150640906378341 0.11072639537362276; -0.012611759737086297 -0.05352376356987194 0.1025041600979924; -0.0005755408110000229 -0.044830667850551016 0.09493441557954609; 0.019044842896509144 -0.04345125363942511 0.07403861776967349; 0.02592414982088686 -0.030002827924179683 0.0741211457115302; 0.0402832985262284 -0.023419092869979216 0.061815224815860395; 0.054217569381438825 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+/home/connor/projects/thesis/archive/EMJS_2021-11-29T21:44:47.574/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-06-24T11:13:35.652 +Launch V∞: [4.204198767059533, -9.994451029411268, 4.407763020256069] km/s +Phase 1: + Planet: Mars + V∞_in: [1.1816902279242838, -9.996430420980913, -3.9141617445235055] km/s + V∞_out: [0.37910175293619774, -9.534044813617678, -5.060049667159223] km/s + time of flight: 4.577040007583382e7 seconds + arrival date: 2024-12-05T05:13:35.652 + thrust profile: [-0.6281059032448896 -0.9645978361567867 0.04825409754226176; -0.8740723336039602 -0.9597496199427967 0.05604914227980348; -0.897647871256038 -0.9575735835349201 0.09800966403698955; -0.8947340470580677 -0.9548346668410663 0.15634176550887674; -0.8837997723274917 -0.9506389891549062 0.2119922535014052; -0.8733870717624931 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+Mass Used: 2029.541947000274 kg +Launch C3: 136.99271349498176 km²/s² +||V∞_in||: 1.748544813193361 km/s diff --git a/archive/EMJS_2021-11-29T21:44:47.574/plot.html b/archive/EMJS_2021-11-29T21:44:47.574/plot.html new file mode 100644 index 0000000..1866930 --- /dev/null +++ b/archive/EMJS_2021-11-29T21:44:47.574/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJS_2021-11-29T21:56:54.243/mission b/archive/EMJS_2021-11-29T21:56:54.243/mission new file mode 100644 index 0000000..a372c50 --- /dev/null +++ b/archive/EMJS_2021-11-29T21:56:54.243/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJS_2021-11-29T21:56:54.243/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-02-03T22:31:58.060 +Launch V∞: [-9.983658485652342, 5.052584189132008, 8.454011703658189] km/s +Phase 1: + Planet: Mars + 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0.4786693481341792; 0.9260901378249389 0.8482781912744276 0.4059545252589148; 0.931827122595938 0.8695510665682376 0.27969911096378186; 0.9351654063561202 0.8873770941740391 0.0557896800207434; 0.9359855094240302 0.9011770122818098 -0.21365898834998476; 0.9338922411647969 0.910802339678919 -0.365757719064907; 0.9278284047571169 0.9146993842728531 -0.45267349649595484; 0.9177962416138067 0.9074601171998934 -0.48335462518998995] % +Phase 2: + Planet: Jupiter + V∞_in: [-4.046083430194879, 6.572285306163753, 0.7499685576972142] km/s + V∞_out: [-6.445354159446693, 3.323503238892241, 2.745880595515267] km/s + time of flight: 6.991559948627624e7 seconds + arrival date: 2028-07-08T07:33:45.060 + thrust profile: [0.5340118690878064 0.8946355483481895 -0.6067329080424446; -0.3678947664519958 0.8593146540157065 -0.5131755344574285; -0.39005831784853146 0.7991144657043887 -0.41508437369833046; -0.10776295134122015 0.7502923022084157 -0.3752944615562001; 0.17190209160722916 0.7255675171054287 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b/archive/EMJS_2021-11-29T22:43:36.591/mission new file mode 100644 index 0000000..6c82714 --- /dev/null +++ b/archive/EMJS_2021-11-29T22:43:36.591/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJS_2021-11-29T22:43:36.591/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-06-09T17:38:19.762 +Launch V∞: [-1.1540177007372212, 5.360837098498792, 0.2984944317979115] km/s +Phase 1: + Planet: Mars + V∞_in: [-2.0043098166092546, 1.5028334917558672, 1.4743578319466457] km/s + V∞_out: [-0.8356117752464607, 0.15439829082406908, 2.7798876463250943] km/s + time of flight: 1.5586920017281148e8 seconds + arrival date: 2029-05-18T18:38:19.762 + thrust profile: [0.1725379661821492 0.3028636782963449 -0.14594530225449512; 0.24010663973374377 0.25478985696879275 0.09151945430842105; 0.11381352719375167 0.3130894749849403 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0.2491356450509427 -0.508230954127345 0.12331066638000482] % +Phase 2: + Planet: Jupiter + V∞_in: [5.611204987956414, 1.0148015551991953, -0.05634775428610248] km/s + V∞_out: [-1.1695945563190893, -1.5488819990446605, 5.3620550672788685] km/s + time of flight: 2.0545559999887675e8 seconds + arrival date: 2035-11-21T17:38:18.762 + thrust profile: [0.5107734951887763 -0.3946064078009902 -0.0045676369422384165; 0.4598697444727305 -0.20748812220867774 0.059353622926187184; 0.33581510576782936 -0.407189511957922 0.15987153660020692; 0.3794276589018478 -0.37511266169747637 0.14960397348233373; 0.13533934017940225 -0.5031320027541039 0.08209543124670671; 0.4245206324807559 -0.6227802169786933 0.05650960675506308; 0.6558675736258086 -0.3397032003626548 0.03308794472495331; 0.5120131659823914 0.2924383586904873 0.05184380445957168; 0.34826053012663044 0.014522849649912385 0.19696263006429715; 0.041523907241033706 -0.3360187093015938 0.21706268681577065; -0.3475762260365926 -0.48685037074106274 0.1315856784159298; -0.3743319370307219 -0.6764350725170731 0.0903118551039194; 0.5097342414424403 -0.7734829334242606 0.09514159989066195; 0.7845273733985942 -0.5753935364819165 0.029842770779258728; 0.7315778039847924 0.3432605037934376 0.004749315755486527; 0.5968872158984753 0.44198729718418783 0.051253635005704054; 0.42636307680116 0.379616657506637 0.10303815501796434; 0.22195498303040814 0.27300879237608766 0.14632762929547719; -0.024188484440234567 0.13680033465416566 0.18166786525750667; -0.25695040241576644 -0.0340498293709866 0.19810666574939037] % +Phase 3: + Planet: Saturn + V∞_in: [-5.337830290816849, -1.2797414036157133, -2.7683894000988465] km/s + V∞_out: [-0.10980431423849103, -0.03384798680602295, 0.02827033505965302] km/s + time of flight: 1.8897119999873626e8 seconds + arrival date: 2041-11-16T21:38:17.762 + thrust profile: [-0.18827080027303889 -0.0037944481429670707 -0.03587675027570545; -0.19565231042967327 0.005129353701615244 -0.0491082915163806; 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+Launch Mass: 3500.0 kg +Launch Date: 2024-04-23T20:49:35.793 +Launch V∞: [-2.4450865737116274, -4.101829409199476, -0.21378743337924264] km/s +Phase 1: + Planet: Mars + V∞_in: [-3.9454321781223207, -4.3349983737367435, -0.23163519766252774] km/s + V∞_out: [-5.484540365422154, -1.7912021635297986, -1.0612283164832435] km/s + time of flight: 1.3168651513492899e8 seconds + arrival date: 2028-06-26T00:24:50.793 + thrust profile: [-0.120722733695335 -0.012176360827686798 -0.030518390794883023; -0.11679617667506606 0.0014999178722870938 -0.035606031789671; -0.07727822397577828 0.3037973459191278 -0.0585534522901871; -0.223884565034074 0.38469778038311786 -0.018658505423278564; -0.5047726947284132 0.1198586588428443 0.04363822566057665; -0.36008917896849646 -0.046966759269397945 -0.012020139167426613; -0.2303697349032088 -0.18990779273074385 -0.1162523931176612; -0.009059953396105604 -0.1826064551186425 -0.09566243569922224; 0.06464171493355703 0.15348717344682897 -0.03592117858719949; 0.039222535062581575 0.45251270837425567 -0.002237551646205031; -0.3129537896040898 0.5005808668195679 0.06976206030714757; -0.6334356581244346 0.342167669148952 0.08785885490233064; -0.6259891593556097 0.07036975867629339 -0.029340487056482453; -0.45498760154179435 -0.5093792240633872 -0.13924939952781157; 0.03362679051118392 -0.46176686054217253 -0.15798494014212214; 0.4358161230258788 -0.13839418528576888 -0.05039097669674436; 0.3044870713576448 0.4992315283787602 -0.0039116386904277205; 0.17193614377332783 0.7613325121786818 0.03200649181430257; -0.5572427328043519 0.7854289375339618 0.10069718693059672; -0.7044302858314516 0.6325274227780806 0.1358242855667267] % +Phase 2: + Planet: Jupiter + V∞_in: [-4.177197074414225, -0.9720140804548069, 0.2337469329489975] km/s + V∞_out: [-1.1897818013258668, 4.123843236773216, -0.16384853893411477] km/s + time of flight: 1.0354715657281214e8 seconds + arrival date: 2031-10-07T11:30:46.793 + thrust profile: [-0.9480754862164437 0.3056342864181156 0.04775925131934315; -0.9545036085062072 -0.08916062469268374 0.07006956877613481; -0.8556415500647792 -0.5308952023053652 0.07581953613413958; -0.6525116764830651 -0.6804771046594907 0.072044066669931; -0.4141337602665943 -0.687613497545176 0.06325121629083955; -0.2876119881822729 -0.56915707346219 0.04608924218869737; -0.23061087236806183 -0.4285889382631892 0.0353521662171739; -0.21444588630200445 -0.2987113553031206 0.00894677998389626; -0.2042602334001383 -0.19716033565885058 -0.010540546258761902; -0.19797650808153522 -0.05516030431031445 -0.02296358167357804; -0.17870024970353923 -0.051487903415797315 -0.028673002243452296; -0.16087764941466745 -0.006028156883433786 -0.029496266489663633; -0.13249691125920962 0.010594568264314964 -0.03373869555595076; -0.1023119680343583 0.024125699413220757 -0.03194152432595998; -0.06667052712715316 0.022162434908797966 -0.0413032534053769; -0.02650461479736716 0.019860230188950657 -0.02825273461209873; 0.008483997200284142 0.010514866140007597 -0.027548374980192067; 0.044674954681201196 0.010390355078242345 -0.02558959064331584; 0.0698391445723141 0.01711123350841671 -0.025534958302052144; 0.07369308900718043 0.036955143265610016 -0.01808340139735954] % +Phase 3: + Planet: Saturn + V∞_in: [-2.855151769198392, 1.832432120626587, 0.030050486577809125] km/s + V∞_out: [0.043566731882813375, 0.1453515199166137, 1.1921829828355344] km/s + time of flight: 2.616408348306797e8 seconds + arrival date: 2040-01-21T17:31:20.793 + thrust profile: [0.04225281791313958 0.029025037669065452 -0.0022530954062099607; 0.03735188618997079 0.03969404585926613 -0.001990942517015921; 0.027816672613794786 0.05946905402188188 -0.0018579377168727645; 0.013243713257944257 0.07889753909094255 -0.0012755910819474462; -0.012739124713320801 0.09684893162964908 1.027454400474268e-5; -0.04822800674369958 0.09918628844749049 0.0017567047619653946; -0.07935450012796613 0.08394550684634153 0.0037636317001541555; -0.096945253591464 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b/archive/EMJS_2021-11-30T00:34:25.423/plot.html new file mode 100644 index 0000000..0575a10 --- /dev/null +++ b/archive/EMJS_2021-11-30T00:34:25.423/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJS_2021-11-30T02:33:04.261/mission b/archive/EMJS_2021-11-30T02:33:04.261/mission new file mode 100644 index 0000000..ef91d65 --- /dev/null +++ b/archive/EMJS_2021-11-30T02:33:04.261/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJS_2021-11-30T02:33:04.261/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-10-05T00:35:20.996 +Launch V∞: [-3.2137533909207794, 5.084712824855146, 1.430949155734375] km/s +Phase 1: + Planet: Mars + V∞_in: [-6.255155316138288, 6.606484457110347, -0.23100377774853306] km/s + V∞_out: [-7.465384617443416, 5.187341596386573, -0.43088705744489453] km/s + time of flight: 1.3257925555072227e7 seconds + arrival date: 2025-03-07T11:20:45.996 + thrust profile: [-0.007759166593782 0.008081441978955738 0.004825043238403784; -0.011235947824502553 0.006629595221827023 0.005298768481147631; -0.014134476908100888 0.004950559801138478 0.006335721099905584; -0.016912120418734602 0.0032538753168045408 0.00722543103380731; -0.019615343774186608 0.0015764448870706 0.00791543407768123; -0.02224614170581595 -0.0003222442781983473 0.008542627265521198; -0.024752022364092727 -0.002502638264186997 0.009081125608978445; -0.027074692908356103 -0.0049669389909122045 0.009549338120131428; -0.02919125492967198 -0.007632280649054239 0.00984618903400726; -0.031034823850380824 -0.0105147854228823 0.010076901834442997; -0.03258867449421671 -0.013557927955447253 0.010239842439460488; -0.033896907887579285 -0.01664233072935544 0.01017836634561616; -0.034798910393570345 -0.01976899064579983 0.0104762622470642; -0.035510243080800585 -0.023010543051237668 0.010185800368979887; 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-0.10811409035917058 -0.009477194232797893 -0.012143321662504066; -0.10924801926559909 0.14082268122578098 -0.05670682044948156; -0.029758444441605168 0.28004126085284164 -0.08287077095226834; -0.005277793889388453 0.43294397265469803 -0.08212135825686287; -0.32054145122009575 0.5753532885361126 -0.03968329559118082; -0.6812467539999161 0.3089367113933967 0.051808034060789085; -0.6510836214832658 -0.4873937421666415 0.12520004751950561; -0.49557588979996686 -0.512322294250635 0.15992845574394862; -0.34374129520368857 -0.5135522557199093 0.16537305271566424; -0.2240792189464561 -0.45518516492142325 0.1550538281965299; -0.13865236852037352 -0.37950308770911234 0.13394772771689303; -0.0785171269810383 -0.2978976352535766 0.10596692987800144; -0.035327531433840355 -0.21564018776939112 0.07474526871132638; -0.005605243694407901 -0.12702627457742785 0.04128648833249606; 0.01020681436565993 -0.02502132504960536 0.004261721313786419] % +Phase 3: + Planet: Saturn + V∞_in: [-1.9690596099587732, 3.2707822497004333, 0.03981900780395632] km/s + V∞_out: [5.114183571314532e-5, -0.00028059524048684205, -1.0322857139071202] km/s + time of flight: 2.4691764297066832e8 seconds + arrival date: 2038-08-10T18:57:38.996 + thrust profile: [-0.010548481282575234 0.04258751351881362 -0.025726963732731655; -0.01128130800439453 0.05537735517283375 -0.02522998253773597; 0.009886584360292121 0.08885355612430626 -0.02421777901196621; 0.034425823426465496 0.1204073126801249 -0.020057117827333014; 0.039281760158963876 0.14271215958548816 -0.013510596261601598; 0.018736852336642556 0.15327407334940432 -0.006130067311322509; -0.022719461407261828 0.1451025891518733 0.0027035496704120453; -0.04847577536899553 0.1212275153694897 0.010891420241408132; -0.06628322085560583 0.08574069656011961 0.01754569902422787; -0.0744351565286978 0.045598034397603175 0.023036321178276163; -0.06578589050933895 0.03204645107589838 0.02550340232781789; -0.06050564660450317 0.014954861896586048 0.022962687464765534; 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100644 index 0000000..d746ddb --- /dev/null +++ b/archive/EMJS_2021-11-30T08:40:36.355/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJS_2021-11-30T08:40:36.355/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-11-29T10:54:51.469 +Launch V∞: [-3.0580432001025106, 2.2375690420359073, 1.0588738801940067] km/s +Phase 1: + Planet: Mars + V∞_in: [-4.571073362651481, 1.5280878123442105, -0.45427388957404374] km/s + V∞_out: [-2.4964790697852464, 4.131812654452342, -0.3633277130442272] km/s + time of flight: 4.098218966605439e7 seconds + arrival date: 2026-03-18T18:51:20.469 + thrust profile: [0.02250623498780786 0.056715344804171675 -0.034873620216503566; -0.01586442265299213 -0.06295338578554689 0.08519483155847359; -0.01017916810128589 -0.13656445837778508 0.13681516443703864; 0.016841859589487678 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0.6250076852929124 -0.25134269316042973] % +Phase 2: + Planet: Jupiter + V∞_in: [-2.888718591099067, 2.98093500374621, -0.03527346962365893] km/s + V∞_out: [2.3790932465957977, 3.378686597227906, 0.3953591906305017] km/s + time of flight: 1.0806802469609727e8 seconds + arrival date: 2029-08-20T13:45:04.469 + thrust profile: [-0.23488496954455496 0.9896419507072445 -0.11601157743285787; -0.948717799093386 0.9810049502433882 -0.11137913018095054; -0.9878845940359288 0.8353827321448694 -0.08704039668042218; -0.9873512008683539 0.283891063339361 -0.05113640206170415; -0.9867884331885424 0.06209683131941994 -0.023752079481471355; -0.9535019575354626 0.09042898307599517 -0.006869177979295686; -0.8629780107614938 0.07500054807185184 0.004358596231624515; -0.7266566061890536 0.04691475374478784 0.014062645283394093; -0.5808329590842135 0.03171216226293981 0.01492806895495031; -0.45651135691182687 0.02498400153146004 0.02067482320548018; -0.35501493081559393 0.019422083647277044 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duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-12-15T22:51:31.653 +Launch V∞: [1.0265298829626757, -6.097752351134353, 0.6856608803521997] km/s +Phase 1: + Planet: Mars + V∞_in: [-0.685353880716249, -3.6396637778190533, -3.2013166230561305] km/s + V∞_out: [0.5302103364593528, -0.9765757196202859, -4.767844807662866] km/s + time of flight: 9.971640000084461e7 seconds + arrival date: 2028-02-13T01:51:31.653 + thrust profile: [0.13284751649644205 0.9411989426214641 -0.46977683989334873; -0.968547907767294 0.9608251103851381 0.49339267132424175; -0.9787154450158303 -0.8432228864566057 -0.5543030062336614; -0.9458849725429278 -0.9442327236046363 -0.7636886633819076; -0.9667535016847152 -0.7358061408218618 -0.11636279319023346; -0.9820303864106136 0.7930475060706941 0.4962497106503541; -0.971227150319471 -0.986463218458502 0.4632222480421968; -0.9271319319791395 -0.8917240929018778 -0.6101593732712101; -0.9139137651217345 -0.5324029885065178 -0.8083289582144534; -0.9773913889808017 0.991657638900593 -0.4106474876750948; -0.990512335176245 0.7321537085435096 0.6605421761973608; -0.9581179828820583 -0.984882219664571 0.6421847460531694; 0.9803502761290055 -0.9432783942684786 -0.7125092685705092; 0.584101463120002 0.9947933997204838 -0.8808317684328829; -0.993526887524295 0.9941311908456837 -0.7387372801949493; -0.9957384470386984 0.9741994738088207 0.5708597976999408; -0.9915748324180956 -0.9960584321805054 0.8295257560724948; 0.9959387668352474 -0.9942746434271464 0.1695440717133519; 0.9960944736420316 0.8745766502055389 -0.7915289853600778; 0.9903811167032217 0.9961817491550279 -0.9573032378642442] % +Phase 2: + Planet: Jupiter + V∞_in: [2.090864620573387, -3.222147331578074, -2.509087132015622] km/s + V∞_out: [-4.488106073949989, -0.5175537490206633, 0.7987014856646427] km/s + time of flight: 1.6423199999993336e8 seconds + arrival date: 2033-04-27T21:51:30.653 + thrust profile: [-0.5660855310698739 0.9967906693759188 -0.8209919327744069; 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0.7031513931411775 -0.3631789642405433 -0.03783836908358169; 0.8144978524655395 -0.5249342706264041 -0.03246396629051213; 0.8897103992638571 -0.708341160251077 -0.03341117930579575] % +Phase 3: + Planet: Saturn + V∞_in: [-9.950524772292589, 2.7136858826882397, 0.8437847433534009] km/s + V∞_out: [-3.9746513384546427, 3.419068378994426, -0.22492206192340505] km/s + time of flight: 2.4062400000004002e8 seconds + arrival date: 2040-12-11T21:51:30.653 + thrust profile: [-0.026861539030662098 0.053037742486198663 -0.03998103891716118; -0.4005257165378705 0.12385064839383274 0.04228749257228828; 0.11316689356297174 -0.5002033317813458 0.0920099903831136; -0.4310529749448192 -0.3737769540652961 -0.16434453658789766; 0.524935339397772 0.326736433374278 -0.011049835879189725; 0.2870548648523757 0.9008250510979924 0.043684490460944636; -0.2578688762031856 0.6811275515417524 0.06979705435650777; -0.16643689458434993 0.44448647933073615 0.03748178826678883; 0.03135747943986613 0.09121026982102139 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b/archive/EMJS_2021-11-30T13:52:11.363/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJS_2021-11-30T14:09:25.262/mission b/archive/EMJS_2021-11-30T14:09:25.262/mission new file mode 100644 index 0000000..89d4a0e --- /dev/null +++ b/archive/EMJS_2021-11-30T14:09:25.262/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJS_2021-11-30T14:09:25.262/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-11-16T09:01:46.766 +Launch V∞: [-1.2358227541627522, 0.323049558821953, 2.495135844447432] km/s +Phase 1: + Planet: Mars + V∞_in: [-5.492217326783208, -0.7599139192265875, -0.7445133837270346] km/s + V∞_out: [-4.404936994877108, -3.4463054890902294, 0.12597397946441688] km/s + time of flight: 1.1637720070766585e8 seconds + arrival date: 2027-07-25T08:01:46.766 + thrust profile: [0.01055136636996065 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2041-05-30T12:01:47.766 + thrust profile: [-0.1762427833398218 0.018451914856523026 -0.33296833868061293; -0.10855107710674605 0.044463310211183146 -0.33965829997250213; -0.04955955263781527 0.10666486336804054 -0.3343168817737069; -0.14933152742910255 0.1645563456813175 -0.2888802750452695; -0.011372547689235173 -0.39964858425741717 0.1289083844812905; 0.17913823101853307 0.33922366300742973 0.3624022918784145; -0.056147608885838356 0.40536943517001855 0.2345805092442894; -0.11646645449972745 0.37970664664911913 0.13215537014712256; -0.10774775336158972 0.3637144687183163 0.07982907905717164; -0.03689877185389765 0.36730516793108037 0.04229495484147119; 0.08041474785484633 0.3975271403801768 0.011450007794323156; 0.2209067582381832 0.4645747308847809 -0.016359218295681436; 0.29077903309671577 0.5746646081920227 -0.03785392741655643; -0.5440697079277356 0.7004154769551414 -0.02197571950265878; -0.5081898184366466 0.06445088273594297 0.0502311733117999; -0.19802320496526152 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+||V∞_in||: 2.021342590587859 km/s diff --git a/archive/EMJS_2021-11-30T15:47:59.016/plot.html b/archive/EMJS_2021-11-30T15:47:59.016/plot.html new file mode 100644 index 0000000..563b16c --- /dev/null +++ b/archive/EMJS_2021-11-30T15:47:59.016/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJS_2021-11-30T16:38:03.240/mission b/archive/EMJS_2021-11-30T16:38:03.240/mission new file mode 100644 index 0000000..c185c63 --- /dev/null +++ b/archive/EMJS_2021-11-30T16:38:03.240/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJS_2021-11-30T16:38:03.240/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-12-14T15:10:10.657 +Launch V∞: [-5.324790803109733, -2.6773113758857146, 0.3590879071328112] km/s +Phase 1: + Planet: Mars + V∞_in: [-7.8280744026110485, -4.482906734167364, -0.5270128091140733] 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a/archive/EMJS_2021-12-01T15:04:58.660/mission b/archive/EMJS_2021-12-01T15:04:58.660/mission new file mode 100644 index 0000000..6e163b8 --- /dev/null +++ b/archive/EMJS_2021-12-01T15:04:58.660/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMJS_2021-12-01T15:04:58.660/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-11-08T18:47:22.305 +Launch V∞: [-4.451427517503081, 4.380713257243984, 0.9509666906856978] km/s +Phase 1: + Planet: Mars + V∞_in: [-7.503625705871378, 2.9922534516224317, 0.3970744313528344] km/s + V∞_out: [-6.203985495450952, 5.1853077278089845, 0.19685948210225732] km/s + time of flight: 7.692258675246356e7 seconds + arrival date: 2026-04-17T02:10:28.305 + thrust profile: [-0.05747333201815444 0.01458857211306159 0.01661972438571343; -0.07640520733942768 -0.0880498378588422 0.009291396823580423; -0.0642351947881695 -0.14583843433809482 -0.01174256444385774; -0.03591836428259514 -0.19097919421877213 -0.030455634296288725; 0.0014696729268849598 -0.21419745388390338 -0.046332000137257384; 0.043321837437152184 -0.23281386608467833 -0.057269006919827066; 0.08487576000339314 -0.23180733654869165 -0.06400789992534636; 0.12836076596832638 -0.2345880635860211 -0.06663468113711396; 0.16914897842720558 -0.2202670166100522 -0.06608715415000553; 0.20331848204335912 -0.19904198276368773 -0.06263191481516477; 0.23625994800571543 -0.18017227778817843 -0.057302223507679384; 0.26476916718248283 -0.15037417766839517 -0.05026099494873699; 0.28150073209231896 -0.11974625587737671 -0.04226763198923683; 0.2911151952723726 -0.08935809631597122 -0.032922957893997004; 0.29662192049119385 -0.05630987736862665 -0.023018382921682446; 0.3163317621362404 -0.01253021176722935 -0.013235490847343547; 0.25582892879782015 0.03994726547045516 -0.0012262871620623078; 0.20630604157449897 0.09278869993819255 0.011047803244751797; 0.13239326442164706 0.18510472327622382 0.022309378373958296; 0.0678407381537921 0.24416553319280734 0.027187329287448894] % +Phase 2: + Planet: Jupiter + V∞_in: [-2.4066983016171593, 3.60782547580802, -0.0729666504902062] km/s + V∞_out: [2.378938038105792, 3.622859356538288, -0.17162450321036135] km/s + time of flight: 1.0365627669349712e8 seconds + arrival date: 2029-07-29T19:35:04.305 + thrust profile: [-0.08661540144522925 0.5452498417652726 0.01940681405322532; -0.3026836754787113 0.3296518390803253 0.005983402538334351; -0.3406876005629003 0.11833095428025397 0.003356530625833691; -0.2835305485605863 0.05826412825528092 0.02255167620704516; -0.2312925636505238 0.037264277244941184 0.05388961098566991; -0.18711959340793846 0.02248626525242582 0.07873824296078222; -0.1586634246283703 0.009933258699574466 0.0871013968397894; -0.13480225405151802 -0.0016459373751799647 0.08376814481354339; -0.11717491300808694 -0.011644771387652143 0.06591943652720958; -0.12385446642299068 -0.021486105366059834 0.04559099694744897; -0.09388047865743618 -0.028093190404018073 0.021912607207877112; -0.08329274681397837 -0.03442999409177474 0.004671009919336775; -0.074293683492257 -0.039542791582250804 -0.005853738709231158; -0.06633940754759032 -0.044531789384190786 -0.009552210711090501; -0.05819808497253237 -0.047725452096228235 -0.008621886584541672; -0.052136936558275115 -0.0524395749605876 -0.002738982045574738; -0.04346694186008132 -0.0559411143833451 0.005899905372803087; -0.019037945479989642 -0.06356156997525016 0.022900432372144015; 0.03382392128782208 -0.03750155602427737 -0.01509909397132852; 0.0372737888254289 -0.03393228709124474 -0.008856011117644847] % +Phase 3: + Planet: Saturn + V∞_in: [-1.348151617130741, 3.372644961627469, -0.15974064227398158] km/s + V∞_out: [0.5003596890905858, 0.5035022711921476, 0.4902757482488732] km/s + time of flight: 2.6430663321089447e8 seconds + arrival date: 2037-12-13T22:05:37.305 + thrust profile: [0.09042797681998876 0.08185621600988492 -0.005657240382538273; 0.08801730768503421 0.06654785786786777 -0.005370519173262853; 0.08823193892876004 0.06301303625131692 -0.005301669247083464; 0.09786240449059495 0.0767776838916466 -0.005515040644430515; 0.08471215842112331 0.09323975234752191 -0.004395184816667355; 0.06296777251631458 0.13453925938779707 -0.0025772294050847586; -0.0014186632217062752 0.15454606073890062 0.000798883942976955; -0.06382656189096726 0.14369239243391718 0.004139373253375935; -0.09924285361658083 0.11731937511826053 0.006398669227156636; -0.11580556499542272 0.09241219909488727 0.007641311131976814; -0.12704630471212713 0.0755704468000314 0.008542821687616114; -0.13059068423655953 0.05648447252052886 0.008518267583078705; -0.1375065378923194 0.029657327876499343 0.007947474105719379; -0.12731258715678567 -0.013661649213132244 0.005928368352642089; -0.08615459629776862 -0.051365993070702234 0.003434419522338479; -0.06064751058410859 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duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-12-15T22:51:31.653 +Launch V∞: [1.0265298829626757, -6.097752351134353, 0.6856608803521997] km/s +Phase 1: + Planet: Mars + V∞_in: [-0.685353880716249, -3.6396637778190533, -3.2013166230561305] km/s + V∞_out: [0.5302103364593528, -0.9765757196202859, -4.767844807662866] km/s + time of flight: 9.971640000084461e7 seconds + arrival date: 2028-02-13T01:51:31.653 + thrust profile: [0.13284751649644205 0.9411989426214641 -0.46977683989334873; -0.968547907767294 0.9608251103851381 0.49339267132424175; -0.9787154450158303 -0.8432228864566057 -0.5543030062336614; -0.9458849725429278 -0.9442327236046363 -0.7636886633819076; -0.9667535016847152 -0.7358061408218618 -0.11636279319023346; -0.9820303864106136 0.7930475060706941 0.4962497106503541; -0.971227150319471 -0.986463218458502 0.4632222480421968; -0.9271319319791395 -0.8917240929018778 -0.6101593732712101; -0.9139137651217345 -0.5324029885065178 -0.8083289582144534; -0.9773913889808017 0.991657638900593 -0.4106474876750948; -0.990512335176245 0.7321537085435096 0.6605421761973608; -0.9581179828820583 -0.984882219664571 0.6421847460531694; 0.9803502761290055 -0.9432783942684786 -0.7125092685705092; 0.584101463120002 0.9947933997204838 -0.8808317684328829; -0.993526887524295 0.9941311908456837 -0.7387372801949493; -0.9957384470386984 0.9741994738088207 0.5708597976999408; -0.9915748324180956 -0.9960584321805054 0.8295257560724948; 0.9959387668352474 -0.9942746434271464 0.1695440717133519; 0.9960944736420316 0.8745766502055389 -0.7915289853600778; 0.9903811167032217 0.9961817491550279 -0.9573032378642442] % +Phase 2: + Planet: Jupiter + V∞_in: [2.090864620573387, -3.222147331578074, -2.509087132015622] km/s + V∞_out: [-4.488106073949989, -0.5175537490206633, 0.7987014856646427] km/s + time of flight: 1.6423199999993336e8 seconds + arrival date: 2033-04-27T21:51:30.653 + thrust profile: [-0.5660855310698739 0.9967906693759188 -0.8209919327744069; -0.994170631248832 0.9947713712108747 0.1448631429571182; -0.9945000494219841 0.9274125399233997 0.4897574376167066; -0.9894742986247569 -0.4507820161619902 0.4166941133651491; -0.9714202588117182 -0.7137518679961032 0.30094666125802183; -0.9405225764860856 -0.7041104481825169 0.1892804023301685; -0.8322614400348775 -0.6078444193505477 0.10175874680514145; -0.5733990958821588 -0.4496883690491375 0.04286046670382909; -0.2872975060978055 -0.27194044695575137 0.01185750904851918; -0.03409685881889757 -0.09226785043335413 0.0007765631982848799; 0.041566915656923824 -0.02743199843891902 0.0012223583050356183; 0.03704247583337095 0.003644238002607764 -0.0017388167642256004; 0.055997436147982374 -0.022254514712059217 -0.007208925051407416; 0.24811520314082097 -0.1362846587264196 -0.02883669922015275; 0.4207497452192147 -0.19686359679762824 -0.03935341240442315; 0.5330387060152292 -0.22897802946531448 -0.04350654265126503; 0.6138159398623063 -0.27334600431296685 -0.042974346394558584; 0.7031513931411775 -0.3631789642405433 -0.03783836908358169; 0.8144978524655395 -0.5249342706264041 -0.03246396629051213; 0.8897103992638571 -0.708341160251077 -0.03341117930579575] % +Phase 3: + Planet: Saturn + V∞_in: [-9.950524772292589, 2.7136858826882397, 0.8437847433534009] km/s + V∞_out: [-3.9746513384546427, 3.419068378994426, -0.22492206192340505] km/s + time of flight: 2.4062400000004002e8 seconds + arrival date: 2040-12-11T21:51:30.653 + thrust profile: [-0.026861539030662098 0.053037742486198663 -0.03998103891716118; -0.4005257165378705 0.12385064839383274 0.04228749257228828; 0.11316689356297174 -0.5002033317813458 0.0920099903831136; -0.4310529749448192 -0.3737769540652961 -0.16434453658789766; 0.524935339397772 0.326736433374278 -0.011049835879189725; 0.2870548648523757 0.9008250510979924 0.043684490460944636; -0.2578688762031856 0.6811275515417524 0.06979705435650777; -0.16643689458434993 0.44448647933073615 0.03748178826678883; 0.03135747943986613 0.09121026982102139 -0.011021906895529003; 0.2773784563100772 0.21421663651317946 -0.0939720012037749; -0.026321949219467622 -0.002583681933706951 0.0022197546795018445; 0.20252009126605577 0.5859029556414175 -0.10288257122681152; -0.5835246166241774 0.9904709316092567 0.042044833954454276; -0.7362038421319124 -0.20746802611665538 0.26205247161144074; 0.025644898980856885 0.13288887758204784 0.067531572098157; -0.1567362766945195 0.020710809244175152 -0.029197896508943184; -0.35499348849403123 0.09675115246414323 0.0008648920068945578; 0.08552766541451494 0.35786531030916835 -0.019970820204502436; 0.07564615169332112 -0.16796111456618562 -0.022460352690263453; 0.25493279832576426 0.09735303708739874 0.0929229928187175] % + +Mass Used: 3003.684776260021 kg +Launch C3: 38.70647817922525 km²/s² +||V∞_in||: 10.348381854523241 km/s + + + +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-11-16T09:01:46.766 +Launch V∞: [-1.2358227541627522, 0.323049558821953, 2.495135844447432] km/s +Phase 1: + Planet: Mars + V∞_in: [-5.492217326783208, -0.7599139192265875, -0.7445133837270346] km/s + V∞_out: [-4.404936994877108, -3.4463054890902294, 0.12597397946441688] km/s + time of flight: 1.1637720070766585e8 seconds + arrival date: 2027-07-25T08:01:46.766 + thrust profile: [0.01055136636996065 0.5035473835223019 0.2144643592551079; -0.04595477215059715 0.6852423614947899 0.16820399057019442; -0.5895802429453626 0.7197253917092584 0.15157285154237687; -0.7242691347954416 0.6365969821781644 0.18351832934110204; -0.7254557218972608 0.33325583626785743 0.20650030599325478; -0.624534757383007 -0.46380253719846265 0.19914261964212518; 0.06888536686167775 -0.3659727992321626 -0.05660421386154573; 0.41960359345145115 0.5802522947366238 -0.02564875636361316; -0.43557904354293114 0.6848106459808407 0.15045741326417394; -0.5906326245605844 0.626327253137284 0.1907051751516841; -0.6145984992977067 0.6853285910994333 0.24790988830917382; -0.7852172198133732 0.397363217233713 0.22913677229660695; -0.6148113166692493 -0.6180162700085184 -0.1063370011071445; -0.3438743055901661 0.08561279547696703 0.1133320954927072; 0.24423988113626285 0.4984911769229264 0.26361771766972686; 0.6070536708822735 0.7233947175576885 0.2890649522953669; -0.39805774605395056 0.8544543105302159 0.2032769540887175; -0.877234342411992 0.5568182222065088 0.1181949174776601; -0.7848468400087453 -0.7818849886318364 -0.025654657156075657; 0.39491632368805846 -0.7677648336006526 -0.018827493121373502] % +Phase 2: + Planet: Jupiter + V∞_in: [-2.011375822763062, -4.005960504046318, 0.6209700805836994] km/s + V∞_out: [-4.246987681230396, 0.16498798356943736, 1.5540119004205253] km/s + time of flight: 1.4691600181840378e8 seconds + arrival date: 2032-03-20T18:01:47.766 + thrust profile: [0.681909870255602 -0.5761969653838755 -0.02754846539663112; 0.7118573450786314 0.31247951434638493 0.043677226876746314; 0.5476987320075556 0.6581866365943503 -0.003833400581880826; 0.10725439389134384 0.7294932911664623 -0.034290527364056536; -0.5427655230030919 0.7281280491625349 -0.0299219686998862; -0.7331645357201648 0.661529122002647 -0.022598124369638494; -0.7921492428190279 0.3933778983017051 -0.021082156107776216; -0.7932731599235451 -0.41313404927011227 -0.019757316586946027; -0.7424285866522327 -0.6896359802485261 -0.021540954373280186; -0.6106751913915949 -0.7225982342788454 -0.020163701822483136; -0.37316409906634423 -0.7007771556440968 -0.011208908465949893; -0.1711206238316838 -0.6415857635215466 0.0059500126042923785; -0.08270331405821842 -0.5687506908923067 0.02659262994655598; -0.049372522261264505 -0.49783910816632987 0.048628191706214005; -0.04372663474025917 -0.41699938093001865 0.07363018971956578; -0.05490501770449129 -0.31189423172940106 0.0949294276017952; -0.09260972837599633 -0.2199470543952063 0.05957362145438097; -0.0634254159444419 -0.17400774633467572 0.16341908215231168; -0.05232699030024355 0.08812711882068765 0.1012502462026133; -0.04359653224713776 0.2114603900012656 0.04944539701697088] % +Phase 3: + Planet: Saturn + V∞_in: [-7.936261563870153, 0.192812008719828, 0.7850203435347649] km/s + V∞_out: [0.08172234404293398, -0.35122508987936396, 0.006338068922481654] km/s + time of flight: 2.9010960004261374e8 seconds + arrival date: 2041-05-30T12:01:47.766 + thrust profile: [-0.1762427833398218 0.018451914856523026 -0.33296833868061293; -0.10855107710674605 0.044463310211183146 -0.33965829997250213; -0.04955955263781527 0.10666486336804054 -0.3343168817737069; -0.14933152742910255 0.1645563456813175 -0.2888802750452695; -0.011372547689235173 -0.39964858425741717 0.1289083844812905; 0.17913823101853307 0.33922366300742973 0.3624022918784145; -0.056147608885838356 0.40536943517001855 0.2345805092442894; -0.11646645449972745 0.37970664664911913 0.13215537014712256; -0.10774775336158972 0.3637144687183163 0.07982907905717164; -0.03689877185389765 0.36730516793108037 0.04229495484147119; 0.08041474785484633 0.3975271403801768 0.011450007794323156; 0.2209067582381832 0.4645747308847809 -0.016359218295681436; 0.29077903309671577 0.5746646081920227 -0.03785392741655643; -0.5440697079277356 0.7004154769551414 -0.02197571950265878; -0.5081898184366466 0.06445088273594297 0.0502311733117999; -0.19802320496526152 -0.07027856584170135 0.014625860167883831; -0.07715652979513347 -0.015846719041313496 0.0076264391612288025; 0.180938962168102 -0.0850580439905663 -0.026509928911235665; 0.28645290190644923 -0.11681132361576753 -0.037935422919142044; 0.4089515815441177 -0.14951729956288723 -0.05914131349793209] % + +Mass Used: 2473.604423137509 kg +Launch C3: 7.857321779407867 km²/s² +||V∞_in||: 7.977322923176217 km/s + + + +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-07-22T06:44:51.639 +Launch V∞: [2.575248384952663, 2.739716813210934, -0.38893905027836745] km/s +Phase 1: + Planet: Mars + V∞_in: [4.32111461530485, 2.7960291205842593, -0.489556914131019] km/s + V∞_out: [1.7907908980924474, 4.820115223157361, -0.5379099033537726] km/s + time of flight: 6.124238397428751e7 seconds + arrival date: 2026-07-01T02:31:14.639 + thrust profile: [0.02204617368488705 0.06285779065282272 0.012605171575819224; -0.011433803484298078 0.08848061166582002 0.07202092139015609; -0.07959321828350713 0.11796051271483557 0.10864894932433573; -0.16842886185138436 0.10168512037796995 0.12068506836380218; -0.23809792134546726 0.03408694703096996 0.10782537552663919; -0.2712846099916887 -0.05259050616229293 0.07714680434548718; -0.2691701026056171 -0.13114175093946576 0.03494697732427611; -0.2432473375546796 -0.19827411241093662 -0.012549713355480184; -0.19688682555894857 -0.25454624209774884 -0.060002522712937; -0.13420719992703317 -0.31198661132994665 -0.10268341121799718; -0.01782601669889528 -0.3411050774098038 -0.13846230630135042; 0.17407803978077827 -0.3653166442745793 -0.1617162480750069; 0.39405333004023496 -0.35863769585862276 -0.16764222379359453; 0.5881727003228676 -0.2918230276130316 -0.1538361990366852; 0.7349673257433222 -0.12576056403661834 -0.12169301624150872; 0.8068721878811431 0.08212623367867798 -0.06681093685570723; 0.7498334641941427 0.6273302531285769 0.0041442783835015165; 0.48778675631358515 0.768425653968566 0.07684034445879483; 0.03235026516840393 0.7961138086551178 0.1340769950940127; -0.187175909543306 0.725754663622694 0.16344645357600582] % +Phase 2: + Planet: Jupiter + V∞_in: [-2.776889048582584, 0.577121588676522, 0.007961135089457616] km/s + V∞_out: [0.7615534564462777, 2.718708568232091, 0.27004925013867337] km/s + time of flight: 1.1292109290692344e8 seconds + arrival date: 2030-01-28T01:29:26.639 + thrust profile: [-0.840176369612668 0.976860342718164 0.058196195949256124; -0.8628465472635846 0.7633342124306659 0.1067403299239058; -0.8382024712014463 0.2581297893476549 0.12338258921323142; -0.8025794731065865 -0.1952513411331264 0.12149932865338556; -0.7572209152982607 -0.32000638227817424 0.10891070865997188; -0.7036267077800332 -0.3720841081186767 0.09043232925350977; -0.6463345866299025 -0.4293290426371054 0.06661829901893401; -0.5816014177883754 -0.44981649190131995 0.05067422918383243; -0.47351459443415633 -0.43975356881090427 0.028888383104343048; -0.4446429769285578 -0.4496298163012175 0.016442900362289542; -0.3753382613887226 -0.44043470262281187 0.004400618346128699; -0.3104508002843935 -0.4100796118163795 -0.004420648978465791; -0.2535633130657495 -0.3762527335843237 -0.010222789989029061; -0.12727676625203097 -0.3385883342435648 -0.016879911592349858; -0.17160701300131967 -0.303175547483604 -0.013946042678809141; -0.14486147929059093 -0.25597770208827797 -0.012578650709578849; -0.12478337244188682 -0.2047807012949446 -0.008914893875013217; -0.10754382990114088 -0.15281428358709293 -0.0036295313604368246; -0.08430003348112626 -0.09766774422527713 0.003387978072041825; -0.049542730705205464 -0.025733639517012987 0.003344362241873508] % +Phase 3: + Planet: Saturn + V∞_in: [-1.4245259099537633, 1.4291602238263075, 0.11854473850651923] km/s + V∞_out: [-0.6879338015175315, -1.3876319593718838, 0.8808502953774751] km/s + time of flight: 3.408146015783399e8 seconds + arrival date: 2040-11-15T16:12:47.639 + thrust profile: [0.0209250957876161 0.07236548568951691 -0.05441358281175795; 0.04271088201266738 0.059837108824994496 -0.04570267674006564; 0.06660112060615696 0.05195757710585663 -0.03370174018627228; 0.07859207469254972 0.05915284312855131 -0.01995033274559411; 0.05470694198510173 0.07831313755730426 -0.010342114841936848; -0.01348106574647589 0.11277794394272658 -0.0034013433219311725; -0.09145707370229726 0.10312222608201255 0.005576461043330823; -0.12850299192302284 0.05752290823836534 0.01577381261339529; -0.13477884086307976 0.013206245882351258 0.018396651241394796; -0.12124443428533518 -0.016003517409004134 0.02309161441900346; -0.10385877836751767 -0.034262782555751645 0.026881849627747586; -0.08713710038230636 -0.04462790000575737 0.02664100559569609; -0.071851222306589 -0.051275998799280825 0.02033038048400631; -0.05351516590047124 -0.05503941535681956 0.024892443243640875; -0.042179454832756653 -0.05447471988772444 0.02020467463443017; -0.03024017392297153 -0.05390626764438977 0.014150662481409669; -0.01972175537440891 -0.05302868663746655 0.005230379873849089; -0.012681981493559499 -0.05225628051430802 -0.0024339834268425693; -0.0044941899601042504 -0.05698931635146416 -0.007176158051852003; 0.009984513981692316 -0.06168319332065979 -0.016333699861465947] % + +Mass Used: 1015.034880811023 kg +Launch C3: 14.289226045623414 km²/s² +||V∞_in||: 2.021342590587859 km/s + + + +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-12-14T15:10:10.657 +Launch V∞: [-5.324790803109733, -2.6773113758857146, 0.3590879071328112] km/s +Phase 1: + Planet: Mars + V∞_in: [-7.8280744026110485, -4.482906734167364, -0.5270128091140733] km/s + V∞_out: [-8.714629007362692, -2.3006682785347587, -0.6459280917863456] km/s + time of flight: 1.4074379597755253e8 seconds + arrival date: 2028-05-30T14:40:05.657 + thrust profile: [-0.09620569960732477 -0.09890174838841997 -0.006304928381722739; 0.01019673300605273 -0.15089658441406675 -0.0021554349727457207; 0.07822408798843489 -0.11071926046790218 0.004988054677396156; 0.09762767912264393 -0.058415019885606094 0.010174486469221193; 0.09596476555630318 -0.005224025746863998 0.004950216517465728; 0.08806191952377797 0.049822770611354 -0.0010597096470122361; 0.052574331589681 0.12454094146924233 0.015095231992096524; -0.04001716917664013 0.21428169922925022 0.018454940281947503; -0.19982535032247195 0.251124726671319 0.015258419491383634; -0.42902456010053436 0.03773585135440942 0.01861953896594965; -0.2620621821264161 -0.3783347111418361 0.004523163861194378; 0.05160537420225073 -0.3786420625260984 -0.011042008482375406; 0.20360488108938318 -0.27582667506971054 -0.012821162414732887; 0.2561047977346709 -0.14853261531425635 -0.005634983638021486; 0.260486703242627 -0.01792491318881055 0.0011583161900218508; 0.23894329094312064 0.10878274252152975 0.0042064519174942515; 0.19707710072889273 0.2344075946499166 0.011104691405835861; 0.13172705128797849 0.35645392804648396 0.01747201373387731; -0.03343397706399435 0.37057486224934993 0.01628713138328902; -0.3349092116148668 0.40830706963065616 0.015783429576975126] % +Phase 2: + Planet: Jupiter + V∞_in: [-5.164409827607087, -2.4015213190761244, 0.3886272138412419] km/s + V∞_out: [-0.10084295997962195, 5.705933697922466, -0.1469580047293293] km/s + time of flight: 8.148046230775028e7 seconds + arrival date: 2030-12-29T16:07:47.657 + thrust profile: [-0.4843312801347405 0.17832592220013307 0.006256115010001196; -0.5117377393427821 -0.03515133875253644 0.01594069776607602; -0.4802829543105851 -0.22759690897497922 0.023218676108680135; -0.41688069406794315 -0.3255769239533844 0.02846987059703982; -0.3518609568473908 -0.3513841428236102 0.03707709560472825; -0.28197549119514226 -0.35416420109695057 0.04330975091368633; -0.22056035580872335 -0.34012444589770013 0.048672605940703245; -0.17030162641170815 -0.3176042986233552 0.054624244098160656; -0.12962198776772624 -0.29003617152610467 0.0600491991040185; -0.09552548126143237 -0.25742381683081617 0.06663476650221734; -0.06576162258943327 -0.22042535210328865 0.07376790136845905; -0.03794666493372705 -0.18080040001875886 0.07922467457462902; -0.017587190801326653 -0.144409275958737 0.07885131961718507; -0.0005846137879528368 -0.11383597257615993 0.06598144523941014; 0.012437749223779474 -0.08192500429520043 0.050363659542438856; 0.025006348976223614 -0.05271986038900855 0.03688810130605497; 0.03735035082457269 -0.023245071824888237 0.025225516789865676; 0.048771155783688964 0.00930403641764618 0.015175514053442753; 0.056121259671254586 0.03626182021235461 0.007719603871138727; 0.06549848774435021 0.06199167605994548 0.0029712452019925654] % +Phase 3: + Planet: Saturn + V∞_in: [-2.4750372046001954, 4.13041506892929, -0.09291157556920056] km/s + V∞_out: [-0.9590001742156767, 0.00014166531615410308, -0.00017399656356734708] km/s + time of flight: 2.204227460822756e8 seconds + arrival date: 2037-12-23T20:40:13.657 + thrust profile: [0.1749523615814178 0.02337696203170268 -0.007290082696294586; 0.17710130749974723 0.04583257449906523 -0.00719233870000948; 0.174350248316964 0.07510311268410168 -0.00750473770426303; 0.16444589553075314 0.10998364297019214 -0.007106342278531456; 0.1384257291897476 0.1488418684122407 -0.006173412802780041; 0.08428653747267639 0.1721787470978516 -0.003985402948896598; 0.019687460364805707 0.15515729051991808 -0.0013753294272070818; -0.021656527704037976 0.12042770713394904 0.0001864640450765926; -0.039588280724834786 0.09367324460087394 0.0010034140790897994; -0.04673002735050872 0.07208768567973076 0.0013797248342607789; -0.04399767552371756 0.05335024899625606 0.0015132659877072718; -0.04235029705061875 0.03689185722542479 0.001509047848856101; -0.037623976049185055 0.022006890975873494 0.0010667085694236217; -0.031346917825053985 0.00585591622491494 0.00023425066193087632; -0.0193407989640302 -0.012237196189479828 -0.0032635963200177364; -0.011688504812844338 0.004985875856387392 -0.0034950987669932717; -0.013753919383294908 -0.020294143888963282 0.0018680092927586343; -0.0042296107469379065 -0.03029078043837534 0.002437090971995948; 0.010887719248873684 -0.04459982317696947 0.003041721188427454; 0.02500057674047783 -0.052736469222675816 0.0029604218341606117] % + +Mass Used: 662.0977457761205 kg +Launch C3: 35.650337425378076 km²/s² +||V∞_in||: 4.816094929158691 km/s + + + +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-11-08T18:47:22.305 +Launch V∞: [-4.451427517503081, 4.380713257243984, 0.9509666906856978] km/s +Phase 1: + Planet: Mars + V∞_in: [-7.503625705871378, 2.9922534516224317, 0.3970744313528344] km/s + V∞_out: [-6.203985495450952, 5.1853077278089845, 0.19685948210225732] km/s + time of flight: 7.692258675246356e7 seconds + arrival date: 2026-04-17T02:10:28.305 + thrust profile: [-0.05747333201815444 0.01458857211306159 0.01661972438571343; -0.07640520733942768 -0.0880498378588422 0.009291396823580423; -0.0642351947881695 -0.14583843433809482 -0.01174256444385774; -0.03591836428259514 -0.19097919421877213 -0.030455634296288725; 0.0014696729268849598 -0.21419745388390338 -0.046332000137257384; 0.043321837437152184 -0.23281386608467833 -0.057269006919827066; 0.08487576000339314 -0.23180733654869165 -0.06400789992534636; 0.12836076596832638 -0.2345880635860211 -0.06663468113711396; 0.16914897842720558 -0.2202670166100522 -0.06608715415000553; 0.20331848204335912 -0.19904198276368773 -0.06263191481516477; 0.23625994800571543 -0.18017227778817843 -0.057302223507679384; 0.26476916718248283 -0.15037417766839517 -0.05026099494873699; 0.28150073209231896 -0.11974625587737671 -0.04226763198923683; 0.2911151952723726 -0.08935809631597122 -0.032922957893997004; 0.29662192049119385 -0.05630987736862665 -0.023018382921682446; 0.3163317621362404 -0.01253021176722935 -0.013235490847343547; 0.25582892879782015 0.03994726547045516 -0.0012262871620623078; 0.20630604157449897 0.09278869993819255 0.011047803244751797; 0.13239326442164706 0.18510472327622382 0.022309378373958296; 0.0678407381537921 0.24416553319280734 0.027187329287448894] % +Phase 2: + Planet: Jupiter + V∞_in: [-2.4066983016171593, 3.60782547580802, -0.0729666504902062] km/s + V∞_out: [2.378938038105792, 3.622859356538288, -0.17162450321036135] km/s + time of flight: 1.0365627669349712e8 seconds + arrival date: 2029-07-29T19:35:04.305 + thrust profile: [-0.08661540144522925 0.5452498417652726 0.01940681405322532; -0.3026836754787113 0.3296518390803253 0.005983402538334351; -0.3406876005629003 0.11833095428025397 0.003356530625833691; -0.2835305485605863 0.05826412825528092 0.02255167620704516; -0.2312925636505238 0.037264277244941184 0.05388961098566991; -0.18711959340793846 0.02248626525242582 0.07873824296078222; -0.1586634246283703 0.009933258699574466 0.0871013968397894; -0.13480225405151802 -0.0016459373751799647 0.08376814481354339; -0.11717491300808694 -0.011644771387652143 0.06591943652720958; -0.12385446642299068 -0.021486105366059834 0.04559099694744897; -0.09388047865743618 -0.028093190404018073 0.021912607207877112; -0.08329274681397837 -0.03442999409177474 0.004671009919336775; -0.074293683492257 -0.039542791582250804 -0.005853738709231158; -0.06633940754759032 -0.044531789384190786 -0.009552210711090501; -0.05819808497253237 -0.047725452096228235 -0.008621886584541672; -0.052136936558275115 -0.0524395749605876 -0.002738982045574738; -0.04346694186008132 -0.0559411143833451 0.005899905372803087; -0.019037945479989642 -0.06356156997525016 0.022900432372144015; 0.03382392128782208 -0.03750155602427737 -0.01509909397132852; 0.0372737888254289 -0.03393228709124474 -0.008856011117644847] % +Phase 3: + Planet: Saturn + V∞_in: [-1.348151617130741, 3.372644961627469, -0.15974064227398158] km/s + V∞_out: [0.5003596890905858, 0.5035022711921476, 0.4902757482488732] km/s + time of flight: 2.6430663321089447e8 seconds + arrival date: 2037-12-13T22:05:37.305 + thrust profile: [0.09042797681998876 0.08185621600988492 -0.005657240382538273; 0.08801730768503421 0.06654785786786777 -0.005370519173262853; 0.08823193892876004 0.06301303625131692 -0.005301669247083464; 0.09786240449059495 0.0767776838916466 -0.005515040644430515; 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-0.03952915140222731 -0.007355989451236212] % + +Mass Used: 537.3508733080857 kg +Launch C3: 39.91019323257055 km²/s² +||V∞_in||: 3.6356242782715444 km/s + + + diff --git a/archive/EMJ_2021-10-17T21:08:51.754/mission b/archive/EMJ_2021-10-17T21:08:51.754/mission new file mode 100644 index 0000000..f1d69a9 --- /dev/null +++ b/archive/EMJ_2021-10-17T21:08:51.754/mission @@ -0,0 +1,29 @@ +archive/EMJ_2021-10-17T21:08:51.754/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 2024-07-06T16:53:06.420 +Launch V∞: [2.823260136727537, 2.381108515747835, -1.1737954184426584] km/s +Phase 1: + Planet: Mars + V∞_in: [2.902861479885485, -0.1301588187286526, 0.5669523646795902] km/s + V∞_out: [1.2390632915772526, -2.6409219673539095, 0.5046925355113366] km/s + time of flight: 8.406297685905933e7 seconds + arrival date: 2027-03-06T15:42:42.420 + 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b/archive/EMJ_2021-10-17T22:10:45.653/mission @@ -0,0 +1,29 @@ +archive/EMJ_2021-10-17T22:10:45.653/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 2024-07-11T15:07:13.403 +Launch V∞: [2.955015332011587, 1.7458476003678773, -1.6442790339059827] km/s +Phase 1: + Planet: Mars + V∞_in: [2.777431397042264, -0.6171132169349891, 0.8159382942604554] km/s + V∞_out: [0.41916073556198946, -2.93012238170956, -0.008635342159592475] km/s + time of flight: 8.130510845924018e7 seconds + arrival date: 2027-02-07T15:52:21.403 + thrust profile: [0.03560871457580073 0.04297807153526013 -0.009741278672567194; 0.010244973922489548 0.0682865729467034 -0.00015039076694469604; -0.01693971645455401 0.07449636960644072 0.004194668780588966; -0.041463139657556526 0.07132437969889172 0.00820671382930803; -0.07040811753124122 0.06106352197572917 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+/home/connor/projects/thesis/archive/EMJ_2021-11-07T15:15:24.057/mission--------------------------- + +Spacecraft: bepi + dry_mass: 2000.0 kg + specific impulse: 2800.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 0.9 +Launch Mass: 4000.0 kg +Launch Date: 2023-01-23T13:44:20.247 +Launch V∞: [-0.1739597247433209, -1.5392251924256757, 0.1510741902051145] km/s +Phase 1: + Planet: Mars + V∞_in: [-1.747388916324353, -2.061505608833443, 0.004246536679567164] km/s + V∞_out: [-2.4403954507440164, -1.1573303397285044, 0.09102116739890352] km/s + time of flight: 1.0791720765728353e8 seconds + arrival date: 2026-06-25T14:44:27.247 + thrust profile: [-0.003437324500446065 -0.06316993477714959 -0.03227448158061817; 0.01567838811254846 -0.026330238009065726 -0.042075545977590216; 0.05142670882061399 0.03192109164526059 -0.030663473328706496; 0.18494150891704356 -0.05996396933783311 0.07272546357288993; 0.01987844881950037 -0.08012428438452728 0.14827651870110511; 0.0478009970849944 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0.07151821136919514] km/s + V∞_out: [-0.032527135720069, 0.001544851923976201, -0.00019858586424769518] km/s + time of flight: 1.3383000099773991e8 seconds + arrival date: 2030-09-21T13:44:27.247 + thrust profile: [-0.1392065495307979 0.004750835268938231 0.023507505308300022; -0.19310508213400865 -0.033187172798787246 0.03720253217974291; -0.08401649310562243 -0.03721535067081677 0.018686610849057983; -0.07189175926991606 -0.010086246689719958 0.002137809069141927; -0.04577388220162917 0.041578634569519 -0.018853960583673845; -0.1661362264023361 0.06506520619848838 -0.009449430204867661; -0.19796870421884868 0.04783193521476848 -0.023213922479647067; -0.12983109381999572 0.047003643397231905 -0.03086558152561419; -0.0882948553314463 0.1475664155854163 -0.017260515869025956; -0.3366163399243817 0.39553588365930525 0.015795560486203543; -0.640980062057629 0.2632981931405252 0.0812643122284222; -0.6170331837293128 -0.3303891659922319 0.08145169051162247; -0.417277476379212 -0.4064979390965165 0.057948112978786846; -0.1920015280971652 -0.28614848876207744 0.021902037419699424; -0.04488825027754133 -0.07688374836411227 -0.0050070954905793545; -0.020349917091670125 -0.03323033529641674 -0.02767377795875804; 0.0034924766822311388 -0.014218666042869754 0.006356643814839159; 0.00039701408140195273 -0.023899377007047005 0.09028397293070597; 0.052254845117264026 0.028631960813363038 0.004727246748924411; 0.03093967952976618 0.02034528891395188 -0.008818558262886378] % + +Mass Used: 1779.3184287128902 kg +Launch C3: 2.422299589776762 km²/s² +||V∞_in||: 8.259134663277639 km/s diff --git a/archive/EMJ_2021-11-07T15:15:24.057/plot.html b/archive/EMJ_2021-11-07T15:15:24.057/plot.html new file mode 100644 index 0000000..36190a0 --- /dev/null +++ b/archive/EMJ_2021-11-07T15:15:24.057/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMJ_2021-11-07T16:44:24.602/mission b/archive/EMJ_2021-11-07T16:44:24.602/mission new file mode 100644 index 0000000..ad6d167 --- /dev/null +++ b/archive/EMJ_2021-11-07T16:44:24.602/mission @@ -0,0 +1,29 @@ +/home/connor/projects/thesis/archive/EMJ_2021-11-07T16:44:24.602/mission--------------------------- + +Spacecraft: bepi + dry_mass: 2000.0 kg + specific impulse: 2800.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 0.9 +Launch Mass: 4000.0 kg +Launch Date: 2027-07-20T13:17:34.631 +Launch V∞: [-2.3530089890058954, 1.806546373465246, -0.8246183971035168] km/s +Phase 1: + Planet: Mars + V∞_in: [-3.557079179490031, 2.2348168420384456, 1.4054671292663363] km/s + V∞_out: [-4.074087303045588, -1.0849670349142753, 1.3593729379381074] km/s + time of flight: 1.0695600026560412e8 seconds + arrival date: 2030-12-09T11:17:34.631 + thrust profile: [-0.0022189023782523748 0.023365002143236557 -0.010993409331132617; 0.2153019288203301 -0.16440845543934793 0.012979033551565024; 0.3639464079118591 0.18422132432552532 0.04272023217963688; 0.11466184077416293 0.3079055688420129 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0.10307557908026614] % +Phase 2: + Planet: Jupiter + V∞_in: [0.38917010093640664, -4.172653280725571, -0.38172849726338637] km/s + V∞_out: [-0.19079117316696953, -0.697272265566823, -3.556895184028567] km/s + time of flight: 9.204480003834815e7 seconds + arrival date: 2033-11-08T19:17:34.631 + thrust profile: [-0.28696988915862254 -0.5466775279353076 0.0161784825048141; -0.05201138624094085 -0.5103548545163037 0.022399691416144073; 0.09258223397854948 -0.42700369632306956 0.02864531312701303; 0.1544195747765251 -0.3175042943871396 0.03319962132309101; 0.16629852231537434 -0.20372710365454566 0.033385847516108444; 0.14766618426707362 -0.10862149045095645 0.026893053884926972; 0.10680433249395786 -0.047590669692367006 0.013917994143247845; 0.05372607652222386 -0.024738666039118885 0.004540404069389168; 0.0454652164291245 -0.03203318353562152 0.003800593821863827; 0.06019445610850742 -0.07020561382583693 -0.0007266034614935319; 0.031747954241254955 -0.05399780408669305 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a/archive/EMMJS b/archive/EMMJS new file mode 100644 index 0000000..1082585 --- /dev/null +++ b/archive/EMMJS @@ -0,0 +1,43 @@ +archive/EMMJS--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-11-08T16:33:41.148 +Launch V∞: [-3.7467429728623447, -0.7427414062360022, 1.0452490382459865] km/s +Phase 1: + Planet: Mars + V∞_in: [-2.885104439331886, -1.327495046167686, -0.027749058108596784] km/s + V∞_out: [-1.635967097498029, -2.7221789573242074, 0.015131202359034032] km/s + time of flight: 6.778595425260136e7 seconds + arrival date: 2026-01-01T05:59:35.148 + thrust profile: [-0.05074044407568138 -0.021150582055882192 0.02730812822478398; -0.05363696950139044 -0.06016484582924907 0.04378542458137859; -0.02771035674834004 -0.10645426057233084 0.04017412625773127; 0.01630657360103497 -0.12411195034078264 0.023350505322999197; 0.05888817282501315 -0.10894637011686983 0.0004869417342207616; 0.08706942097452976 -0.07439720218837492 -0.023367157675286705; 0.09495132401480658 -0.035316011414834675 -0.04390702621881143; 0.08752285351021441 -0.004210304140208955 -0.05824943912322043; 0.06832834450779833 0.01653042551161497 -0.06490194085584605; 0.04924860864138059 0.022800133521631457 -0.062427366917489194; 0.03691868046224741 0.011541999666891671 -0.049506900069146154; 0.02451718791619906 0.019175805931995835 -0.026347851368135194; -0.032064249204675696 0.028639492606652335 0.024093899166278167; -0.08306772663523894 -0.03165903417995458 0.04031997576998134; -0.09308798794042389 -0.09539353910087413 0.04749994325844049; -0.02511528438762353 -0.14606890192307997 0.03354911283916682; 0.04310668443858089 -0.14207536740537 0.010418445496805094; 0.09246132545360927 -0.10807413652564378 -0.01547233992587798; 0.11319881808511016 -0.06123358244390861 -0.03864051024951101; 0.11067805251913554 -0.018856574108340608 -0.05612659024233843] % +Phase 2: + Planet: Mars + V∞_in: [-5.884459586892747, -3.363236848676117, -0.5090555323000778] km/s + V∞_out: [-6.754575036027653, -0.6433971508597986, -0.39980914727121014] km/s + time of flight: 7.419247222558242e7 seconds + arrival date: 2028-05-08T23:00:47.148 + thrust profile: [0.09654790671377476 -0.02421154193760562 -0.017928801450145315; -0.013697559588275829 0.2078634802144036 -0.1014668129386949; -0.1556430254864518 0.42999351341524117 -0.15436045217579106; -0.34594668129342293 0.5414366154963298 -0.18269379097659816; -0.5454038742991185 0.5440039323636802 -0.17114242041739094; -0.6681265735588777 0.3905344944333295 -0.11698706816633163; -0.7178501053667702 -0.2147414683533294 -0.03563087595180013; -0.7220121820048746 -0.6387659476154413 0.04867755848318845; -0.6341573780307701 -0.8263426625319585 0.11250663825239217; -0.42165856247956973 -0.9426406733296913 0.15700663915570923; -0.2282676099099079 -0.9148864509029049 0.18224086165253006; -0.19975433285802874 -0.7643878036213333 0.18722809378704905; -0.23887594019854455 -0.571448552171104 0.1698384408589319; -0.20476059817742176 -0.3599675936442139 0.12804247162016902; -0.021622630852921543 -0.18516594772639078 0.08091546982169469; 0.06780313268150127 -0.07159692617114882 -0.012001883119840365; 0.0737246732088521 0.19689739773217652 -0.0905687562910174; -0.07537764165798895 0.41078706656960723 -0.1422877828900227; -0.2938291349463374 0.6466716586743462 -0.17361703816996657; -0.601397213043171 0.6791254738338734 -0.16212519541868492] % +Phase 3: + Planet: Jupiter + V∞_in: [-4.520674651049057, -2.5409484551232677, 0.26037246970875744] km/s + V∞_out: [-0.8008259820354645, 5.108593255783271, -0.47079137990954545] km/s + time of flight: 8.970106359744217e7 seconds + arrival date: 2031-03-13T03:58:30.148 + thrust profile: [-0.9144771548791947 0.6902760792706399 -0.02961910274543401; -0.9666896369671112 0.2364932018447611 -0.03360017687916256; -0.9297691297960539 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0.03978470139669819 0.0415658896303641 -0.008546043818250205; 0.05975267589922902 0.07118967492032456 -0.006512156351974285] % +Phase 4: + Planet: Saturn + V∞_in: [-1.3584481648257494, 2.8741322587661022, -0.2546304125259141] km/s + V∞_out: [-0.03780230346481573, 0.0035967292583968646, 0.0007694792047629233] km/s + time of flight: 2.6826096516036582e8 seconds + arrival date: 2039-09-12T00:54:35.148 + thrust profile: [0.15488733950530229 0.004571931625674222 0.014146553973814535; 0.1553899576809856 0.03891862438324717 0.011973507362994223; 0.14041589251623252 0.07646409264944304 0.008869602158932547; 0.11548352038842227 0.1179485961935457 0.005517550148134544; 0.06394148482320672 0.14725938798843563 0.0012092021978766729; 0.0044327089101765475 0.13700916415178752 -0.005822274387507308; -0.029434414888955224 0.100612821704748 -0.017148622938312798; -0.033398085410118725 0.07353093978663178 -0.020258407230342786; -0.022858879964930717 0.05475230911401911 -0.0235821272789971; 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+ + + diff --git a/archive/EMMJS_2021-12-03T11:37:09.379/mission b/archive/EMMJS_2021-12-03T11:37:09.379/mission new file mode 100644 index 0000000..8feba19 --- /dev/null +++ b/archive/EMMJS_2021-12-03T11:37:09.379/mission @@ -0,0 +1,43 @@ +/home/connor/projects/thesis/archive/EMMJS_2021-12-03T11:37:09.379/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-02-26T04:10:12.359 +Launch V∞: [-4.841701064906604, 3.475969740428134, -4.8994214190507] km/s +Phase 1: + Planet: Mars + V∞_in: [0.02729198924983877, 5.017291114045934, -2.960466892478738] km/s + V∞_out: [-0.7796648643413417, 5.029374064409783, -2.8347788324016983] km/s + time of flight: 1.9570320002726743e8 seconds + arrival date: 2029-05-10T06:10:12.359 + thrust profile: [0.51200489277245 0.1491712750305638 -0.5617898782756465; 0.5985472817937932 0.4314745458970473 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-0.5980335383406491 -0.5746723266973839 0.15575901290142588; 0.590900565213738 0.39693261331727714 0.20472515338144043] % +Phase 2: + Planet: Mars + V∞_in: [3.0241033936172084, 1.6385004369573686, -5.605711794771172] km/s + V∞_out: [2.4283811769402535, -1.1475844477691648, -6.003401620464895] km/s + time of flight: 1.1737080029703692e8 seconds + arrival date: 2033-01-27T17:10:12.359 + thrust profile: [-0.1768137656168143 0.3393511738335891 -0.353565456723947; -0.15954083659688176 -0.5487799730055659 -0.24022806443793981; 0.5157742145013325 -0.7252600963065111 -0.4938126290082077; 0.698500596084941 0.03900690309877106 -0.23316637699244064; 0.6365913895344839 0.20777317872832707 -0.2830962364627441; 0.5861304271928349 -0.1184358449845895 -0.4564142893293172; 0.6860855423630463 -0.5456724995449903 -0.44617293698271493; 0.6670491113213445 -0.38498567211274926 -0.3230834818585812; 0.5283999818464645 -0.09570871485046831 -0.478027472175741; 0.6580560949600205 0.46722570225829474 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/dev/null +++ b/archive/EMMJS_2021-12-03T11:37:09.379/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMMJS_2021-12-03T14:06:15.707/mission b/archive/EMMJS_2021-12-03T14:06:15.707/mission new file mode 100644 index 0000000..74fc251 --- /dev/null +++ b/archive/EMMJS_2021-12-03T14:06:15.707/mission @@ -0,0 +1,43 @@ +/home/connor/projects/thesis/archive/EMMJS_2021-12-03T14:06:15.707/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-07-25T10:56:35.081 +Launch V∞: [-0.946994040198373, 0.7451481404956214, -0.8183806644150764] km/s +Phase 1: + Planet: Mars + V∞_in: [0.014258156666681189, 2.7730331960192176, -1.1269036535413253] km/s + V∞_out: [0.5141370030166348, -0.1036905077662334, -2.9466045466696906] km/s + time of flight: 1.1404800000012271e8 seconds + arrival date: 2027-03-06T10:56:35.081 + thrust profile: [0.9385530212613687 0.4901574978623852 0.10061758150690266; 0.963070949930897 0.8321550483186799 0.008076995378552753; 0.9477571571642094 0.9610236014179844 -0.3985885112414162; -0.8711740070381366 0.9585545422957218 -0.473960549642588; -0.35180875323453037 0.5538991572461103 -0.3047172625720546; 0.945857985340927 0.9318586412463802 0.07532442345652893; 0.916860585821232 0.9461601676367617 0.09256592206997157; 0.9203902037763169 0.9428723645501874 -0.3780093114569496; 0.1105180481588208 0.9388923575412604 -0.5467563429465788; 0.9600557668435807 0.08776536568096838 -0.6082094846555337; 0.9694071291822624 0.9576019390193865 0.042076881935371874; 0.7379014033007257 0.9676653528673065 0.20011181540529835; -0.7026385155061656 0.9228908375337035 -0.34668134552520397; 0.34660988424967165 0.77350231915288 -0.6692179888555208; 0.9672945056421521 -0.9455364762862372 -0.5850573257116493; 0.9859396795925156 0.16374570712498915 -0.26188762301350715; 0.9545064259275549 0.9869744571812468 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0.09302676824184232 -0.04257715628694308; -0.5866822473952952 -0.1769325756395129 0.23680697649509092; -0.14301190082784437 0.09180461385600784 -0.028924399094075886; -0.18983362654037655 -0.01602479614573261 -0.1446728759943558; 0.17123430049602928 0.2161630553091436 -0.12107554476977027; 0.0336023230656082 -0.34829018802826484 -0.06164799648134331; -0.0137744016652137 0.032090633273540385 -0.01461460357642287; 0.023301081130224558 0.023046782785575825 -0.0014039211755592525; 0.04517905715080291 0.07387132921915998 0.025233349143655093; 0.019815422280705618 -0.054453865039265595 -0.04881233646684176; 0.010800262146714945 0.40350474993323376 0.07282207796248781; 0.06922178100116284 -0.38131801494106843 -0.09824591875105594; 0.3129500615782364 -0.8033474844184223 -0.09841107223379629] % + +Mass Used: 2769.31857214896 kg +Launch C3: 2.1217903753437817 km²/s² +||V∞_in||: 6.915038096131817 km/s diff --git a/archive/EMMJS_2021-12-03T14:06:15.707/plot.html b/archive/EMMJS_2021-12-03T14:06:15.707/plot.html new file mode 100644 index 0000000..625f58b --- /dev/null +++ b/archive/EMMJS_2021-12-03T14:06:15.707/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMMJS_2021-12-03T17:38:37.546/mission b/archive/EMMJS_2021-12-03T17:38:37.546/mission new file mode 100644 index 0000000..7d91033 --- /dev/null +++ b/archive/EMMJS_2021-12-03T17:38:37.546/mission @@ -0,0 +1,43 @@ +/home/connor/projects/thesis/archive/EMMJS_2021-12-03T17:38:37.546/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-11-08T16:33:41.148 +Launch V∞: [-3.7467429728623447, -0.7427414062360022, 1.0452490382459865] km/s +Phase 1: + Planet: Mars + V∞_in: [-2.885104439331886, -1.327495046167686, -0.027749058108596784] km/s + V∞_out: [-1.635967097498029, -2.7221789573242074, 0.015131202359034032] km/s + time of flight: 6.778595425260136e7 seconds + arrival date: 2026-01-01T05:59:35.148 + thrust profile: [-0.05074044407568138 -0.021150582055882192 0.02730812822478398; -0.05363696950139044 -0.06016484582924907 0.04378542458137859; -0.02771035674834004 -0.10645426057233084 0.04017412625773127; 0.01630657360103497 -0.12411195034078264 0.023350505322999197; 0.05888817282501315 -0.10894637011686983 0.0004869417342207616; 0.08706942097452976 -0.07439720218837492 -0.023367157675286705; 0.09495132401480658 -0.035316011414834675 -0.04390702621881143; 0.08752285351021441 -0.004210304140208955 -0.05824943912322043; 0.06832834450779833 0.01653042551161497 -0.06490194085584605; 0.04924860864138059 0.022800133521631457 -0.062427366917489194; 0.03691868046224741 0.011541999666891671 -0.049506900069146154; 0.02451718791619906 0.019175805931995835 -0.026347851368135194; -0.032064249204675696 0.028639492606652335 0.024093899166278167; -0.08306772663523894 -0.03165903417995458 0.04031997576998134; -0.09308798794042389 -0.09539353910087413 0.04749994325844049; -0.02511528438762353 -0.14606890192307997 0.03354911283916682; 0.04310668443858089 -0.14207536740537 0.010418445496805094; 0.09246132545360927 -0.10807413652564378 -0.01547233992587798; 0.11319881808511016 -0.06123358244390861 -0.03864051024951101; 0.11067805251913554 -0.018856574108340608 -0.05612659024233843] % +Phase 2: + Planet: Mars + V∞_in: [-5.884459586892747, -3.363236848676117, -0.5090555323000778] km/s + V∞_out: [-6.754575036027653, -0.6433971508597986, -0.39980914727121014] km/s + time of flight: 7.419247222558242e7 seconds + arrival date: 2028-05-08T23:00:47.148 + thrust profile: [0.09654790671377476 -0.02421154193760562 -0.017928801450145315; -0.013697559588275829 0.2078634802144036 -0.1014668129386949; -0.1556430254864518 0.42999351341524117 -0.15436045217579106; -0.34594668129342293 0.5414366154963298 -0.18269379097659816; -0.5454038742991185 0.5440039323636802 -0.17114242041739094; -0.6681265735588777 0.3905344944333295 -0.11698706816633163; -0.7178501053667702 -0.2147414683533294 -0.03563087595180013; -0.7220121820048746 -0.6387659476154413 0.04867755848318845; -0.6341573780307701 -0.8263426625319585 0.11250663825239217; -0.42165856247956973 -0.9426406733296913 0.15700663915570923; -0.2282676099099079 -0.9148864509029049 0.18224086165253006; -0.19975433285802874 -0.7643878036213333 0.18722809378704905; -0.23887594019854455 -0.571448552171104 0.1698384408589319; -0.20476059817742176 -0.3599675936442139 0.12804247162016902; -0.021622630852921543 -0.18516594772639078 0.08091546982169469; 0.06780313268150127 -0.07159692617114882 -0.012001883119840365; 0.0737246732088521 0.19689739773217652 -0.0905687562910174; -0.07537764165798895 0.41078706656960723 -0.1422877828900227; -0.2938291349463374 0.6466716586743462 -0.17361703816996657; -0.601397213043171 0.6791254738338734 -0.16212519541868492] % +Phase 3: + Planet: Jupiter + V∞_in: [-4.520674651049057, -2.5409484551232677, 0.26037246970875744] km/s + V∞_out: [-0.8008259820354645, 5.108593255783271, -0.47079137990954545] km/s + time of flight: 8.970106359744217e7 seconds + arrival date: 2031-03-13T03:58:30.148 + thrust profile: [-0.9144771548791947 0.6902760792706399 -0.02961910274543401; -0.9666896369671112 0.2364932018447611 -0.03360017687916256; -0.9297691297960539 -0.38607984447798555 -0.01355789584429883; -0.8346154484217878 -0.6214014693922587 0.0166085094653681; -0.7129033965945708 -0.700963733220583 0.041959359935916686; -0.5741438889568534 -0.6419595568492229 0.05459259074755743; -0.43236122782537784 -0.6653422888597984 0.06339767277888375; -0.32424450019548473 -0.6113143615391297 0.0649952740051996; -0.2507213613172347 -0.5715625368541332 0.06495239951441104; -0.2066973617297525 -0.5173029196105642 0.059981187403511056; -0.17530451342656214 -0.46356648825594077 0.047624841826828745; -0.1477866838400433 -0.3897245825635479 0.049242714379565865; -0.12010797428356033 -0.31542712311456955 0.03834216234998446; -0.09300258495305348 -0.23794128216440627 0.032748124103639975; -0.06465067006435225 -0.16076271327460043 0.023845385656830805; -0.03888290411251017 -0.09081101903598543 0.01503347691667522; -0.012590046428086619 -0.034506030314933926 0.008899905471236012; 0.011376964842136187 0.007648534577971764 -0.00016213377538379614; 0.03978470139669819 0.0415658896303641 -0.008546043818250205; 0.05975267589922902 0.07118967492032456 -0.006512156351974285] % +Phase 4: + Planet: Saturn + V∞_in: [-1.3584481648257494, 2.8741322587661022, -0.2546304125259141] km/s + V∞_out: [-0.03780230346481573, 0.0035967292583968646, 0.0007694792047629233] km/s + time of flight: 2.6826096516036582e8 seconds + arrival date: 2039-09-12T00:54:35.148 + thrust profile: [0.15488733950530229 0.004571931625674222 0.014146553973814535; 0.1553899576809856 0.03891862438324717 0.011973507362994223; 0.14041589251623252 0.07646409264944304 0.008869602158932547; 0.11548352038842227 0.1179485961935457 0.005517550148134544; 0.06394148482320672 0.14725938798843563 0.0012092021978766729; 0.0044327089101765475 0.13700916415178752 -0.005822274387507308; -0.029434414888955224 0.100612821704748 -0.017148622938312798; -0.033398085410118725 0.07353093978663178 -0.020258407230342786; -0.022858879964930717 0.05475230911401911 -0.0235821272789971; -0.013323435304460137 0.041377292100863744 -0.02450308078568975; 0.017138449993525783 0.0028560178783815105 -0.007160323142177257; 0.001062473462116934 0.0017720804053553297 -0.03347589005736904; -0.005736640138015923 -0.01153596653687124 -0.031458002877494486; 0.0015233910519389863 -0.004860382970013982 -0.028357121836203404; 0.006148876075267932 -0.01671721636961961 2.8524011567020264e-5; -0.0025972753111940814 -0.024320445695816754 -0.02183259610480299; -0.011337447226728808 -0.029412701131799595 -0.010842354984299675; -0.008925944814787248 -0.03382785337511997 -0.002144952702459933; -0.002362954309468288 -0.03692199124600801 0.010934038390259249; 0.006643709781956786 -0.044837750975252416 0.015646911234478936] % + +Mass Used: 971.9203240703632 kg +Launch C3: 15.682293253184955 km²/s² +||V∞_in||: 3.1891776846675537 km/s diff --git a/archive/EMMJS_2021-12-03T17:38:37.546/plot.html b/archive/EMMJS_2021-12-03T17:38:37.546/plot.html new file mode 100644 index 0000000..d570150 --- /dev/null +++ b/archive/EMMJS_2021-12-03T17:38:37.546/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMMJS_archive b/archive/EMMJS_archive new file mode 100644 index 0000000..270d20c --- /dev/null +++ b/archive/EMMJS_archive @@ -0,0 +1,136 @@ +archive/EMMJS_archive +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-02-26T04:10:12.359 +Launch V∞: [-4.841701064906604, 3.475969740428134, -4.8994214190507] km/s +Phase 1: + Planet: Mars + V∞_in: [0.02729198924983877, 5.017291114045934, -2.960466892478738] km/s + V∞_out: [-0.7796648643413417, 5.029374064409783, -2.8347788324016983] km/s + time of flight: 1.9570320002726743e8 seconds + arrival date: 2029-05-10T06:10:12.359 + thrust profile: [0.51200489277245 0.1491712750305638 -0.5617898782756465; 0.5985472817937932 0.4314745458970473 -0.29088252333102027; -0.45166509877363964 0.5194585980906682 0.5146294788199312; 0.390520290781806 -0.5192326236428068 0.4429840782407487; 0.5160025656800347 0.43684584169735574 -0.4960808446595455; 0.5098504634472127 0.5199893315046626 0.4441400784392527; -0.49987113488322754 -0.47893620910952606 0.48036085120848565; 0.5368410355569405 0.5166822047764457 -0.4858670271400151; 0.44238316289905827 0.547824927494726 -0.4656337244770621; 0.21668892035180595 0.6021857778661118 -0.19651661385197258; 0.4341377302277037 -0.16678624993961083 0.5761938702855823; 0.5718885908183827 0.5536579188076003 0.33795675555520704; -0.39527664332753926 0.5814857962643089 -0.4679595952307845; -0.008428218148373924 0.5415048084721836 -0.45110046854424596; 0.33161932673220734 -0.45295582817342434 0.46836263037592774; 0.5280374896116378 0.5764518977818923 0.3342129870989262; 0.3107502688966615 0.5511548090736831 -0.5014473758638118; 0.07343276836897304 0.6646323168301356 -0.33765386861899715; -0.5980335383406491 -0.5746723266973839 0.15575901290142588; 0.590900565213738 0.39693261331727714 0.20472515338144043] % +Phase 2: + Planet: Mars + V∞_in: [3.0241033936172084, 1.6385004369573686, -5.605711794771172] km/s + V∞_out: [2.4283811769402535, -1.1475844477691648, -6.003401620464895] km/s + time of flight: 1.1737080029703692e8 seconds + arrival date: 2033-01-27T17:10:12.359 + thrust profile: [-0.1768137656168143 0.3393511738335891 -0.353565456723947; -0.15954083659688176 -0.5487799730055659 -0.24022806443793981; 0.5157742145013325 -0.7252600963065111 -0.4938126290082077; 0.698500596084941 0.03900690309877106 -0.23316637699244064; 0.6365913895344839 0.20777317872832707 -0.2830962364627441; 0.5861304271928349 -0.1184358449845895 -0.4564142893293172; 0.6860855423630463 -0.5456724995449903 -0.44617293698271493; 0.6670491113213445 -0.38498567211274926 -0.3230834818585812; 0.5283999818464645 -0.09570871485046831 -0.478027472175741; 0.6580560949600205 0.46722570225829474 -0.11535896533777851; 0.5612619202113102 -0.1931961652510376 -0.4400901944952552; 0.4590177925799 -0.6932770941014383 -0.5144556676853405; 0.7561006651195121 -0.6660301702898956 -0.558073578122206; 0.7758630959701225 -0.08472708630272804 -0.41036611726373284; 0.566096622638857 0.7122289950338151 -0.11214847640185667; -0.4306590268194921 0.4288485227605312 0.2105331105689206; -0.5085374829983493 -0.516980326040015 0.16675646570585556; -0.5812762098132924 -0.6592114464112737 -0.39525785227607435; 0.3559795650447502 -0.8283244516408661 -0.5816275654619777; 0.7220122543976706 -0.8709955103801817 -0.5752271662039113] % +Phase 3: + Planet: Jupiter + V∞_in: [5.060776761478531, -2.65457156740014, 1.2093916749224973] km/s + V∞_out: [-4.655218918764466, -2.2507227956970843, 2.7173192390054806] km/s + time of flight: 7.437600000965603e7 seconds + arrival date: 2035-06-07T13:10:12.359 + thrust profile: [0.5554028628906259 -0.8562653819570508 -0.4353192179666242; 0.6836770270628973 -0.8068634065800825 -0.40691024348661053; 0.6938434264699962 -0.7253280301253697 -0.3838170511550203; 0.645874750163326 -0.6289501430894447 -0.3499668164482744; 0.5889993418389312 -0.5421974665324047 -0.3250231983004846; 0.521131977446493 -0.4767106284566455 -0.3139270110389849; 0.44907608028844187 -0.42835191134595757 -0.30427273241100156; 0.3771619836123307 -0.38593020022499613 -0.29345181442595814; 0.30758537653438345 -0.34138417397604953 -0.2806050625679753; 0.24090511199415704 -0.2908278788914028 -0.2653604699658747; 0.17676587080788508 -0.23266346298480622 -0.24755096472050972; 0.11564885705822119 -0.16792372723278565 -0.22685867498381254; 0.07637432600785862 -0.10221693792171678 -0.20194486428807676; 0.019753903444897154 -0.058193667702053815 -0.18756658332981802; -0.044040327145306354 -0.00021057373845115093 -0.15565868544825787; -0.1020149066984689 0.047297427488451 -0.11989375229021738; -0.15572852811033114 0.08561531859322227 -0.08266441800646043; -0.20039007901031922 0.11872106917143616 -0.04576729741807346; -0.24124782668690306 0.1511930898415435 -0.009960538806793113; -0.28349017928188214 0.1924753920006318 0.02615368339855036] % +Phase 4: + Planet: Saturn + V∞_in: [-7.256385977948657, 0.7771719462797614, -0.785892915072424] km/s + V∞_out: [-5.9473393974944736e-6, -7.362203906933263e-7, 6.306068555232033e-7] km/s + time of flight: 1.4662439997163886e8 seconds + arrival date: 2040-01-29T14:10:11.359 + thrust profile: [-0.18959418256753224 0.13412715420236315 -0.043410183532822624; -0.19766571870169566 0.1372601657158578 -0.037968113030145044; -0.1971783405485536 0.129832118307628 -0.04157452597322259; -0.19192072677853972 0.11752160892327206 -0.04544882251204915; -0.18096355607909057 0.10099613325234727 -0.04845756455495175; -0.16440940142977603 0.0827695902679096 -0.0501168011338542; -0.14159683191947461 0.06939209018313232 -0.04938123378650775; -0.11494734465063888 0.05950353242028259 -0.04787565574075916; -0.08842871021960914 0.05331851047785903 -0.04243441932918664; -0.06244946835797671 0.049895056937498274 -0.03534701683264976; -0.0380028875571515 0.047256901837732644 -0.02725064975669285; -0.01886788294008128 0.04286456425792469 -0.019192970894846496; 0.0054749884299889135 0.041277048472854974 -0.010750429199969911; 0.02389959629376803 0.03888123568193434 -0.0015386535754099552; 0.0428231915186611 0.03753775483224003 0.00740487148339779; 0.06481451674589596 0.03713565978563092 0.014580239918154077; 0.09005525246175461 0.0369062161152353 0.018428292697994248; 0.1201760127678751 0.03212421201511818 0.04118543343400019; 0.15404590862831494 0.02789044310966664 0.043771491647338116; 0.18466591121075765 0.02447914444489793 0.052012952789042624] % + +Mass Used: 2528.0301016677718 kg +Launch C3: 59.52876507974255 km²/s² +||V∞_in||: 7.3400791119043935 km/s + + + +--------------------------- +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-07-25T10:56:35.081 +Launch V∞: [-0.946994040198373, 0.7451481404956214, -0.8183806644150764] km/s +Phase 1: + Planet: Mars + V∞_in: [0.014258156666681189, 2.7730331960192176, -1.1269036535413253] km/s + V∞_out: [0.5141370030166348, -0.1036905077662334, -2.9466045466696906] km/s + time of flight: 1.1404800000012271e8 seconds + arrival date: 2027-03-06T10:56:35.081 + thrust profile: [0.9385530212613687 0.4901574978623852 0.10061758150690266; 0.963070949930897 0.8321550483186799 0.008076995378552753; 0.9477571571642094 0.9610236014179844 -0.3985885112414162; -0.8711740070381366 0.9585545422957218 -0.473960549642588; -0.35180875323453037 0.5538991572461103 -0.3047172625720546; 0.945857985340927 0.9318586412463802 0.07532442345652893; 0.916860585821232 0.9461601676367617 0.09256592206997157; 0.9203902037763169 0.9428723645501874 -0.3780093114569496; 0.1105180481588208 0.9388923575412604 -0.5467563429465788; 0.9600557668435807 0.08776536568096838 -0.6082094846555337; 0.9694071291822624 0.9576019390193865 0.042076881935371874; 0.7379014033007257 0.9676653528673065 0.20011181540529835; -0.7026385155061656 0.9228908375337035 -0.34668134552520397; 0.34660988424967165 0.77350231915288 -0.6692179888555208; 0.9672945056421521 -0.9455364762862372 -0.5850573257116493; 0.9859396795925156 0.16374570712498915 -0.26188762301350715; 0.9545064259275549 0.9869744571812468 0.4480444603786351; -0.9777686070631371 0.9725195168208975 0.193691849051127; -0.9708472634149672 0.7500006701210962 -0.37076685227103995; -0.9229893981992848 -0.9773469965294133 -0.6290625133929346] % +Phase 2: + Planet: Mars + V∞_in: [-0.8165677595901083, -0.06087475377585851, 3.052309046353131] km/s + V∞_out: [-2.9671064112310424, -0.9629127612065755, 0.5071630145897023] km/s + time of flight: 2.5657200000050467e7 seconds + arrival date: 2027-12-28T09:56:35.081 + thrust profile: [-0.41833750150854715 -0.23745700390485924 0.5060156710931941; -0.39335607115842763 -0.21531365718730944 0.6214127928981721; -0.3741710013483589 -0.18178973996137726 0.7015878071805001; -0.3643811289828083 -0.1509347162037813 0.751160544358552; -0.3628330570779499 -0.11199271269023013 0.7793128986864543; -0.37235570205858287 -0.07302372672984968 0.7974839419031854; -0.3874662882006923 -0.03576203680036734 0.8098641766992978; -0.4074499881135819 -0.006584284581002934 0.8169150088581699; -0.4281109131913487 0.01182349039523377 0.8189971077067131; -0.4459261627474135 0.02257293277791146 0.8172972584690744; -0.4568773433902438 0.024804843226578856 0.8108158124505926; -0.4596411297003703 0.025045134417719155 0.7994526969817127; -0.4544566197190047 0.02267340988409504 0.7798827612879172; -0.44051961933116424 0.02370501075040903 0.7512234553177294; -0.41845307963023165 0.03005154105743171 0.708359052016344; -0.3881992767298684 0.04309990454210432 0.642522507646677; -0.34752334469565116 0.06138846846654963 0.5427837231822192; -0.2956992996903972 0.07742676936562033 0.40261391380265427; -0.17065939997376794 0.03880630671620183 0.2558269001777807; -0.235765575949598 0.13041638287567744 0.1404777210162043] % +Phase 3: + Planet: Jupiter + V∞_in: [-1.7554396063175077, -4.3095849115029985, -0.1325601348507023] km/s + V∞_out: [-4.236997629309691, -1.8724795170284283, -0.4561606000854912] km/s + time of flight: 1.4433840000004688e8 seconds + arrival date: 2032-07-24T23:56:35.081 + thrust profile: [-0.5079766273797471 -0.10849515042583255 -0.0073545543900051516; -0.8149330561784093 0.34076004302958 -0.10326028863924017; -0.9395306205116954 -0.6895587367092969 -0.1170733748155399; -0.8439334413601929 -0.9377459623599967 0.015887598730331222; 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Planet: Saturn + V∞_in: [-6.539365214334455, 2.218176712783986, -0.36626020172775725] km/s + V∞_out: [-3.665136112061718, 6.451338183645968, -0.16457889689277141] km/s + time of flight: 1.812492000000014e8 seconds + arrival date: 2038-04-22T18:56:35.081 + thrust profile: [0.05264623774997263 0.215338495237562 0.003754114844726852; 0.021165626937991143 0.22155170870739663 0.0047677855635804905; -0.0033929172288595286 0.31227924099890236 0.06539164976806457; 0.5694561518181592 0.6749368464572498 -0.11566610061632827; 0.1324891033231393 0.3597380526244606 -0.022962295545894153; 0.024627138889422973 0.3245686299565964 0.04183403216303953; 0.04019245536713721 0.744671990758876 0.03457514031015897; 0.03322017112484851 0.09302676824184232 -0.04257715628694308; -0.5866822473952952 -0.1769325756395129 0.23680697649509092; -0.14301190082784437 0.09180461385600784 -0.028924399094075886; -0.18983362654037655 -0.01602479614573261 -0.1446728759943558; 0.17123430049602928 0.2161630553091436 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-1.327495046167686, -0.027749058108596784] km/s + V∞_out: [-1.635967097498029, -2.7221789573242074, 0.015131202359034032] km/s + time of flight: 6.778595425260136e7 seconds + arrival date: 2026-01-01T05:59:35.148 + thrust profile: [-0.05074044407568138 -0.021150582055882192 0.02730812822478398; -0.05363696950139044 -0.06016484582924907 0.04378542458137859; -0.02771035674834004 -0.10645426057233084 0.04017412625773127; 0.01630657360103497 -0.12411195034078264 0.023350505322999197; 0.05888817282501315 -0.10894637011686983 0.0004869417342207616; 0.08706942097452976 -0.07439720218837492 -0.023367157675286705; 0.09495132401480658 -0.035316011414834675 -0.04390702621881143; 0.08752285351021441 -0.004210304140208955 -0.05824943912322043; 0.06832834450779833 0.01653042551161497 -0.06490194085584605; 0.04924860864138059 0.022800133521631457 -0.062427366917489194; 0.03691868046224741 0.011541999666891671 -0.049506900069146154; 0.02451718791619906 0.019175805931995835 -0.026347851368135194; 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0.6791254738338734 -0.16212519541868492] % +Phase 3: + Planet: Jupiter + V∞_in: [-4.520674651049057, -2.5409484551232677, 0.26037246970875744] km/s + V∞_out: [-0.8008259820354645, 5.108593255783271, -0.47079137990954545] km/s + time of flight: 8.970106359744217e7 seconds + arrival date: 2031-03-13T03:58:30.148 + thrust profile: [-0.9144771548791947 0.6902760792706399 -0.02961910274543401; -0.9666896369671112 0.2364932018447611 -0.03360017687916256; -0.9297691297960539 -0.38607984447798555 -0.01355789584429883; -0.8346154484217878 -0.6214014693922587 0.0166085094653681; -0.7129033965945708 -0.700963733220583 0.041959359935916686; -0.5741438889568534 -0.6419595568492229 0.05459259074755743; -0.43236122782537784 -0.6653422888597984 0.06339767277888375; -0.32424450019548473 -0.6113143615391297 0.0649952740051996; -0.2507213613172347 -0.5715625368541332 0.06495239951441104; -0.2066973617297525 -0.5173029196105642 0.059981187403511056; -0.17530451342656214 -0.46356648825594077 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-0.29698573943715145 0.17818484103244142] % +Phase 3: + Planet: Jupiter + V∞_in: [1.4924422600995255, -5.560592732188845, -0.4685665727537283] km/s + V∞_out: [0.2666192989414379, -0.035476903402614585, 0.4252672489349129] km/s + time of flight: 7.801559990038186e7 seconds + arrival date: 2033-04-26T15:53:15.571 + thrust profile: [-0.05667547933380966 -0.34967018073611944 0.002732189029373461; 0.010392070890743524 -0.38900231469874 0.012454157781016004; 0.09333137039669492 -0.3933837603455368 0.02000090481188271; 0.15503747405291288 -0.3683065023975787 0.025757684941636973; 0.18293674988995412 -0.3205125326753517 0.029768540395580415; 0.17930535445082396 -0.2591475229314961 0.0318370703301853; 0.15076970710143955 -0.19372274550885235 0.03170102566964771; 0.10458817867769576 -0.13175745133709596 0.028987564999421418; 0.04878214365636921 -0.07674432001861356 0.02291451019660362; -0.002030516198702912 -0.02688349362194637 0.011613325437291943; -0.006034286792027756 0.004438215059932985 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a/archive/EMMJ_2021-11-07T18:27:10.222/mission b/archive/EMMJ_2021-11-07T18:27:10.222/mission new file mode 100644 index 0000000..64fd973 --- /dev/null +++ b/archive/EMMJ_2021-11-07T18:27:10.222/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EMMJ_2021-11-07T18:27:10.222/mission--------------------------- + +Spacecraft: bepi + dry_mass: 2000.0 kg + specific impulse: 2800.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 0.9 +Launch Mass: 4000.0 kg +Launch Date: 2027-02-01T18:33:11.110 +Launch V∞: [-3.150497013090804, -2.3173169584138944, 0.341495631383101] km/s +Phase 1: + Planet: Mars + V∞_in: [-0.7086971873088551, -0.10655494257324054, 0.11988806590713104] km/s + V∞_out: [0.2238809651804253, -0.3118676174457644, 0.6168980985050387] km/s + time of flight: 8.953200023401788e7 seconds + arrival date: 2029-12-04T00:33:11.110 + thrust profile: [-0.12186870505136849 0.09462644883825748 -0.05810534392839175; -0.030639242847821345 -0.04245910692035197 -0.0894052455624086; 0.14113718480937812 -0.11440231644835337 -0.08324956933880284; 0.2837902510213314 -0.06260096981677356 -0.0550413035881179; 0.35855908041409906 0.04073648975482989 -0.020180975564470557; 0.3729359388901653 0.15239321939968276 0.016136485697739962; 0.3362801729367708 0.23639200487749643 0.047870876871699004; 0.26251183204522277 0.2735012454673692 0.06987761022138216; 0.17815253145241594 0.2588190065709617 0.07748014522346204; 0.11663205314604401 0.2103183053176405 0.07202476138100809; 0.11053399149833462 0.17008886355865674 0.06219240053201351; 0.16138151083151792 0.16508258430710807 0.0517839189038665; 0.21005359977761767 0.21368458752750677 0.0315693543261013; 0.19623229223435448 0.2814455053854785 0.001570447612348246; 0.12163118057275962 0.3027077944605196 -0.0304471015663471; 0.050711982127557564 0.25718214500209285 -0.05394847268359673; 0.02648153137529395 0.16832831911941415 -0.05881608102540833; 0.04710479095848209 0.08697307038303437 -0.03899890258876461; 0.07958628725681302 0.06854595922468731 -0.009001942082726883; 0.08605410384534219 0.09736430380889433 0.020673442685919103] % +Phase 2: + Planet: Mars + V∞_in: [-0.86775765928764, 0.239785321439957, -0.2793440299073699] km/s + V∞_out: [-0.728269228104112, 0.22205886592425675, -0.5557724748024003] km/s + time of flight: 1.9774800534204435e7 seconds + arrival date: 2030-07-20T21:33:11.110 + thrust profile: [-0.030570769176673163 0.011978049730521367 -0.1686311146776997; -0.03734362480961287 0.018449018456192904 -0.17005264964682357; -0.04542948419070008 0.025365372398860525 -0.16992835340263743; -0.05521690145245066 0.03285244672122282 -0.16774923049721527; -0.06706930468913055 0.04078685922552811 -0.16334874802709573; -0.08131104167653695 0.04884139923754264 -0.15672575498494773; -0.09819592248044624 0.05655952543787853 -0.1479650657154312; -0.11787873911002066 0.06337920264640957 -0.13717350608484466; -0.14034999306643528 0.06867765983804668 -0.12442413309677075; -0.16539190427907322 0.07179396518491549 -0.10977409185801229; -0.1925589065058879 0.07205624162537454 -0.09328712290120528; -0.22119886531630267 0.06885264399706031 -0.07507799161161761; -0.2505343015720731 0.061677462874266016 -0.05534950074382844; -0.2797189023307287 0.05017836496163492 -0.03436640779599943; -0.3079203344948388 0.03418116061894368 -0.012445205871944063; -0.334368663091996 0.013690266374333697 0.010060492482634029; -0.35838748770071316 -0.011093871325495122 0.03277754892305918; -0.37942569771654455 -0.039796379505630045 0.055325239511752944; -0.3970806444181828 -0.07189338316019264 0.07733706717380652; -0.4112725932874617 -0.10674559801233943 0.098568724917307] % +Phase 3: + Planet: Jupiter + V∞_in: [3.096628165859758, -5.54752603323759, 0.16307349334680107] km/s + V∞_out: [-0.10793078996383877, 0.0924800512858945, -0.022459388754450135] km/s + time of flight: 8.654760001509127e7 seconds + arrival date: 2033-04-17T14:33:11.110 + thrust profile: [-0.5212124178884477 -0.24272925296458728 0.016173224831160182; -0.48041901371361273 -0.42824969367860183 0.03503551018937675; -0.35657251411134105 -0.5210283603639988 0.03882674235576436; -0.18159148927663898 -0.5413874907790582 0.03142458257784628; -0.021760680952925514 -0.5187437230839083 0.020044129391221313; 0.08815802808124944 -0.468755585771906 0.008811701650286144; 0.14996577274874454 -0.39950153509190717 -0.0006374540546909846; 0.1756826332108901 -0.31843613205645516 -0.007389149611688129; 0.17606438164463012 -0.23381194273364414 -0.01163475824093298; 0.159181144560096 -0.15334688886711978 -0.013041705195263514; 0.13078599845765138 -0.08380131179134265 -0.011046703931163082; 0.09565122980609836 -0.03262766659535713 -0.006008779003864255; 0.06498733257355833 -0.009875081025971531 -0.0018112250669574325; 0.057070637186324664 -0.005117739296306144 -0.0016028113399474964; 0.06624558635734848 0.0072126749803919175 -0.0040159232988713255; 0.05783875168815469 0.01498693837279799 -0.003335562522287042; 0.04729181899024323 0.02021996828138974 -0.0030204665772785907; 0.057434402651546965 0.035842653333588784 -0.00310080378363583; 0.053208582397478485 0.046380716067435886 -0.0063431045982933485; 0.02806058144310276 0.03766447626177584 -0.005388583041760812] % + +Mass Used: 1879.386292887199 kg +Launch C3: 15.412208581500444 km²/s² +||V∞_in||: 6.355371275643704 km/s diff --git a/archive/EMMJ_2021-11-07T18:27:10.222/plot.html b/archive/EMMJ_2021-11-07T18:27:10.222/plot.html new file mode 100644 index 0000000..05bf8ec --- /dev/null +++ b/archive/EMMJ_2021-11-07T18:27:10.222/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMN_2021-10-15T14:10:16.844/mission b/archive/EMN_2021-10-15T14:10:16.844/mission new file mode 100644 index 0000000..3f1a6f6 --- /dev/null +++ b/archive/EMN_2021-10-15T14:10:16.844/mission @@ -0,0 +1,29 @@ +archive/EMN_2021-10-15T14:10:16.844/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 2022-06-15T03:21:18.518 +Launch V∞: [0.048117896423172386, -0.5162092686244537, 0.40407035227141913] km/s +Phase 1: + Planet: Mars + V∞_in: [-0.9344418663833501, -1.94113411605789, -1.3161154740790337] km/s + V∞_out: [-2.14211756398572, 0.9624191156710435, -0.9264823839100106] km/s + time of flight: 1.2644457083492844e8 seconds + arrival date: 2026-06-17T14:50:48.518 + thrust profile: [-0.10448028441523405 -0.1256907202270118 -0.16091866640079286; -0.19904783374877122 0.10871884567825597 -0.1306688148649953; -0.19709408994597308 -0.1674300798982282 0.005069018791283623; -0.004291263269297833 -0.399104721177389 0.09790570282026163; 0.29748596325897214 -0.19017236336276858 0.06829748140772242; 0.18208731695990318 0.19543127312804398 -0.1515167603279824; -0.147097144668956 0.26471504859691886 -0.12993685282980716; -0.3254377977798237 -0.07921471871314706 -0.013320620685086488; -0.18111215875786393 -0.3419227077323917 0.07609889998875147; 0.23174255714522965 -0.32712228294832624 0.06447883065044928; 0.6721056690892853 -0.02043336602254751 -0.010181899875232497; 0.22228391170390308 0.2855335978224687 -0.10159902960358226; -0.168431496892007 0.30418945279932713 -0.070730113166975; -0.32913534843792436 -0.00484741033042222 -0.008166308801170486; -0.26947039532575157 -0.28510731387791954 0.07359876392089902; 0.05790671500570107 -0.3802998506280197 0.0866314905921983; 0.26049733990679225 -0.28812017972418896 0.01928824704441663; 0.40015076156150897 -0.011025507485978085 -0.057150879950288155; 0.20552272464587207 0.21210558478528038 -0.108254263904822; -0.0647634110268568 0.24072563384380027 -0.05160771738920396] % +Phase 2: + Planet: Neptune + V∞_in: [2.828147217989047, 0.7175168734464545, 1.0176840385312307] km/s + V∞_out: [3.088960098692494, 0.0009651340319555146, 0.0070539549539161365] km/s + time of flight: 3.697305578398602e8 seconds + arrival date: 2038-03-05T21:46:45.518 + thrust profile: [-0.682488113771849 0.13920676013767327 0.13229199047890008; -0.3820716934910725 -0.6941984698101173 0.012657220760168286; 0.5853107150693558 -0.6317019149478917 -0.02534339780785512; 0.6740197859912153 -0.5324864753684241 -0.06972765095384162; 0.6868798169923216 -0.222502142017196 -0.0661829601036205; 0.6280074153513623 0.12208601430674178 -0.08384824254232823; 0.6143769984593854 0.19563277757575892 -0.05047133576620455; 0.5240798395183139 0.21175930544481952 -0.029002996472197947; 0.443569382057989 0.20852765023008743 -0.02019580607789296; 0.4131293690460721 0.18484645183186532 -0.043147082866315294; 0.3421032285788577 0.17265685215195495 -0.04625167892683922; 0.31496404643914705 0.09909975530478392 -0.032788142105343726; 0.25985581121428897 0.07020561472862764 -0.016911332791942423; -0.132085517447492 -0.04615718911621035 0.13481526251714143; -0.25767269995543396 -0.09890431522085448 0.08074154160499622; -0.32635582434111154 -0.1543465615608083 0.053298387650411234; -0.3800377852121974 -0.17219786514243648 0.04605792593383556; -0.45767813054385165 -0.19901912427065352 0.045668370100405344; -0.49742956858989346 -0.21654911975942986 0.04409302561596516; -0.6018269818439854 -0.2341358293674843 0.018963648582648505] % + +Mass Used: 1936.6395511020824 kg +Launch C3: 0.4320601905547333 km²/s² +||V∞_in||: 3.090133970005313 km/s diff --git a/archive/EMN_2021-10-15T14:10:16.844/plot.html b/archive/EMN_2021-10-15T14:10:16.844/plot.html new file mode 100644 index 0000000..5cdeb29 --- /dev/null +++ b/archive/EMN_2021-10-15T14:10:16.844/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMS_2021-10-18T16:59:17.315/mission b/archive/EMS_2021-10-18T16:59:17.315/mission new file mode 100644 index 0000000..0ad2481 --- /dev/null +++ b/archive/EMS_2021-10-18T16:59:17.315/mission @@ -0,0 +1,29 @@ +archive/EMS_2021-10-18T16:59:17.315/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 2023-04-28T02:09:03.278 +Launch V∞: [-0.28345133710132847, 1.0743854420236858, -0.7978154104086252] km/s +Phase 1: + Planet: Mars + V∞_in: [-3.9967794624862174, -1.796615553688495, 0.18069271269193854] km/s + V∞_out: [-1.548984364644081, -4.0995103503572965, -0.1751138267279006] km/s + time of flight: 7.294333712413637e7 seconds + arrival date: 2025-08-19T08:11:20.278 + thrust profile: [0.27129342959528535 0.3105357481410173 -0.13776198909539616; 0.2857943315505697 0.37422284577893283 -0.07741685575269751; 0.29147675327956785 0.43700523965167776 -0.03795847200581804; 0.26195889887210855 0.5028181624971211 -0.0005396605815887358; 0.15264241517349655 0.5627027239358379 0.04026796082311949; -0.21472716598613734 0.5656221884285355 0.07589844603666616; -0.44097859377494264 0.6011415225988948 0.08882761279301371; -0.5596322482349072 0.5924790276186342 0.10349315642725657; -0.6494338922092608 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-0.009051525807691481] km/s + time of flight: 1.543622855088476e8 seconds + arrival date: 2040-10-17T03:40:17.209 + thrust profile: [0.13343967665884301 -0.10506545000498568 -0.0477351077659778; 0.1302117419653648 -0.03935460102717447 -0.05153213061680276; 0.11177284747102363 -0.01257220530234715 -0.04992659428886335; 0.09652693312293067 -0.002381618439009866 -0.04765269265520941; 0.0850825371473891 0.0014317391384792745 -0.04538853860191621; 0.0764692224980894 0.002389375863760724 -0.043313336682117246; 0.06984581101704013 0.001982743995643555 -0.04109653594773106; 0.06469926152021455 0.0007704842623266529 -0.03917176815195523; 0.06065861914276538 -0.0009274805284651806 -0.03711303987104724; 0.057503566679394116 -0.003082072948930367 -0.034909201620028106; 0.0550645718937643 -0.005650610120539781 -0.03268940722476422; 0.05322150250858926 -0.008613752406916884 -0.030366444716783268; 0.0518961775636053 -0.012130900432895326 -0.027730459432375138; 0.05102478831673343 -0.01609208695110308 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0.09844081095460211 0.015736280260922626; -0.0028322518503023707 0.08407047604089865 0.03216268095410213; -0.009665030744853838 0.05418448600092389 0.054271394924132535; 0.00829991223524997 0.03671735113395197 0.07037788504936107; 0.05287971274655226 0.010024909695991463 0.04123949561959472; 0.03098994422797628 0.013396671609721751 9.284814456508857e-5; -0.002877075807447608 0.0005192110683645124 -0.004545971900385684; -0.028522171379334084 -0.019564193850904677 -0.005660284903915027] % + +Mass Used: 462.9647257745969 kg +Launch C3: 60.04270225525677 km²/s² +||V∞_in||: 6.020657137117126 km/s diff --git a/archive/EMS_2021-12-11T12:46:58.095/plot.html b/archive/EMS_2021-12-11T12:46:58.095/plot.html new file mode 100644 index 0000000..a71e3b8 --- /dev/null +++ b/archive/EMS_2021-12-11T12:46:58.095/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMS_2021-12-12T02:20:38.349/mission b/archive/EMS_2021-12-12T02:20:38.349/mission new file mode 100644 index 0000000..ae0916e --- /dev/null +++ b/archive/EMS_2021-12-12T02:20:38.349/mission @@ -0,0 +1,29 @@ +/home/connor/projects/thesis/archive/EMS_2021-12-12T02:20:38.349/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-06-27T01:02:22.769 +Launch V∞: [6.7386630924747735, 2.681719926533396, -0.33192262753473517] km/s +Phase 1: + Planet: Mars + V∞_in: [7.715602805644678, 2.5340401706785007, 0.59216879433437] km/s + V∞_out: [8.14158010025008, 0.11467559822796293, -0.05931443388440504] km/s + time of flight: 9.561374944761689e7 seconds + arrival date: 2027-07-08T16:24:51.769 + thrust profile: [0.023301022793894528 0.014506194191639996 -0.0023755438375060796; -0.0033183751580871247 0.07336782130026553 -0.010811507865922472; -0.06164727407552523 0.1056496969546475 -0.015161235314008188; -0.11620137406382157 0.10874515644970927 -0.01361354605050158; 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a/archive/EMS_2021-12-12T14:59:57.936/mission b/archive/EMS_2021-12-12T14:59:57.936/mission new file mode 100644 index 0000000..0ec75c5 --- /dev/null +++ b/archive/EMS_2021-12-12T14:59:57.936/mission @@ -0,0 +1,29 @@ +/home/connor/projects/thesis/archive/EMS_2021-12-12T14:59:57.936/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-10-25T14:05:40.189 +Launch V∞: [-2.237183685934752, -2.721647916047431, 1.299312276740919] km/s +Phase 1: + Planet: Mars + V∞_in: [-0.678207962240434, -3.5504123945109747, -1.2418379495810854] km/s + V∞_out: [2.332007819175787, -2.421453655328241, -1.8183105258695256] km/s + time of flight: 1.855655995918323e8 seconds + arrival date: 2029-09-11T08:05:39.189 + thrust profile: [0.19727184520667015 -0.3838952007487214 0.17961473110199166; 0.2077514036189871 0.5200804821813247 -0.10558577682756237; 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0.006052029723090913; -0.13685498996724776 0.07579955310252746 0.0051696709685845; -0.11590045234482386 0.03683619622380138 0.005503034114011019; -0.09714808717387836 -7.510913642337649e-5 0.005881543716786649; -0.07947906741787436 -0.03636451674166609 0.006573855151556507; -0.060762284460828354 -0.07185315172378559 0.007324504256710228; -0.040146440269578795 -0.10503734607332527 0.008063012601483146; -0.01826447390719847 -0.13480682166408572 0.008650026851941802; -0.0014999731370244022 -0.16167322260227676 0.010344109911906468; 0.019647516899938273 -0.18187401707529088 0.008884133379429506; 0.07031314483210122 -0.20333200721827405 0.010747903674476903] % + +Mass Used: 1995.6659445951054 kg +Launch C3: 14.1005706160276 km²/s² +||V∞_in||: 3.1951834373386236 km/s diff --git a/archive/EMS_2021-12-12T14:59:57.936/plot.html b/archive/EMS_2021-12-12T14:59:57.936/plot.html new file mode 100644 index 0000000..286d826 --- /dev/null +++ b/archive/EMS_2021-12-12T14:59:57.936/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EMS_2021-12-12T15:39:06.197/mission b/archive/EMS_2021-12-12T15:39:06.197/mission new file mode 100644 index 0000000..6a33614 --- /dev/null +++ b/archive/EMS_2021-12-12T15:39:06.197/mission @@ -0,0 +1,29 @@ +/home/connor/projects/thesis/archive/EMS_2021-12-12T15:39:06.197/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-04-04T08:15:42.979 +Launch V∞: [4.591627441054104, -0.9372602729162841, -1.402102560672615] km/s +Phase 1: + Planet: Mars + V∞_in: [9.367085838054193, 1.2385416703463588, -1.2664210112872778] km/s + V∞_out: [9.488354168340724, -0.7139124540608336, -0.5849794139568701] km/s + time of flight: 2.4606079841224298e8 seconds + arrival date: 2031-01-20T06:29:00.979 + thrust profile: [0.48110193115514666 0.1658344957098272 0.18875138957299367; 0.2722197721770649 0.41958962982537107 0.2031126777241352; -0.14912794861230844 0.31014754435480146 0.20231048078147726; 0.41900792223774436 0.33923945509259673 -0.3410850527690159; 0.2511755140919902 0.5014702815333173 0.0058685456880530696; -0.15486070913892752 0.2360830420399679 0.2645880501135092; 0.225939307553581 0.3555635470518182 -0.2579478714227079; 0.4692868559854733 0.36449584745921737 -0.26361975800532383; 0.17776955473214556 0.5344512134705717 0.2677028115850273; 0.29341528211428775 0.25652205797659977 -0.003223292822703167; 0.47969842043937694 0.383501318717164 0.00793282457827181; 0.0557455430628551 0.42410040402941707 0.12847485289641172; 0.42501735100730476 0.4434488658095193 0.17406200336317385; 0.2586191172669515 0.3545965771776789 0.13169086497478733; 0.3994448644962761 0.3523601532459076 0.1980455999347843; 0.2712389420869066 0.2551872658044702 0.16820587889445787; 0.7160832227791448 0.05007832921773097 0.03084211842871704; -0.4014048218424198 0.4263176448200758 0.02349504793730896; -0.4648045356639775 -0.012165497397007176 0.07112680698673901; 0.3334382990840683 -0.6819542566923011 -0.05838594675754101] % +Phase 2: + Planet: Saturn + V∞_in: [-3.033179205299309, 8.323540792555027, -0.834135394854228] km/s + V∞_out: [-1.7989044724374927, 4.992471036908333, 2.7395017565836506] km/s + time of flight: 1.343904325951288e8 seconds + arrival date: 2035-04-24T17:09:32.979 + thrust profile: [0.7399454327526205 -0.5303156843529576 -0.01303320908827589; 0.8546930606858686 0.056047121557869325 0.01672326772293818; 0.8757001417012732 0.8092300745166227 0.08014191465251598; 0.7798406512457665 0.8508819508472818 0.0649883040365693; -0.03926761644682386 0.8522354272278931 0.027089526497775643; -0.434264020033893 0.8459075469832358 -0.0040464336106154335; -0.5548067523933243 0.8328498997908219 -0.030544100084358417; -0.5947401029696081 0.8138198308943535 -0.049034191658682065; -0.6075585777480846 0.7820903525414267 -0.062173373203187395; -0.6029505069844785 0.7335072879202299 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+ + + diff --git a/archive/EMS_2021-12-12T16:01:04.514/mission b/archive/EMS_2021-12-12T16:01:04.514/mission new file mode 100644 index 0000000..89cc076 --- /dev/null +++ b/archive/EMS_2021-12-12T16:01:04.514/mission @@ -0,0 +1,29 @@ +/home/connor/projects/thesis/archive/EMS_2021-12-12T16:01:04.514/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-07-08T05:11:21.442 +Launch V∞: [7.608076212455678, 2.807333338029972, -0.7296465923907695] km/s +Phase 1: + Planet: Mars + V∞_in: [8.010347423561068, 3.2469372890009143, 0.9052053694493565] km/s + V∞_out: [8.595491836222386, 0.9305961590076297, 0.8829460767922697] km/s + time of flight: 1.285682951483629e8 seconds + arrival date: 2027-08-04T06:36:16.442 + thrust profile: [0.07414876190498018 0.061418074622027974 -0.012644930305191268; 0.005288427050926843 0.06622341067027271 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0.03968790735981553 -0.17103970596354526 0.01802812299096526; 0.09266705743272931 -0.1535778429859241 0.025140107388620526; 0.20165971230655427 -0.14421264141271573 0.040991785807895254] % +Phase 2: + Planet: Saturn + V∞_in: [5.172452466285559, 3.681404565790302, -0.7376128757432779] km/s + V∞_out: [1.0471838805707034, -0.9458496802640074, -1.0540623554828816] km/s + time of flight: 1.3794018891807556e8 seconds + arrival date: 2031-12-17T19:19:24.442 + thrust profile: [0.4631902795092741 -0.08224771535152973 -0.006480928889750821; 0.41704341820262636 0.21095659271139136 -0.02620914649646857; 0.2797622883993905 0.28592479641588525 -0.047115859690752125; 0.16999303712128083 0.27059720181308317 -0.05726221774165335; 0.10505343297735933 0.24439744913692196 -0.06242988174728664; 0.06300675973086067 0.21817544269642067 -0.06368113246047818; 0.035798514967212466 0.18835657288959481 -0.06877313709544629; 0.01319570173604884 0.17195586849080916 -0.06353926803226635; -0.0028206814647056726 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0000000..ecc11df --- /dev/null +++ b/archive/EMS_2021-12-12T16:01:04.514/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EN_2021-10-14T21:24:00.053/mission b/archive/EN_2021-10-14T21:24:00.053/mission new file mode 100644 index 0000000..dee2e52 --- /dev/null +++ b/archive/EN_2021-10-14T21:24:00.053/mission @@ -0,0 +1,22 @@ +archive/EN_2021-10-14T21:24:00.053/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 2022-08-05T13:09:42.428 +Launch V∞: [7.8646219457877775, 5.391423246731976, 0.21664193585734026] km/s +Phase 1: + Planet: Neptune + V∞_in: [4.3825277514495635, 0.4972219444711066, -0.033282491583832376] km/s + V∞_out: [1.2613145775799692, 1.2541088206742887, 1.19448213244607] km/s + time of flight: 7.239210268385214e7 seconds + arrival date: 2024-11-20T10:04:44.428 + thrust profile: [0.5570971125040689 0.46523336275569166 0.24443397992833363; 0.5455353078277998 0.37771233171043145 -0.2905042836424388; 0.5373067044309571 -0.3697335845815613 -0.23280971000434258; 0.5789141430780081 -0.4290239526125613 0.17533812742230417; 0.6282895761794832 -0.4760003782283056 -0.02869288371312378; 0.5937505020656196 -0.44907996753558815 0.008871484612811375; 0.583505825104241 -0.4419058605742258 0.0024181680115527163; 0.5999629018966298 -0.4488350427074705 -0.0010636832749702108; 0.6282809657618084 -0.4727189600895791 -0.0029164733714258264; 0.6387620784811242 -0.4812400030251487 -0.004086578863408878; 0.6291065200722094 -0.4782777977932136 -0.004926811268235369; 0.6685784074664406 -0.5147308829624088 -0.005566898376192713; 0.6402182196889159 -0.4886680265057143 -0.005534056457267186; 0.7138116778721744 -0.5642610603445648 -0.006396711596120154; 0.6435783521271209 -0.5330961196095906 -0.005999671526644724; 0.596620975387932 -0.5192282791418487 -0.005575460237394601; 0.5813910956156 -0.5172814194247172 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+Launch Mass: 2500.0 kg +Launch Date: 2022-04-16T10:37:51.889 +Launch V∞: [9.93430356594082, -9.814231711705617, -9.723022803164637] km/s +Phase 1: + Planet: Neptune + V∞_in: [-3.330351073892173, -5.42324969269204, 0.08855958401956425] km/s + V∞_out: [-3.300747312670549, -3.328777757532345, 3.3127008443655095] km/s + time of flight: 1.007092354462312e8 seconds + arrival date: 2025-06-25T01:25:06.889 + thrust profile: [0.8753926904953222 0.6832826274506226 -0.12190291359862054; 0.8755956380471712 0.6667237002096869 -0.1464038516358984; 0.8745742225785343 0.5149107423186586 -0.17002603241860648; 0.8637408209307073 0.25941037509054327 -0.19687061798657313; 0.8873044529895101 -0.013949833656543549 -0.20801896083211308; 0.8603140096952885 -0.22178564312493226 -0.21226327319113722; 0.8722049558724008 -0.35639346957623513 -0.20814872623709274; 0.8798839779340266 -0.4459725813099044 -0.2408854578792029; 0.8297808636995301 -0.4620621965066881 -0.1882977763047611; 0.860562943045671 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+ + + + diff --git a/archive/EN_2021-10-14T23:27:47/mission b/archive/EN_2021-10-14T23:27:47/mission new file mode 100644 index 0000000..fce5237 --- /dev/null +++ b/archive/EN_2021-10-14T23:27:47/mission @@ -0,0 +1,22 @@ +archive/EN_2021-10-14T23:27:47/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 2022-10-01T14:30:44.231 +Launch V∞: [-1.5243188475966056, 5.9256671205622045, 0.2916154666540272] km/s +Phase 1: + Planet: Neptune + V∞_in: [3.6975966998821526, -1.4215737222278524, 0.3088257373177974] km/s + V∞_out: [3.445686587806444, 0.6826200114085932, -1.001538192708208] km/s + time of flight: 2.855355071164953e8 seconds + arrival date: 2031-10-19T09:55:51.231 + thrust profile: [-0.8759933715507354 0.9721696493713093 -0.019442309148699335; -0.8008537600952194 -0.5941302460728478 -0.06796587793610398; -0.627589785584642 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0.04136003156954945; -0.013754111231380713 0.1364854049755323 -0.023729392781819306] % + +Mass Used: 1572.0861495426557 kg +Launch C3: 37.52211835324206 km²/s² +||V∞_in||: 3.9734703394813478 km/s diff --git a/archive/EN_2021-10-14T23:27:47/plot.html b/archive/EN_2021-10-14T23:27:47/plot.html new file mode 100644 index 0000000..798871a --- /dev/null +++ b/archive/EN_2021-10-14T23:27:47/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/ES_2021-10-14T21:47:36.309/mission b/archive/ES_2021-10-14T21:47:36.309/mission new file mode 100644 index 0000000..9c9834d --- /dev/null +++ b/archive/ES_2021-10-14T21:47:36.309/mission @@ -0,0 +1,22 @@ +archive/ES_2021-10-14T21:47:36.309/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 2022-06-29T19:16:25.625 +Launch V∞: [6.0695706106569, -1.6109289130217384, -0.5333379447287113] km/s +Phase 1: + Planet: Saturn + V∞_in: [4.5493209273514195, 3.4608913977285543, -0.8868908653713397] km/s + V∞_out: [0.2563878990001578, 0.01892815524720286, -0.25544585694329036] km/s + time of flight: 2.9165245490120065e8 seconds + arrival date: 2031-09-26T09:50:39.625 + thrust profile: [0.14860958019742154 -0.20538020578753946 -0.0029857947830181546; 0.24425057362359953 -0.2010582389064345 -0.0022184731127427326; 0.06264366361767877 -0.26323134665411474 -0.015605032621348582; 0.1099776426723479 -0.2600231353505949 -0.07726868093658261; 0.33089491385526876 -0.40130576368271437 -0.02266361781007407; 0.29811739992127256 0.351626147581589 -0.01408132684301641; 0.10201345317223925 -0.054395098700720686 4.985459044362331e-5; -0.24365090429430264 -0.3034489310316968 -0.034487807729955106; -0.3334152550285137 -0.45649243866916195 -0.011088824883799378; -0.08095386910938922 -0.6725665822129208 -0.0006414830511198784; 0.7230355014836508 0.16667047850911612 0.022288360045254307; 0.46498186625266963 0.48480806636556717 -0.015108144063144823; 0.26260730236394 0.4260170082088822 -0.0328608028939281; 0.1457862799193408 0.3335616939365715 -0.04011809832347775; 0.1150253917004787 0.3411618936049045 -0.04313725384357472; 0.025947430647644983 0.23890044376344466 -0.04428837586570222; -0.03181842621885434 0.16589322750633057 -0.0438537282163; -0.07240941628806781 0.0912664675638024 -0.04627441978486195; -0.15565598989729182 -0.011295552314065267 -0.03729510262375746; -0.17780659953830016 -0.08636206589783667 -0.024129636397547234] % + +Mass Used: 860.8985796524989 kg +Launch C3: 39.71922872384681 km²/s² +||V∞_in||: 5.784519476498304 km/s diff --git a/archive/ES_2021-10-14T21:47:36.309/plot.html b/archive/ES_2021-10-14T21:47:36.309/plot.html new file mode 100644 index 0000000..e990736 --- /dev/null +++ b/archive/ES_2021-10-14T21:47:36.309/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EU_2021-10-14T21:56:32.783/mission b/archive/EU_2021-10-14T21:56:32.783/mission new file mode 100644 index 0000000..aaf3419 --- /dev/null +++ b/archive/EU_2021-10-14T21:56:32.783/mission @@ -0,0 +1,22 @@ +archive/EU_2021-10-14T21:56:32.783/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 2500.0 kg +Launch Date: 2022-06-06T12:32:32.955 +Launch V∞: [8.066701974215304, -5.184463452194054, 0.07048095785765573] km/s +Phase 1: + Planet: Uranus + V∞_in: [0.41889683618179546, 1.9616780923678787, 0.0041185023421876354] km/s + V∞_out: [-1.0813442250676473, 1.269652537135473, -1.103843466471438] km/s + time of flight: 5.623145280158398e8 seconds + arrival date: 2040-03-31T19:01:20.955 + thrust profile: [0.33113071235942554 0.37947009945825905 0.0026520116773191722; 0.14260319554091308 0.28557696226011836 0.004417291796288417; 0.06647276062018873 0.25607146683316817 0.0005698747089161628; 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0.0014259188993576994; -0.0579299799142576 -0.14259393483414515 0.0009732733502837638] % + +Mass Used: 759.4776549013495 kg +Launch C3: 91.9553095933655 km²/s² +||V∞_in||: 2.0059093846683953 km/s diff --git a/archive/EU_2021-10-14T21:56:32.783/plot.html b/archive/EU_2021-10-14T21:56:32.783/plot.html new file mode 100644 index 0000000..0ee46ae --- /dev/null +++ b/archive/EU_2021-10-14T21:56:32.783/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EVMJS b/archive/EVMJS new file mode 100644 index 0000000..658218f --- /dev/null +++ b/archive/EVMJS @@ -0,0 +1,43 @@ +archive/EVMJS--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-04-20T12:58:59.053 +Launch V∞: [-8.920597561322369, -7.117372634919496, -1.472451871563068] km/s +Phase 1: + Planet: Venus + V∞_in: [-5.017961509289203, -5.654947873213361, -1.4864114620218827] 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[0.18326801514146682 0.11845670033224177 -0.0016084372043512012; 0.1675872421589649 0.14235871799128041 -0.002787329388980011; 0.14198390921850934 0.16511394888691344 -0.0037731022920933425; 0.10352323696814321 0.18228824596062612 -0.004414585252525113; 0.052724231521741716 0.18616944898352478 -0.004616750142156716; 0.0011654214657718389 0.1688827891674893 -0.004589773974233177; -0.031151502893950005 0.13429086557793365 -0.0048861485136074976; -0.0387542725070042 0.09962903031836343 -0.005697801228946161; -0.032764472688793025 0.0752213826812925 -0.006648655387876376; -0.02303421181483975 0.059664277716287864 -0.007393815905338262; -0.013366915890350172 0.04886766638458846 -0.007849749770643184; -0.004273656127481105 0.04004011769410306 -0.008128123571266301; 0.005274989439679697 0.03136991809704025 -0.008359024971909892; 0.01659789890620425 0.02034976567361285 -0.008341112112060404; 0.027347691011068397 0.0015674507187789124 -0.007372599601001636; 0.03221036017744093 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+ duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-04-20T12:58:59.053 +Launch V∞: [-8.920597561322369, -7.117372634919496, -1.472451871563068] km/s +Phase 1: + Planet: Venus + V∞_in: [-5.017961509289203, -5.654947873213361, -1.4864114620218827] km/s + V∞_out: [-7.390394917247088, -2.021337895911062, -0.8148956710919548] km/s + time of flight: 4.572852817115571e7 seconds + arrival date: 2025-10-01T19:21:07.053 + thrust profile: [-0.21862938814794752 -0.05580927018043333 -0.036914761844326786; -0.24413346338652692 -0.02556655529310196 -0.03840768064934617; -0.26465223193143633 -0.031988862192285895 -0.03672328500867164; -0.2775111471212138 -0.0533843665242742 -0.03463858507707235; -0.282355262314745 -0.07982445428959191 -0.033636788586472385; -0.28050912409469175 -0.10607204371684377 -0.032167717475040075; -0.2733689146909765 -0.12962521272658228 -0.03161077625553056; -0.26190711303703673 -0.14877589397585794 -0.030649321801181607; -0.24697067176434023 -0.16354203331437878 -0.029534650090164597; -0.22916216500741854 -0.1736646300332696 -0.02774354605279356; -0.20930307239303453 -0.1793556553425328 -0.02624057086532488; -0.1881341647769172 -0.18020842931174086 -0.022018620586908344; -0.16781156346033524 -0.1755305190264814 -0.017713311035217196; -0.1529314715768468 -0.16133304311878607 -0.011294101805393433; -0.1439292332041623 -0.13894686830886066 -0.005512101036767262; -0.13595373894772989 -0.11376326317155387 0.008492968124788823; -0.14161082765712693 -0.0633805633113515 0.026736612907202688; -0.14271356865834361 0.024062134302168376 0.04098391846668108; -0.1414981556176295 0.035473208118311124 0.03720171942581438; -0.13060050476893825 0.04192201790827888 0.030084566679769147] % +Phase 2: + Planet: Mars + V∞_in: [-9.28829223014179, -7.607789338281241, -0.2942705558666007] km/s + V∞_out: [-8.317437974959708, -8.663545949996019, 0.030785372299447233] km/s + time of flight: 5.8747531161094815e7 seconds + arrival date: 2027-08-12T18:06:38.053 + thrust profile: [-0.174672404758962 0.02506293138125133 -0.02426121230831768; -0.05008204073446195 -0.07279118574621102 -0.08129060414874276; 0.18941101625787235 -0.07952903306738271 -0.10689582281590368; 0.35705302923506294 0.027307923111368104 -0.0479794442058468; 0.41799317552955584 0.12801887957214292 -0.029898349295167635; 0.4511914489377908 0.23489263829219467 -0.020213669874118333; 0.4656012050626349 0.3325378259130575 -0.014159348767163066; 0.4657014753978555 0.41280917091846614 -0.013135235235423743; 0.45029470699103086 0.4771859548843401 -0.012168900825375072; 0.4106794937152572 0.5294663391131441 -0.011594787023374607; 0.33819071474272516 0.5678785558859125 -0.010353193332547849; 0.2001630795815917 0.5937428427734591 -0.00709996654137991; -0.035108210746352266 0.6005435960325474 -0.0011602329790232843; -0.29361875930485426 0.5723600768872681 0.008300256500510222; -0.4548836328849185 0.4770722319186511 0.014296267759918423; -0.5113471724292226 0.19706675000368873 0.01697398652461365; -0.4134871925757221 -0.2340982056617441 0.01763457992701102; -0.17230637273503518 -0.34708241891449854 0.032309764753320355; 0.1190741484482409 -0.3404978442614275 0.03287368817385319; 0.30168780764812786 -0.2869031294203351 0.028403718812872233] % +Phase 3: + Planet: Jupiter + V∞_in: [-2.998311290651761, -5.22937520865022, 0.1407756821047572] km/s + V∞_out: [-2.856148992180316, 5.306598853387247, -0.19607428788923498] km/s + time of flight: 1.4159768899978405e8 seconds + arrival date: 2032-02-06T14:48:06.053 + thrust profile: [0.37857744177475117 -0.5722922563923073 0.022790081593862904; 0.4498819042137626 -0.33368177218590706 -0.006756732610181868; 0.45137346520621063 0.2646268898149342 -0.06715401087102708; 0.3370898120722347 0.5147560334694927 -0.0942931710827749; 0.10406019537076351 0.6331750657513396 -0.10357703864723887; -0.3067722620848112 0.6948315815503575 -0.0862070073278207; -0.5894971893625187 0.7222874275705 -0.047061967331428964; -0.7438646368242161 0.7031736402976893 0.007847733426895626; -0.8153797919927924 0.4618300002958423 0.06963851455772195; -0.8054139924887445 -0.5908908470157955 0.097381115730603; -0.6892129370491469 -0.7264006520777874 0.08776061857832115; -0.45980277149808124 -0.7029156090490672 0.07926634239802542; -0.23430875626887712 -0.6386864247061581 0.07411409321833815; -0.11447347572705899 -0.5560871561049769 0.0680750057792953; -0.06705788386230047 -0.46200938046607043 0.06022766091205061; -0.049086029532628715 -0.35725786450463903 0.05078115410828272; -0.04044489185865085 -0.23996050920253587 0.04039683492314978; -0.034110498545589486 -0.10823424969630317 0.03211353029920855; -0.025504423988764145 0.06607493481717405 0.015337634169998754; -0.016379042728758193 0.201103314416455 -0.001097801876741442] % +Phase 4: + Planet: Saturn + V∞_in: [-3.7553623927693303, 3.8045661430805238, -0.0017497584909869502] km/s + V∞_out: [0.00016771014375336496, 0.02190103395006303, -0.00015322066785738935] km/s + time of flight: 2.0181733919676498e8 seconds + arrival date: 2038-06-30T11:10:25.053 + thrust profile: [0.18326801514146682 0.11845670033224177 -0.0016084372043512012; 0.1675872421589649 0.14235871799128041 -0.002787329388980011; 0.14198390921850934 0.16511394888691344 -0.0037731022920933425; 0.10352323696814321 0.18228824596062612 -0.004414585252525113; 0.052724231521741716 0.18616944898352478 -0.004616750142156716; 0.0011654214657718389 0.1688827891674893 -0.004589773974233177; -0.031151502893950005 0.13429086557793365 -0.0048861485136074976; -0.0387542725070042 0.09962903031836343 -0.005697801228946161; -0.032764472688793025 0.0752213826812925 -0.006648655387876376; -0.02303421181483975 0.059664277716287864 -0.007393815905338262; -0.013366915890350172 0.04886766638458846 -0.007849749770643184; -0.004273656127481105 0.04004011769410306 -0.008128123571266301; 0.005274989439679697 0.03136991809704025 -0.008359024971909892; 0.01659789890620425 0.02034976567361285 -0.008341112112060404; 0.027347691011068397 0.0015674507187789124 -0.007372599601001636; 0.03221036017744093 -0.01353396250128953 -0.004949290348108288; 0.03641858295092107 -0.025405796803472054 -0.003362734977936097; 0.04156323966242008 -0.03555478122658915 -0.002142996490186938; 0.04760308383336786 -0.0450888885925399 -0.0011510722358481168; 0.05448090196904719 -0.0542737048917187 -0.0003050212878129177] % + +Mass Used: 1175.3239683910674 kg +Launch C3: 132.40216858944106 km²/s² +||V∞_in||: 5.345790240905041 km/s + + + diff --git a/archive/EVMS_2021-12-13T10:50:18.877/mission b/archive/EVMS_2021-12-13T10:50:18.877/mission new file mode 100644 index 0000000..598c592 --- /dev/null +++ b/archive/EVMS_2021-12-13T10:50:18.877/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EVMS_2021-12-13T10:50:18.877/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-09-04T21:45:02.327 +Launch V∞: [-5.6873787586821285, -5.786560442422183, 0.9648939525882495] km/s +Phase 1: + Planet: Venus + V∞_in: [-7.006322293689667, -9.989734050925524, 1.6254097214081484] km/s + V∞_out: [-4.934010055766463, -9.703163112990516, 5.746968526613558] km/s + time of flight: 6.009580685315006e7 seconds + arrival date: 2026-08-01T11:01:48.327 + thrust profile: [0.9617110897949794 -0.8739870599865779 0.8811871230841061; 0.9871206021010024 0.9481933351857079 0.8854228336153014; 0.9863523895604293 0.994327102707624 0.946716091473592; -0.9902056621813372 0.9875449005030636 0.9064066950201374; -0.9820144764851901 0.9653224112558945 -0.8337378769726054; -0.9555449311854642 0.9657521915091073 -0.8456397221554082; 0.8186521316331613 0.967179361186583 -0.8354191171549058; 0.9767230165471376 0.9633104362664976 0.8377573650125992; -0.923042165035667 0.9919872228857152 0.9072115878002239; -0.9795463340184644 0.9795259853082192 0.8043752807295302; 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0.19857305554347673 -0.15250831748180288 0.670517038923704; 0.7186153785765315 -0.29289494991471887 -0.6203374026439823; 0.7630231141068492 0.7474131605948617 -0.34388402323483247; -0.14653416819603318 0.7578630202380595 0.6440008885838143; -0.5716565111866172 0.05476072550231505 0.5826761302304793; 0.7550937919052704 -0.5973801143592986 -0.5772563443665387; 0.8445567824974203 0.7474760718003378 -0.39238459367822853; 0.4972794197237329 0.8504015084039828 0.5954464117194335; -0.6051101474071697 0.6920479334729668 0.6384433528223871; -0.5485003210233016 -0.6848384869177934 -0.17001698436070412; 0.8818645425824932 -0.5572287228442382 -0.6059169981172697; 0.9056867468320952 0.8620079636158319 -0.21179500810720392; 0.4498657884312737 0.9206863989478159 0.626472113013419; -0.7063855626923453 0.8392260172345695 0.6657911934666387; -0.7725890297740363 -0.6321620848297606 0.35516589931735515; 0.7603264864364883 -0.8557533022845115 -0.6311629259349868; 0.9561247545973677 -0.5017701499231864 -0.6272119558821079; 0.9705083590037089 0.91129864219974 -0.2888985356409027] % +Phase 3: + Planet: Saturn + V∞_in: [5.038952819515676, 7.9798066215675565, -0.8715896824986642] km/s + V∞_out: [-0.012236099214684017, -0.9981497941651291, -0.828378100790254] km/s + time of flight: 2.2176624458787963e8 seconds + arrival date: 2036-12-07T01:48:56.327 + thrust profile: [0.9561858721260394 0.9849199946256132 0.5225438470279931; -0.027932742829215068 0.9733888937163413 0.43219740244487903; -0.44415834968745566 0.9310525799775682 0.30834923084684457; -0.41854368011913534 0.8702966170896927 0.208080577565248; -0.32933795593388565 0.815451911934079 0.1254126724065932; -0.23552180201632114 0.7723076604175301 0.06921155682993804; -0.1614904990435074 0.73600434327184 0.037191049603114215; -0.10093276866257177 0.7015622404196313 0.01739015687986595; -0.07061055518612644 0.6657821229767328 0.004884538754076532; -0.04673703754899972 0.625817515327918 -0.0025122978941227465; -0.041112337800284074 0.5793466390354832 -0.006303799076519013; -0.04283624698244216 0.5243842265930279 -0.007497163409016717; -0.05346092222703407 0.459582480493242 -0.0067340993382808785; -0.06895608005212821 0.3833475120313622 -0.004880957209105144; -0.09923125957632768 0.29425585856793157 -0.0013249599275947555; -0.13231914932868194 0.1912438331345806 0.00453604080839281; -0.15508316129336963 -0.043236971591321775 0.007944115104287169; -0.17629889261241166 -0.11291544563125626 0.012864022185234279; -0.14568672081150158 -0.25880004071832907 0.015796279090581688; -0.1516335446629711 -0.3568240854796575 0.021534187052804105] % + +Mass Used: 2773.596934253452 kg +Launch C3: 66.76157923825527 km²/s² +||V∞_in||: 9.477764916347974 km/s diff --git a/archive/EVMS_2021-12-13T10:50:18.877/plot.html b/archive/EVMS_2021-12-13T10:50:18.877/plot.html new file mode 100644 index 0000000..25dd7a2 --- /dev/null +++ b/archive/EVMS_2021-12-13T10:50:18.877/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EVMS_2021-12-13T15:09:50.799/mission b/archive/EVMS_2021-12-13T15:09:50.799/mission new file mode 100644 index 0000000..5778d91 --- /dev/null +++ b/archive/EVMS_2021-12-13T15:09:50.799/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EVMS_2021-12-13T15:09:50.799/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2023-03-26T07:12:24.150 +Launch V∞: [-4.691695981755256, 2.4100997067687473, -1.107625419239362] km/s +Phase 1: + Planet: Venus + V∞_in: [-4.566977871130657, 4.760076803915006, -1.7341280162885988] km/s + V∞_out: [-6.208492431552701, -1.9096233111972523, -2.080047657050257] km/s + time of flight: 2.0717178639097057e7 seconds + arrival date: 2023-11-21T01:58:42.150 + thrust profile: [-0.14461666591877725 -0.010674923527958081 0.07319622237982218; -0.2632510872185629 0.01896952413347131 -0.11219362381384182; -0.35509253776259864 0.05130847606843313 -0.1020767266141743; -0.43017679281809584 0.05045981562535008 -0.1422217250671829; -0.5045985167824136 0.01741583415172031 -0.16844373611917648; -0.569330040676884 -0.05201323466205199 -0.18486385532265195; -0.6249141520690602 -0.13905479590410533 -0.19964164942840817; -0.668271188513656 -0.2602797013356586 -0.20608604356710608; -0.6652598099366694 -0.39412254799113705 -0.19894484200845694; -0.71516785653991 -0.49228396872807745 -0.21106475073434702; -0.7140520681258179 -0.6492058751655467 -0.1932030922695093; -0.6868766770794695 -0.7396924869993249 -0.17353711242581565; -0.6152532209931442 -0.8020815173678328 -0.14764124943790446; -0.4622171233071141 -0.8398654668968106 -0.11185995276929935; -0.16854886447084155 -0.849107084555043 -0.06766821177549498; 0.23324400917872504 -0.8297560629709333 -0.01536095606168015; 0.5186243199535893 -0.769610557984718 0.03995200418629567; 0.6187570125005067 -0.6500477297841986 0.08764709560669148; 0.5808087120622782 -0.5121872212939763 0.11783856477232442; 0.4583737403324055 -0.3712720822360683 0.13462225195583247] % +Phase 2: + Planet: Mars + V∞_in: [-9.200127095735333, -6.894307184186653, -0.4734726391357551] km/s + V∞_out: [-7.90745728238742, -8.353687515473082, -0.3001668168215188] km/s + time of flight: 5.676487860450122e7 seconds + arrival date: 2025-09-08T02:00:00.150 + thrust profile: [0.9450818166379835 -0.39326487285299566 0.08478396733763034; 0.5033926889693318 -0.49600851782195465 -0.09864181576764529; 0.593874568813462 -0.5134648071397765 -0.21563608217734162; 0.6726275954838512 -0.44694734612516734 -0.3151164039729524; 0.6947676879446373 -0.29388960390973834 -0.3690682632127033; 0.7117640920103931 0.07243876441940703 -0.41029659430010107; 0.7001034602049846 0.6195031306652655 -0.4186969404202771; 0.695103119957999 0.6808867140504492 -0.4033934445136916; 0.6468162520522805 0.7276709960247509 -0.3673200063653498; 0.5786083720048963 0.7618030225293763 -0.2740863676479381; 0.43998280657362615 0.7813682905260836 -0.09859638125917183; -0.04546726863354173 0.7884156184890568 0.05317843281930274; -0.6546093330399981 0.7727091843423107 0.11218174811377148; -0.7965171690457952 0.7496124509846286 0.19970259425421277; -0.8736983626104139 0.6200392713895918 0.2654841797347523; -0.9103125128246278 -0.6456308917849752 0.27992773703210205; -0.9019970750226028 -0.9023670767015256 0.1864233187998923; -0.6771646049748614 -0.9414644139448815 0.011110810182933379; 0.3521154040459276 -0.9440844390692263 -0.16519285405497774; 0.7774895055238358 -0.9371489950391606 -0.2516063758929405] % +Phase 3: + Planet: Saturn + V∞_in: [5.616813665429002, 6.787110157183047, 1.2069938406439464] km/s + V∞_out: [2.1970387730495697, 3.225023288265242, 4.175802839196012] km/s + time of flight: 1.6257487956751725e8 seconds + arrival date: 2030-11-02T17:41:19.150 + thrust profile: [0.9505134233163771 -0.979494400300436 -0.30984147298673975; 0.9511180319113616 -0.9647970604644283 -0.6501969016781382; 0.9424633459203795 -0.9926658842113464 -0.6207418959532092; 0.9304882859838348 0.23850084565208374 -0.5933249374851602; 0.9098194053379338 0.5493464195536784 -0.5111960642202787; 0.8829443918138722 0.6659627102171121 -0.3774953044827189; 0.8472666578022966 0.7031440366152961 -0.2698632635749556; 0.8051838923072202 0.7113118353482547 -0.23246846453046197; 0.7503491889394095 0.7106325372593361 -0.03813921871732603; 0.6848270191956657 0.702152969321232 0.03334922254887817; 0.6172988381336922 0.6882916490356381 0.08048503574576253; 0.5480320293122681 0.6685098976431961 0.10512250251977935; 0.4755966950131009 0.636871879957033 0.11757167935113788; 0.3912388892675421 0.5870441077418865 0.12131662398055057; 0.3071016125028102 0.5153387959524959 0.11568557231704885; 0.2061494535664333 0.42029155244133604 0.10481292164087117; 0.14105224096703986 0.31043414548479376 0.09141235006535123; 0.04128524414299072 0.18984755798020106 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kg +Launch Date: 2024-01-06T04:29:48.093 +Launch V∞: [0.5457290374235895, 4.341334791096552, -0.7559687755701914] km/s +Phase 1: + Planet: Venus + V∞_in: [0.8335159107192338, 6.90456105315263, 3.5067701274587337] km/s + V∞_out: [6.76973645767487, 3.7624182770964607, 0.8285997001531188] km/s + time of flight: 1.0236386879690988e8 seconds + arrival date: 2027-04-04T22:54:16.093 + thrust profile: [0.20124636719972494 0.28871460999851783 -0.24826466053632043; 0.21757301989581354 0.24241685861764573 -0.2950961505210993; 0.271442849091815 0.07872734315816171 -0.19097989520692127; 0.1879742866678929 0.27655633192716367 0.10042573300235896; -0.14244608091005748 0.33201061328346854 0.19340046097242167; 0.17387986662182686 0.3014608753850556 -0.15431719711609648; 0.18777345028680853 0.2673897380502672 -0.25525617202163087; 0.2556315993639935 0.17739994769888612 -0.27159167007539076; 0.26609722508102157 0.2783459216563457 0.051977998587726774; 0.0438700045849084 0.37141025221234536 0.20109295136087044; 0.06232447288714108 0.35663405987308516 0.024990128722474907; 0.026521151688839967 0.3160983251683631 -0.16548739972882243; 0.19612956542640614 0.24782370475857005 -0.2471047602651378; 0.31651280507021246 0.18621565754181835 -0.19804312266917037; 0.24435157836852087 0.3468639663937176 0.1852596358565247; -0.00965870127546034 0.3979396968294011 0.22213565307438407; 0.023169341463938578 0.30016276019204574 -0.18664622656660942; 0.1268886531461076 0.20680899035126646 -0.25936562207083624; 0.2125169373278653 0.24319285890159614 -0.22236991044858823; 0.35244171182303646 0.25085960304558635 -0.1638088094827891] % +Phase 2: + Planet: Mars + V∞_in: [8.963228181916202, 3.147920284899006, -0.7449749580149643] km/s + V∞_out: [9.377239868662178, 1.0270817933951877, -1.3450268054813155] km/s + time of flight: 1.22946548225175e8 seconds + arrival date: 2031-02-25T22:43:24.093 + thrust profile: [0.2815247284876436 0.4687108668970388 0.07024363175566978; -0.28575122080824394 0.3851477052454153 0.016801525539966562; -0.3747967738284827 0.29808121010819033 -0.07185502866615309; -0.442929227216859 0.19222627634169495 -0.135743553778548; -0.4487478745447117 0.1327038699880746 -0.09503248552633654; -0.49852432866134694 -0.13114566918915876 0.14249733878062454; -0.4800686097933296 -0.20421918036330872 -0.007593654428925882; -0.29831925246774027 -0.05272129811015332 -0.01656649869964936; 0.035964682967361335 -0.09683145552380305 -0.15527299210182244; -0.09302182221116087 -0.33887428309830736 -0.2404084153476241; 0.5923912702376002 -0.02542163181573757 0.2009826493089844; -0.02623028033428319 0.13880579512402433 0.24850570533865052; 0.29039130962158227 0.3062352881282009 0.1527335375754828; -0.12082271353315516 0.4096496613048553 0.02796560796386028; -0.027194067272572214 0.35743634565580396 -0.04064730736657738; 0.04127166490432071 0.24768556235295525 0.09118781754436289; -0.11854966698415786 0.22553475056440592 0.08555412347860751; -0.1806405003127596 0.10096300132551984 -0.15472306505086783; -0.20075020241889296 -0.009061662245205257 -0.11023054116740935; -0.2987954790790834 -0.230652241463122 -0.11725959697110766] % +Phase 3: + Planet: Saturn + V∞_in: [-3.1812528488033522, 8.51185716671171, -0.7460758734937367] km/s + V∞_out: [-0.21505538492794815, 6.349830695161589, -0.12985627371130587] km/s + time of flight: 1.315250993552624e8 seconds + arrival date: 2035-04-28T05:28:23.093 + thrust profile: [0.7987730439865184 -0.41345767452772897 0.001505324112112355; 0.8674728852573501 0.6602259691893515 -0.0759345729834176; 0.7597133759248544 0.8594908841609692 -0.19125255627342094; 0.2872093106917861 0.8668264267695036 -0.18904379386155162; -0.5401943922623963 0.8498080030613695 -0.16437663889563423; -0.6896408194237241 0.8199272255247071 -0.15201175224165175; -0.7134753635114731 0.7870386683779858 -0.14239308646192794; -0.7170346050334127 0.7501463142097656 -0.13294598405115826; -0.7002315120575128 0.7090750008587086 -0.12315905659225605; -0.6872097378697336 0.6676696143275933 -0.11572226052465101; -0.6627939184703779 0.6168905813867107 -0.10527146741337202; -0.633554979686539 0.5685903428331747 -0.09336745543158023; -0.5918530549537074 0.508122677783068 -0.07972015422869783; -0.5468540100379315 0.43929599357406623 -0.06477133727408631; -0.48985935766804956 0.3608169402041227 -0.04832795620510983; -0.42117899759427235 0.2697982895066768 -0.030347981218191687; -0.3351818344708077 0.16466291198509436 -0.01189485088684984; -0.23232691164467884 0.0500315224688059 0.00787577036146254; -0.1131949765395752 -0.06833292217756129 0.02847742053557143; 0.005991615157979781 -0.182291757352861 0.05024929371428449] % + +Mass Used: 1536.01990119313 kg +Launch C3: 19.71649674030971 km²/s² +||V∞_in||: 9.117494794269444 km/s diff --git a/archive/EVMS_2021-12-13T17:44:34.669/plot.html b/archive/EVMS_2021-12-13T17:44:34.669/plot.html new file mode 100644 index 0000000..41fbddf --- /dev/null +++ b/archive/EVMS_2021-12-13T17:44:34.669/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EVMS_2021-12-13T21:46:30.548/mission b/archive/EVMS_2021-12-13T21:46:30.548/mission new file mode 100644 index 0000000..24284a8 --- /dev/null +++ b/archive/EVMS_2021-12-13T21:46:30.548/mission @@ -0,0 +1,36 @@ +/home/connor/projects/thesis/archive/EVMS_2021-12-13T21:46:30.548/mission--------------------------- + +Spacecraft: mySat + dry_mass: 200.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.00025 kN + num_thrusters: 1 + duty_cycle: 1.0 +Launch Mass: 3500.0 kg +Launch Date: 2024-05-14T22:50:54.151 +Launch V∞: [1.1286314645978788, 6.894494804991318, -0.8285243221011761] km/s +Phase 1: + Planet: Venus + V∞_in: [-0.4975358362817743, 7.143314145080825, 1.4331811045093779] km/s + V∞_out: [6.0255649206667625, 4.05582288696785, 0.7567303017536462] km/s + time of flight: 5.201873526429285e7 seconds + arrival date: 2026-01-07T00:29:49.151 + thrust profile: [-0.13658867986140374 -0.24246001363888786 -0.0018351721366561648; -0.19874653605027093 -0.42347951183192895 0.059887224602709746; -0.006030933718274198 -0.6165659086877646 0.05143110252875157; 0.5690891294297716 -0.6337278673409295 -0.012184805314118167; 0.6969370055919233 -0.3303175586786053 -0.07217788171252011; 0.64128971249768 0.26314536468162564 -0.09952967531295756; 0.5208719713422499 0.32770505919622234 -0.10513933945114934; 0.4271266849981205 0.20190088190483316 -0.10365532774681949; 0.4176630482221774 -0.011898915901332388 -0.08241345687785652; 0.47262980673060484 -0.13896143178119608 -0.03374381004058062; 0.4421659456699236 -0.17124612763461697 0.02403617877878262; 0.3583106766681072 -0.28808344084851756 0.06553065121634129; 0.4748177430173668 -0.46986296014010215 0.04039987329214622; 0.5807725097378242 -0.2734128860609197 -0.035376229041435836; 0.5547393823521555 0.03932247507743895 -0.09732884535240749; 0.4576988071163949 0.017725627686673677 -0.1304971469405435; 0.40441128328564385 -0.22624714092575637 -0.12589052393340233; 0.5227891982702978 -0.37951138376215193 -0.08197543798043004; 0.6869211599682585 -0.3895945340441026 -0.04215815195764137; 0.6943636261137554 -0.06601804604492464 0.0018331949690765612] % +Phase 2: + Planet: Mars + V∞_in: [6.338828850719935, 0.2060782119786431, -0.4977472310639235] km/s + V∞_out: [5.762367354839256, -2.687069620550792, -0.2168349056959969] km/s + time of flight: 3.949974283472407e7 seconds + arrival date: 2027-04-09T04:38:51.151 + thrust profile: [0.458336717149733 0.1771870373806907 0.056427191918473445; 0.403817033597994 0.351117374215139 0.15075644725276122; 0.048711917893504396 0.41093296017258263 0.16380972666043295; -0.18354926599538152 0.4256482504531366 0.15401233744770568; -0.42370527996013474 0.23794979462159155 0.1314849420842794; -0.5679456579714863 0.1393409941124382 0.09924531892954472; -0.6520211065270787 0.025161300456823018 0.0635649864433606; -0.6989667221671542 -0.10489669213488008 0.0253021698618907; -0.7262214288474695 -0.24555410262257685 -0.0121562278547937; -0.743313608223649 -0.384644672098393 -0.05649462601447925; -0.7525404848639327 -0.507291521547137 -0.08734741229955949; -0.7578561155541664 -0.5996752434898261 -0.12360313032488564; -0.7592183352851313 -0.665338122647058 -0.15810104649178947; -0.7558073245676104 -0.7094328622253643 -0.19027889839324838; -0.7464517819119382 -0.7464555301053758 -0.21801144025375926; -0.7296456019615701 -0.7634101584430326 -0.24323055639952082; -0.7009447676318107 -0.7794725581151669 -0.262851486143965; -0.6543199308894584 -0.7903707443682346 -0.2772415958605197; -0.5827848217677881 -0.8004854095656452 -0.28523650701311554; -0.4849301355226277 -0.8048943851748858 -0.28659470269055276] % +Phase 3: + Planet: Saturn + V∞_in: [4.322617308702803, 2.354348521583675, -0.7376335957485771] km/s + V∞_out: [3.011554362103189, -2.0958590497922804, -2.908427301510971] km/s + time of flight: 1.8820349650227648e8 seconds + arrival date: 2033-03-26T11:23:47.151 + thrust profile: [0.9368347194497842 -0.965371940721398 -0.5613882989973752; 0.9714384488821548 -0.7607872705031594 -0.09024131587466705; 0.9505668891632969 0.8312812365923358 0.07095989545704967; 0.8695060114456342 0.8325193176250749 0.07116267827484891; 0.6939833190653248 0.8028129129322639 0.031577569215995506; 0.49217044040756264 0.7963553158741095 -0.021466953451174452; 0.3421171062041329 0.6993381181757932 -0.06563494914488495; 0.24925579641473375 0.4813067954039389 -0.1267909830819491; 0.19205090715099823 0.2932984515362608 -0.11766481272251779; 0.15209938030796544 0.1642850960501914 -0.12314405675789696; 0.11581486470625263 0.09373283562323559 -0.12395161654174959; 0.08005933539569969 0.07505479185768685 -0.11065807756901873; 0.04290428379494743 0.06421252941862582 -0.09362719990942882; 0.009670159523961858 0.05833849578599656 -0.07211230161173374; -0.05839187604989335 0.06373138672808198 -0.06233551857721689; -0.012522824962244553 0.049309431568300005 -0.040752415650939504; -0.04320895480635503 0.05485848479687612 0.0021594467585038988; -0.03809749205187863 0.0378883881221725 0.04099809276024048; -0.035012269320380346 -0.006618884738808792 0.05971979961122836; -0.03288959167972974 -0.001403295597270634 0.07024375436873588] % + +Mass Used: 1258.284359858289 kg +Launch C3: 49.49432015124584 km²/s² +||V∞_in||: 4.977155882645959 km/s diff --git a/archive/EVMS_2021-12-13T21:46:30.548/plot.html b/archive/EVMS_2021-12-13T21:46:30.548/plot.html new file mode 100644 index 0000000..984e1cd --- /dev/null +++ b/archive/EVMS_2021-12-13T21:46:30.548/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EV_2021-10-14T13:05:26.925/mission b/archive/EV_2021-10-14T13:05:26.925/mission new file mode 100644 index 0000000..3030bf1 --- /dev/null +++ b/archive/EV_2021-10-14T13:05:26.925/mission @@ -0,0 +1,22 @@ +archive/EV_2021-10-14T13:05:26.925/mission--------------------------- + +Spacecraft: mySat + dry_mass: 2000.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 1.0 +Launch Mass: 4000.0 kg +Launch Date: 2021-10-18T09:45:17.709 +Launch V∞: [0.3617667798192156, -2.039064934241794, -0.4342053441028627] km/s +Phase 1: + Planet: Venus + V∞_in: [0.7379871188280966, -2.392854603152152, 1.8896396443096521] km/s + V∞_out: [1.5127292165463757, 1.3099790858071492, 1.5207956068242738] km/s + time of flight: 1.3532010222205028e7 seconds + arrival date: 2022-03-24T00:38:47.709 + thrust profile: [0.11231015117371024 0.007222064740843916 0.047728104397320795; 0.12870381785557966 0.0566247978579788 0.21123650796860152; 0.12027023095334755 -0.008319633479200587 0.2578960766796108; 0.1347206943320554 -0.041609855302546406 0.30007660604057945; 0.19732275634506516 -0.048371534566925216 0.3566123678413536; 0.21018837696130593 -0.024190305368071867 0.38809649284784414; 0.28257952762883287 -0.010112243164057075 0.41959051839022865; 0.2845322594924626 0.05626043110186557 0.4427965235656657; 0.31989327360636083 0.10103389278981802 0.4572574662714401; 0.33347393333469577 0.06241718586254669 0.4778597182282868; 0.3395281862489285 0.10625631669191643 0.48095526186056015; 0.3383164423285961 0.1315535303664453 0.47222541173940435; 0.3311524095828194 0.16330336645453894 0.4609284090556696; 0.3201419295734179 0.1732833508978107 0.44244539961592666; 0.3013233347975498 0.20789558713014178 0.4227677382665769; 0.2721414750714771 0.17990409519215725 0.377125147146521; 0.198279076527229 0.21324470037966742 0.33028246998700145; 0.16370869214515785 0.10728022878269601 0.2608933387609283; 0.0684810317630511 0.08638181193636332 0.17016012690566112; 0.09669087307328576 0.06507874083792248 0.01466958168256049] % + +Mass Used: 183.95963971161564 kg +Launch C3: 4.477195289882742 km²/s² +||V∞_in||: 3.1370553270112 km/s diff --git a/archive/EV_2021-10-14T13:07:15.278/mission b/archive/EV_2021-10-14T13:07:15.278/mission new file mode 100644 index 0000000..d39fa09 --- /dev/null +++ b/archive/EV_2021-10-14T13:07:15.278/mission @@ -0,0 +1,22 @@ +archive/EV_2021-10-14T13:07:15.278/mission--------------------------- + +Spacecraft: mySat + dry_mass: 2000.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 1.0 +Launch Mass: 4000.0 kg +Launch Date: 2021-10-22T22:17:17.936 +Launch V∞: [1.080421766777506, -2.0628288582618195, -0.4536456444832625] km/s +Phase 1: + Planet: Venus + V∞_in: [0.7677143929066254, -3.4082880069676302, 2.3505897429525078] km/s + V∞_out: [-1.2798972791822951, -1.4365988008982025, 1.4502645187385164] km/s + time of flight: 1.4034657251252254e7 seconds + arrival date: 2022-04-03T08:48:14.936 + thrust profile: [0.1077661610742549 -0.09491507818452108 0.05312663076674047; 0.12462914010398723 -0.07372591873371813 0.073138215254182; 0.116881889714844 -0.06002677793428502 0.08095094342691629; 0.08293330133219345 -0.033724789600279505 0.12504790352006753; 0.09536827065302887 -0.004670650549755097 0.12635922504551902; 0.11091447261989335 0.004225864016796435 0.11537170625950409; 0.11303189248647355 0.03522866468488595 0.10914719877371856; 0.10740688646287562 0.06346630312429946 0.10249991019205282; 0.10449348372920764 0.05724537061115196 0.11359932836059951; 0.10049809726762707 0.07718474763324121 0.10349197510314542; 0.1007467313556788 0.08871232473224286 0.09586219439229779; 0.09639430875336537 0.10697634912585294 0.0790205018556672; 0.07665394337566692 0.1131155289012668 0.09223832705427028; 0.059511019561048636 0.12561664167233738 0.08431030720745564; 0.043597933388487026 0.13349728498081367 0.08121771907181134; 0.019379366866230683 0.14556439472332783 0.0634054361596215; 0.014456095940828476 0.14570335135746015 0.061398125952688364; -0.030752555428140677 0.1509195385631795 0.02876841287831368; -0.07387466238056084 0.13312162588233253 -0.034469925955284295; -0.02102718303541206 0.15219056670120726 -0.0065142822772471356] % + +Mass Used: 71.46119686087513 kg +Launch C3: 5.6283684633630235 km²/s² +||V∞_in||: 4.210829451211353 km/s diff --git a/archive/EV_2021-10-14T13:07:15.278/plot.html b/archive/EV_2021-10-14T13:07:15.278/plot.html new file mode 100644 index 0000000..647c590 --- /dev/null +++ b/archive/EV_2021-10-14T13:07:15.278/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EV_2021-10-14T13:09:46.191/mission b/archive/EV_2021-10-14T13:09:46.191/mission new file mode 100644 index 0000000..d0f4d30 --- /dev/null +++ b/archive/EV_2021-10-14T13:09:46.191/mission @@ -0,0 +1,22 @@ +archive/EV_2021-10-14T13:09:46.191/mission--------------------------- + +Spacecraft: mySat + dry_mass: 2000.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 1.0 +Launch Mass: 4000.0 kg +Launch Date: 2022-08-27T18:20:28.271 +Launch V∞: [4.976680389443524, -1.705424182457512, -0.3485682941979716] km/s +Phase 1: + Planet: Venus + V∞_in: [4.210457531789055, 0.3638419019608806, 2.167260083943969] km/s + V∞_out: [-0.02718879860259023, 0.00013680384875937985, -0.40279343753838176] km/s + time of flight: 2.616182260016269e7 seconds + arrival date: 2023-06-26T13:30:50.271 + thrust profile: [0.1081478833164793 -0.04747352000316829 0.009803784528203987; 0.11190267398595631 -0.08489441529847341 -0.007286984410559111; 0.12911430752493627 -0.11099328002003525 -0.01943723546946303; 0.16688603565301258 -0.12840027043968893 -0.02332008672269124; 0.21714048180407453 -0.1362382567528611 -0.02567076757100798; 0.2764401329174762 -0.13402041782174592 -0.0287511421326799; 0.33266188746520187 -0.11957670801586273 -0.031093308044346353; 0.3820659935956181 -0.09253553276581379 -0.031479580308358644; 0.41374954552181137 -0.05951601425001449 -0.03348539939450036; 0.4271557515022211 -0.02469794622072092 -0.03284633186694413; 0.4196852691041662 0.011180284532007942 -0.03287929676767141; 0.39104446127168524 0.05467052960463492 -0.03128098668740266; 0.3397344905954879 0.11008642002736206 -0.024504191585152588; 0.2681377457360699 0.17570003550101684 -0.016577172053069123; 0.046833731659678475 0.23938547094636797 0.008263855085563338; 0.20692889271962633 0.2635523571087766 0.020761614548693325; 0.13667494276947326 0.28012067330618706 0.033686527674503336; -0.11957290103408791 0.269968116350337 0.04482701107136116; -0.16727049842201927 0.21796253025589696 0.0361909665435463; -0.21921062997276963 0.1091389154173985 0.005030961855685549] % + +Mass Used: 250.70235015664184 kg +Launch C3: 27.797319196502702 km²/s² +||V∞_in||: 4.749457845699708 km/s diff --git a/archive/EV_2021-10-14T13:09:46.191/plot.html b/archive/EV_2021-10-14T13:09:46.191/plot.html new file mode 100644 index 0000000..05bff00 --- /dev/null +++ b/archive/EV_2021-10-14T13:09:46.191/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EV_2021-10-14T13:09:51.898/mission b/archive/EV_2021-10-14T13:09:51.898/mission new file mode 100644 index 0000000..5e52ee3 --- /dev/null +++ b/archive/EV_2021-10-14T13:09:51.898/mission @@ -0,0 +1,22 @@ +archive/EV_2021-10-14T13:09:51.898/mission--------------------------- + +Spacecraft: mySat + dry_mass: 2000.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 1.0 +Launch Mass: 4000.0 kg +Launch Date: 2021-10-18T18:36:15.124 +Launch V∞: [1.0916199935243702, -1.9934859843614063, -0.6362963816167255] km/s +Phase 1: + Planet: Venus + V∞_in: [0.5827260218152104, -3.245906754637226, 2.514356091647749] km/s + V∞_out: [0.7695910297576717, -0.7556093941856095, -0.9104795095643681] km/s + time of flight: 1.4088953343151927e7 seconds + arrival date: 2022-03-30T20:12:08.124 + thrust profile: [0.03400397265810093 -0.1316395434244445 0.05699291900148288; 0.10473854742812332 -0.10525549757762309 -0.0006423273456525108; 0.11599902542775602 -0.06774249825652275 0.080606830950913; 0.1310987485805775 -0.04491628698617216 0.08120644367980684; 0.11533623131335603 -0.007730090103315951 0.12352673112630569; 0.11050163762503666 -0.014810624798424184 0.13358846300335825; 0.1368738413328123 0.031717507020523894 0.10537133013453537; 0.09607405762646531 0.039259635505570926 0.15075696692326396; 0.0932396587968502 0.050763423433988285 0.1524441259012387; 0.08835554978882662 0.06063431886658857 0.15285406762333867; 0.08337674859842645 0.07132142354385927 0.1521790088231852; 0.0783436520935084 0.07932345824922571 0.14956272424615258; 0.07190901949541267 0.09252700451278721 0.14364426645965755; 0.06152160664529564 0.10487327862985339 0.1337849292702545; 0.04522536761353614 0.12354914208182705 0.12221429106614988; 0.030730806933955798 0.1497661375884409 0.07201582662332497; 0.0013732827723847787 0.13783629400588643 0.09217277545311839; -0.047657124648179124 0.14299205548044944 0.04461491903740098; -0.04887637661869137 0.14261702502367085 -0.01118738193598132; -0.04624479767152048 0.12992926199532367 -0.060407791765814726] % + +Mass Used: 76.32181558799766 kg +Launch C3: 5.570493665366048 km²/s² +||V∞_in||: 4.146982858887446 km/s diff --git a/archive/EV_2021-10-14T13:09:51.898/plot.html b/archive/EV_2021-10-14T13:09:51.898/plot.html new file mode 100644 index 0000000..de1b215 --- /dev/null +++ b/archive/EV_2021-10-14T13:09:51.898/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/archive/EV_2021-10-14T13:48:25.788/mission b/archive/EV_2021-10-14T13:48:25.788/mission new file mode 100644 index 0000000..569cab6 --- /dev/null +++ b/archive/EV_2021-10-14T13:48:25.788/mission @@ -0,0 +1,22 @@ +archive/EV_2021-10-14T13:48:25.788/mission--------------------------- + +Spacecraft: mySat + dry_mass: 2000.0 kg + specific impulse: 3200.0 kg/s + max_thrust: 0.0005 kN + num_thrusters: 2 + duty_cycle: 1.0 +Launch Mass: 4000.0 kg +Launch Date: 2022-03-03T16:03:54.308 +Launch V∞: [3.1331875390553874, 4.743765316753105, -0.6321137349156039] km/s +Phase 1: + Planet: Venus + V∞_in: [0.7336287799525429, 9.092380028023765, -2.060897868194347] km/s + V∞_out: [-0.005397228824250161, -6.841249447820443, 3.86835501811607e-7] km/s + time of flight: 1.431136134384693e7 seconds + arrival date: 2022-08-16T07:26:35.308 + thrust profile: [-0.029700857947171155 0.037677806973394956 -0.0016513225652095235; -0.09203896237700117 0.06668008002755799 -0.003907365708797221; -0.15385799693549973 0.09456424369948617 -0.00567508250690443; -0.19644155536268554 0.12045167230584422 -0.010220562279956805; -0.28443665959408854 0.13387251178059187 -0.010826054663009434; -0.35314485464965406 0.1508209960737375 -0.014312066894957601; -0.42349740669156993 0.15073261096749926 -0.01617441359738227; -0.49179611760767494 0.1313289360663566 -0.019420534802667432; -0.5498265630622056 0.07689683044740066 -0.022535038089659315; -0.5841007485384517 -0.028343225924705343 -0.025645308771199683; -0.6463113947204338 -0.19361054238923944 -0.030545065432850942; -0.7020011201668798 -0.3987157016634757 -0.035892266940698137; -0.660261751730148 -0.564813684339657 -0.03928441369489666; -0.5533792180410886 -0.6697142859509423 -0.039751339872136054; -0.35878759946251465 -0.6287274757834188 -0.03432166295686523; -0.07897641529965045 -0.6890633639101433 -0.024417495241929963; 0.1132061820810732 -0.5814939033233674 -0.011948487492265437; 0.1525591439015402 -0.4915765280189982 -0.0025092936276034316; 0.10348417965356019 -0.4089525878329189 0.0030668463178562854; 0.024035973004629382 -0.3568182136414068 0.0051715969680988395] % + +Mass Used: 225.67816334678992 kg +Launch C3: 32.719741309190596 km²/s² +||V∞_in||: 9.351838631194836 km/s diff --git a/archive/EV_2021-10-14T13:48:25.788/plot.html b/archive/EV_2021-10-14T13:48:25.788/plot.html new file mode 100644 index 0000000..05a3cd7 --- /dev/null +++ b/archive/EV_2021-10-14T13:48:25.788/plot.html @@ -0,0 +1,30 @@ + + + + + + + + + diff --git a/ipopt.out b/ipopt.out new file mode 100644 index 0000000..e69de29 diff --git a/julia/Manifest.toml b/julia/Manifest.toml index 63a9eb8..86b5088 100644 --- a/julia/Manifest.toml +++ b/julia/Manifest.toml @@ -81,6 +81,12 @@ git-tree-sha1 = "56fbc7d843c24bb3a3689e81b064aa730f72db8c" uuid = "07f52509-e9d9-513c-a20d-3b911885bf96" version = "66.1.0+0" +[[CSTParser]] +deps = ["Tokenize"] +git-tree-sha1 = "f9a6389348207faf5e5c62cbc7e89d19688d338a" +uuid = "00ebfdb7-1f24-5e51-bd34-a7502290713f" +version = "3.3.0" + [[ChainRules]] deps = ["ChainRulesCore", "Compat", "LinearAlgebra", "Random", "Statistics"] git-tree-sha1 = "d88340ab502af66cfffc821e70ae72f7dbdce645" @@ -179,10 +185,22 @@ git-tree-sha1 = "a32185f5428d3986f47c2ab78b1f216d5e6cc96f" uuid = "ffbed154-4ef7-542d-bbb7-c09d3a79fcae" version = "0.8.5" +[[DocumentFormat]] +deps = ["CSTParser", "FilePathsBase", "Tokenize"] +git-tree-sha1 = "cf048d65cbcdec70f10745e5801eeb0c6478a7f7" +uuid = "ffa9a821-9c82-50df-894e-fbcef3ed31cd" +version = "3.2.4" + [[Downloads]] deps = ["ArgTools", "LibCURL", "NetworkOptions"] uuid = "f43a241f-c20a-4ad4-852c-f6b1247861c6" +[[FilePathsBase]] +deps = ["Compat", "Dates", "Mmap", "Printf", "Test", "UUIDs"] +git-tree-sha1 = "04d13bfa8ef11720c24e4d840c0033d145537df7" +uuid = "48062228-2e41-5def-b9a4-89aafe57970f" +version = "0.9.17" + [[FileWatching]] uuid = "7b1f6079-737a-58dc-b8bc-7a2ca5c1b5ee" @@ -299,6 +317,12 @@ git-tree-sha1 = "8076680b162ada2a031f707ac7b4953e30667a37" uuid = "682c06a0-de6a-54ab-a142-c8b1cf79cde6" version = "0.21.2" +[[JSONRPC]] +deps = ["JSON", "UUIDs"] +git-tree-sha1 = "1e9a820a29b37864a6738b8fd00eedf3fb8d772e" +uuid = "b9b8584e-8fd3-41f9-ad0c-7255d428e418" +version = "1.3.3" + [[JSONSchema]] deps = ["HTTP", "JSON", "URIs"] git-tree-sha1 = "2f49f7f86762a0fbbeef84912265a1ae61c4ef80" @@ -316,6 +340,12 @@ git-tree-sha1 = "c7f1c695e06c01b95a67f0cd1d34994f3e7db104" uuid = "b964fa9f-0449-5b57-a5c2-d3ea65f4040f" version = "1.2.1" +[[LanguageServer]] +deps = ["CSTParser", "DocumentFormat", "JSON", "JSONRPC", "Markdown", "Pkg", "REPL", "StaticLint", "SymbolServer", "Tokenize", "URIParser", "UUIDs"] +git-tree-sha1 = "126d75fcacc527270a200c397d6ebbd6f826197a" +uuid = "2b0e0bc5-e4fd-59b4-8912-456d1b03d8d7" +version = "4.1.0" + [[Lazy]] deps = ["MacroTools"] git-tree-sha1 = "1370f8202dac30758f3c345f9909b97f53d87d3f" @@ -584,10 +614,22 @@ git-tree-sha1 = "3240808c6d463ac46f1c1cd7638375cd22abbccb" uuid = "90137ffa-7385-5640-81b9-e52037218182" version = "1.2.12" +[[StaticLint]] +deps = ["CSTParser", "Serialization", "SymbolServer"] +git-tree-sha1 = "cb3b96572fa30bf80f281eb4efedca8f29e27bc3" +uuid = "b3cc710f-9c33-5bdb-a03d-a94903873e97" +version = "8.0.1" + [[Statistics]] deps = ["LinearAlgebra", "SparseArrays"] uuid = "10745b16-79ce-11e8-11f9-7d13ad32a3b2" +[[SymbolServer]] +deps = ["InteractiveUtils", "LibGit2", "Markdown", "Pkg", "REPL", "SHA", "Serialization", "Sockets", "UUIDs"] +git-tree-sha1 = "98fba1388841bdea0e412143894df31bab27b969" +uuid = "cf896787-08d5-524d-9de7-132aaa0cb996" +version = "7.1.0" + [[TOML]] deps = ["Dates"] uuid = "fa267f1f-6049-4f14-aa54-33bafae1ed76" @@ -612,6 +654,11 @@ uuid = "a4e569a6-e804-4fa4-b0f3-eef7a1d5b13e" deps = ["InteractiveUtils", "Logging", "Random", "Serialization"] uuid = "8dfed614-e22c-5e08-85e1-65c5234f0b40" +[[Tokenize]] +git-tree-sha1 = "0952c9cee34988092d73a5708780b3917166a0dd" +uuid = "0796e94c-ce3b-5d07-9a54-7f471281c624" +version = "0.5.21" + [[TranscodingStreams]] deps = ["Random", "Test"] git-tree-sha1 = "216b95ea110b5972db65aa90f88d8d89dcb8851c" diff --git a/julia/Project.toml b/julia/Project.toml index 5a3549f..8bfc3ca 100644 --- a/julia/Project.toml +++ b/julia/Project.toml @@ -7,10 +7,12 @@ version = "0.1.0" Dates = "ade2ca70-3891-5945-98fb-dc099432e06a" Distributed = "8ba89e20-285c-5b6f-9357-94700520ee1b" ForwardDiff = "f6369f11-7733-5829-9624-2563aa707210" +LanguageServer = "2b0e0bc5-e4fd-59b4-8912-456d1b03d8d7" LinearAlgebra = "37e2e46d-f89d-539d-b4ee-838fcccc9c8e" PlotlyBase = "a03496cd-edff-5a9b-9e67-9cda94a718b5" PlotlyJS = "f0f68f2c-4968-5e81-91da-67840de0976a" Random = "9a3f8284-a2c9-5f02-9a11-845980a1fd5c" SNOW = "105f6ee8-0889-46b1-9d4b-65e03cbc8f13" SPICE = "5bab7191-041a-5c2e-a744-024b9c3a5062" +SymbolServer = "cf896787-08d5-524d-9de7-132aaa0cb996" Test = "8dfed614-e22c-5e08-85e1-65c5234f0b40" diff --git a/julia/find_neptune.jl b/julia/find_neptune.jl index c27f843..bb86365 100644 --- a/julia/find_neptune.jl +++ b/julia/find_neptune.jl @@ -19,17 +19,16 @@ function easy_cost(m::Union{Mission, Mission_Guess}, C3::Float64, v∞::Float64) norm_mass = (m.start_mass - prop(m)[7]) / m.start_mass norm_C3 = ( m.launch_v∞ ⋅ m.launch_v∞ ) / C3 norm_v∞ = norm(m.phases[end].v∞_in) / v∞ - return norm_mass + norm_C3# + norm_v∞ + return 3norm_mass + norm_C3# + norm_v∞ end -# Using some fairly realistic parameters now sc = Sc("mySat", 200., 3200., 0.00025, 1, 1.0) fuel = 3300. max_c3 = 200. max_v∞ = 500. -voyager_launch = DateTime(1977,9,5) -launch_window = voyager_launch - Year(2), voyager_launch + Year(2) -latest_arrival = voyager_launch + Year(25) +ideal_launch = DateTime(2024,1,1) +launch_window = ideal_launch - Day(365), ideal_launch + Day(365) +latest_arrival = ideal_launch + Year(18) println("Max thrust at full bore: $(fuel/(mfr(sc)*Thesis.year)) years") println("Max mission length: $((latest_arrival - launch_window[1]).value/(1000Thesis.year)) years") @@ -42,7 +41,7 @@ Thesis.mbh(fbs) = mbh(fbs, max_v∞, latest_arrival, easy_cost, - search_patience=20_000, + search_patience=10_000, drill_patience=200, verbose=true) @@ -56,7 +55,7 @@ end log(_::Nothing, _::Vector{Mission}, _::Vector{Body}) = println("No Mission Found...") -planets = [Earth, Jupiter, Saturn, Uranus, Neptune] +planets = [Earth, Venus, Mars, Saturn] best, archive = mbh(planets) log(best, archive, planets) diff --git a/julia/src/Thesis.jl b/julia/src/Thesis.jl index d3b6106..0287548 100644 --- a/julia/src/Thesis.jl +++ b/julia/src/Thesis.jl @@ -1,5 +1,7 @@ module Thesis + homedir = "/home/connor/projects/thesis" + using LinearAlgebra using ForwardDiff using PlotlyJS @@ -11,8 +13,8 @@ module Thesis furnsh("../../spice_files/naif0012.tls") furnsh("../../spice_files/de430.bsp") catch - furnsh("spice_files/naif0012.tls") - furnsh("spice_files/de430.bsp") + furnsh("/home/connor/projects/thesis/spice_files/naif0012.tls") + furnsh("/home/connor/projects/thesis/spice_files/de430.bsp") end include("./types/errors.jl") @@ -25,8 +27,8 @@ module Thesis include("./utilities/conversions.jl") include("./utilities/plotting.jl") include("./nlp_solver.jl") + include("./utilities/lamberts.jl") include("./mbh.jl") include("./genetic_algorithm.jl") - include("./utilities/lamberts.jl") end diff --git a/julia/src/mbh.jl b/julia/src/mbh.jl index cf98ad7..e793bc4 100644 --- a/julia/src/mbh.jl +++ b/julia/src/mbh.jl @@ -47,17 +47,17 @@ end """ Generates a new randomized guess for the mission decision variables """ -function mission_guess( flybys::Vector{Body}, - sc::Sc, - start_mass::Float64, - launch_window::Tuple{DateTime, DateTime}, - max_C3::Float64, - max_v∞_in_mag::Float64, - latest_arrival::DateTime) +function rand_mission_guess( flybys::Vector{Body}, + sc::Sc, + start_mass::Float64, + launch_window::Tuple{DateTime, DateTime}, + max_C3::Float64, + max_v∞_in_mag::Float64, + latest_arrival::DateTime) mission_guess = Bad_Mission("Keep trying to generate a guess") + lambert_guess = Bad_Mission("Keep trying to generate a guess") while mission_guess == Bad_Mission("Keep trying to generate a guess") - # TODO: Eventually I can calculate n more intelligently - n = 40 + n = 20 # Determine the launch conditions launch_date = rand(launch_window...) @@ -76,8 +76,16 @@ function mission_guess( flybys::Vector{Body}, total_tof = sum(tofs) end + times = [ launch_date ] + current_time = launch_date + for tof in tofs + current_time += Second(tof) + push!(times, current_time) + end + # For each phase, determine the v∞_in and δ phases = Vector{Phase}() + lambert_phases = Vector{Phase}() for i in 1:num_phases flyby = flybys[i+1] v∞_in_normalized = rand(-1:0.0001:1, 3) @@ -93,7 +101,12 @@ function mission_guess( flybys::Vector{Body}, periapsis = (flyby.μ/(v∞_in ⋅ v∞_in)) * ( 1/sin(δ/2) - 1 ) end thrusts = rand(-1:0.0001:1,(n,3)) + # Add the phases push!(phases, Phase(flyby, v∞_in, v∞_out, tofs[i], thrusts)) + + # Also add the lambert phases + v∞_out_lambert = lamberts(flybys[i], flyby, times[i], times[i+1])[1] + push!(lambert_phases, Phase(flyby, v∞_in, v∞_out_lambert, tofs[i], zeros(n,3))) end # Finally, determine the arrival v∞ @@ -103,6 +116,7 @@ function mission_guess( flybys::Vector{Body}, # And we can construct a mission guess object with these values try mission_guess = Mission_Guess( sc, start_mass, launch_date, launch_v∞, phases ) + lambert_guess = Mission_Guess( sc, start_mass, launch_date, launch_v∞, lambert_phases ) catch e if isa(e, Mass_Error) ||isa(e,V∞_Error) || isa(e,HitPlanet_Error) continue @@ -110,17 +124,18 @@ function mission_guess( flybys::Vector{Body}, rethrow() end end + end - return mission_guess + return mission_guess, lambert_guess end function record(m::Mission, planets::Vector{Body}) t = Dates.now() abbrev = join([ planet.name[1] for planet in planets ]) - mkdir("archive/$(abbrev)_$(t)") - store(m, "archive/$(abbrev)_$(t)/mission") + mkdir("$(homedir)/archive/$(abbrev)_$(t)") + store(m, "$(homedir)/archive/$(abbrev)_$(t)/mission") p = plot(m, title="$(abbrev) Trajectory") - savefig(p,"archive/$(abbrev)_$(t)/plot.html") + savefig(p,"$(homedir)/archive/$(abbrev)_$(t)/plot.html") end @@ -143,7 +158,7 @@ function mbh( flybys::Vector{Body}, test::Bool=false ) # Convenience Functions - random_guess() = mission_guess(flybys,sc,start_mass,launch_window,max_C3,max_v∞,latest_arrival) + random_guess() = rand_mission_guess(flybys,sc,start_mass,launch_window,max_C3,max_v∞,latest_arrival) cost(m::Union{Mission,Mission_Guess}) = cost_fn(m, max_C3, max_v∞) cost(_::Nothing) = Inf solve(g::Mission_Guess) = solve_mission(g, launch_window, latest_arrival, max_C3, max_v∞) @@ -169,43 +184,68 @@ function mbh( flybys::Vector{Body}, search_count += 1 drill_count = 0 verbose && log() - x_star = solve(random_guess()) - x_star.converged || continue - x_basin = x_star + x_star, x_lambert = solve.(random_guess()) - # If it does, though, we check to see if it's better than the current - if cost(x_star) < cost(x_current) x_current = x_star end - - # Either way, we need to drill into this particular basin, since it's valid - while drill_count < drill_patience - - verbose && log() - - #Perturb to generate a slightly different x_star - x_star = solve(perturb(x_basin)) - - # If better than the best, then keep it as current - if x_star.converged && cost(x_star) < cost(x_current) - x_current = x_star - x_basin = x_star - drill_count = 0 - # If better than the best in this particular basin, keep it as basin - elseif x_star.converged && cost(x_star) < cost(x_basin) - x_basin = x_star - drill_count = 0 - # Otherwise, keep drilling - else - drill_count += 1 + # To improve solution time, we'll try drilling down the lambert's solution first + if x_lambert.converged + x_lambert_best = x_lambert + # If it does converge we check to see if it's better than the current + if cost(x_lambert) < cost(x_current) x_current = x_lambert end + while drill_count < drill_patience + verbose && log() + # If better than the best, then keep it as current + if x_lambert.converged && cost(x_lambert) < cost(x_current) + x_current = x_lambert + x_lambert_best = x_lambert + drill_count = 0 + # If better than the best of lambert trajectories so far, keep it as lambert_best + elseif x_lambert.converged && cost(x_lambert) < cost(x_lambert_best) + x_lambert_best = x_lambert + drill_count = 0 + # Otherwise, keep drilling + else + drill_count += 1 + end + end + drill_count = 0 + if x_current ∉ archive + push!(archive, x_current) + record(x_current, flybys) end end - if x_current ∉ archive - push!(archive, x_current) - record(x_current, flybys) + # Afterwards, we'll try a completely random guess + if x_star.converged + x_basin = x_star + # If it does converge we check to see if it's better than the current + if cost(x_star) < cost(x_current) x_current = x_star end + # Either way, we need to drill into this particular basin, since it's valid + while drill_count < drill_patience + verbose && log() + #Perturb to generate a slightly different x_star + x_star = solve(perturb(x_basin)) + # If better than the best, then keep it as current + if x_star.converged && cost(x_star) < cost(x_current) + x_current = x_star + x_basin = x_star + drill_count = 0 + # If better than the best in this particular basin, keep it as basin + elseif x_star.converged && cost(x_star) < cost(x_basin) + x_basin = x_star + drill_count = 0 + # Otherwise, keep drilling + else + drill_count += 1 + end + end + if x_current ∉ archive + push!(archive, x_current) + record(x_current, flybys) + end end # If in test mode, we don't need to actually optimize. Just grab the first valid basin-best - if test + if test && x_current !== nothing println() return x_current, [ x_current ] end diff --git a/julia/src/nlp_solver.jl b/julia/src/nlp_solver.jl index 99a8cfd..0c869a9 100644 --- a/julia/src/nlp_solver.jl +++ b/julia/src/nlp_solver.jl @@ -123,7 +123,7 @@ function solve_mission( guess::Mission_Guess, "acceptable_constr_viol_tol" => 100tol, "bound_relax_factor" => 0., "max_iter" => 100_000, - "max_cpu_time" => 3. * length(guess.phases), + "max_cpu_time" => 5. * length(guess.phases), "print_level" => print_level) options = Options(solver=IPOPT(ipopt_options), derivatives=ForwardFD()) diff --git a/julia/test/mbh.jl b/julia/test/mbh.jl index 1db9993..2fa268c 100644 --- a/julia/test/mbh.jl +++ b/julia/test/mbh.jl @@ -17,7 +17,7 @@ # Mission Parameters that won't change (they're very lenient) sc, fuel = bepi, 2_000. max_c3, max_v∞ = 100., 20. - launch_window = DateTime(2022,1,1), DateTime(2024,12,25) + launch_window = DateTime(2027,1,1), DateTime(2027,12,25) latest_arrival = DateTime(2034,12,25) # Convenience function for these tests diff --git a/julia/test/missions/mbh_1_phase_archive b/julia/test/missions/mbh_1_phase_archive index ae6544c..d2d8726 100644 --- a/julia/test/missions/mbh_1_phase_archive +++ b/julia/test/missions/mbh_1_phase_archive @@ -7,19 +7,19 @@ Spacecraft: bepi num_thrusters: 2 duty_cycle: 0.9 Launch Mass: 4000.0 kg -Launch Date: 2024-08-10T04:39:14.851 -Launch V∞: [5.086503138635964, 5.7458326772994415, -0.07148502064229807] km/s +Launch Date: 2027-09-12T06:04:50.667 +Launch V∞: [-0.1356894386368732, 5.956064811848478, 0.01939640608336112] km/s Phase 1: Planet: Jupiter - V∞_in: [0.036227390916599315, 0.15967408190094506, 0.14767480118449552] km/s - V∞_out: [0.02010676850789124, 0.050598467400280935, -0.04060341677187609] km/s - time of flight: 2.2119244577042913e8 seconds - arrival date: 2031-08-14T06:59:59.851 - 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] % + V∞_in: [-0.2571115997565001, -0.23716727061524712, 0.1301306668580519] km/s + V∞_out: [-0.014179189011866182, -0.008514489265672389, -0.020254493877991896] km/s + time of flight: 1.8070773341225305e8 seconds + arrival date: 2033-06-03T18:40:23.667 + thrust profile: [-0.28796335426441344 0.2918284262842529 0.004232031537641381; -0.4146826747229724 -0.02204183876659545 0.006463923516828132; -0.3658131284334198 -0.20897490324756807 0.004830213098433344; -0.3009950427607718 -0.29983050286376706 0.0026330364724320627; -0.21226927941652138 -0.31438885498847047 0.00016223993548310865; -0.13803056237326825 -0.31060963133872505 -0.002084476169128304; -0.07968485985716361 -0.29051876651351477 -0.004227991069940268; -0.03393237770799525 -0.2616050729753513 -0.005805065906776818; 0.00010399437044312852 -0.22612386906622065 -0.00723203544008763; 0.02431397619795949 -0.1841020095991609 -0.007967346627807494; 0.03387857848006785 -0.1473548203513266 -0.008904505604898574; 0.0464200796450669 -0.10786650792140276 -0.008591232690818134; 0.05146001248652659 -0.0649385531036076 -0.007930560486331771; 0.05288431148130223 -0.014078912962736419 -0.00441593039414774; 0.0455197215338432 -0.024008992010477768 -0.009803033072905896; 0.05520804599773281 0.0034148633177632287 -0.0036277778862629463; 0.045785853836455455 0.00794833182192021 -0.0217178944298006; 0.04513924118080819 0.05766612276661263 -0.0007249356261771857; 0.0848074300734865 0.06484381201504433 0.010866963214099381; 0.08645863137101507 0.10712102831006817 -0.005895302546374282] % -Mass Used: 1077.835193306381 kg -Launch C3: 58.892217443051806 km²/s² -||V∞_in||: 0.22049055124520436 km/s +Mass Used: 1398.921932467841 kg +Launch C3: 35.493495887266185 km²/s² +||V∞_in||: 0.37321398612237705 km/s diff --git a/julia/test/missions/mbh_1_phase_best b/julia/test/missions/mbh_1_phase_best index 8751fd1..c483b5b 100644 --- a/julia/test/missions/mbh_1_phase_best +++ b/julia/test/missions/mbh_1_phase_best @@ -7,16 +7,16 @@ Spacecraft: bepi num_thrusters: 2 duty_cycle: 0.9 Launch Mass: 4000.0 kg -Launch Date: 2024-08-10T04:39:14.851 -Launch V∞: [5.086503138635964, 5.7458326772994415, -0.07148502064229807] km/s +Launch Date: 2027-09-12T06:04:50.667 +Launch V∞: [-0.1356894386368732, 5.956064811848478, 0.01939640608336112] km/s Phase 1: Planet: Jupiter - V∞_in: [0.036227390916599315, 0.15967408190094506, 0.14767480118449552] km/s - V∞_out: [0.02010676850789124, 0.050598467400280935, -0.04060341677187609] km/s - time of flight: 2.2119244577042913e8 seconds - arrival date: 2031-08-14T06:59:59.851 - 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] % + V∞_in: [-0.2571115997565001, -0.23716727061524712, 0.1301306668580519] km/s + V∞_out: [-0.014179189011866182, -0.008514489265672389, -0.020254493877991896] km/s + time of flight: 1.8070773341225305e8 seconds + arrival date: 2033-06-03T18:40:23.667 + thrust profile: [-0.28796335426441344 0.2918284262842529 0.004232031537641381; -0.4146826747229724 -0.02204183876659545 0.006463923516828132; -0.3658131284334198 -0.20897490324756807 0.004830213098433344; -0.3009950427607718 -0.29983050286376706 0.0026330364724320627; -0.21226927941652138 -0.31438885498847047 0.00016223993548310865; -0.13803056237326825 -0.31060963133872505 -0.002084476169128304; -0.07968485985716361 -0.29051876651351477 -0.004227991069940268; -0.03393237770799525 -0.2616050729753513 -0.005805065906776818; 0.00010399437044312852 -0.22612386906622065 -0.00723203544008763; 0.02431397619795949 -0.1841020095991609 -0.007967346627807494; 0.03387857848006785 -0.1473548203513266 -0.008904505604898574; 0.0464200796450669 -0.10786650792140276 -0.008591232690818134; 0.05146001248652659 -0.0649385531036076 -0.007930560486331771; 0.05288431148130223 -0.014078912962736419 -0.00441593039414774; 0.0455197215338432 -0.024008992010477768 -0.009803033072905896; 0.05520804599773281 0.0034148633177632287 -0.0036277778862629463; 0.045785853836455455 0.00794833182192021 -0.0217178944298006; 0.04513924118080819 0.05766612276661263 -0.0007249356261771857; 0.0848074300734865 0.06484381201504433 0.010866963214099381; 0.08645863137101507 0.10712102831006817 -0.005895302546374282] % -Mass Used: 1077.835193306381 kg -Launch C3: 58.892217443051806 km²/s² -||V∞_in||: 0.22049055124520436 km/s +Mass Used: 1398.921932467841 kg +Launch C3: 35.493495887266185 km²/s² +||V∞_in||: 0.37321398612237705 km/s diff --git a/julia/test/missions/mbh_2_phase_archive b/julia/test/missions/mbh_2_phase_archive index 107354c..67b5c45 100644 --- a/julia/test/missions/mbh_2_phase_archive +++ b/julia/test/missions/mbh_2_phase_archive @@ -7,26 +7,26 @@ Spacecraft: bepi num_thrusters: 2 duty_cycle: 0.9 Launch Mass: 4000.0 kg -Launch Date: 2024-03-01T19:28:21.132 -Launch V∞: [-1.4933474839937355, -1.896757005945588, 0.1342176084154792] km/s +Launch Date: 2027-07-20T13:17:34.631 +Launch V∞: [-2.3530089890058954, 1.806546373465246, -0.8246183971035168] km/s Phase 1: Planet: Mars - 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] % + V∞_in: [-3.557079179490031, 2.2348168420384456, 1.4054671292663363] km/s + V∞_out: [-4.074087303045588, -1.0849670349142753, 1.3593729379381074] km/s + time of flight: 1.0695600026560412e8 seconds + arrival date: 2030-12-09T11:17:34.631 + thrust profile: [-0.0022189023782523748 0.023365002143236557 -0.010993409331132617; 0.2153019288203301 -0.16440845543934793 0.012979033551565024; 0.3639464079118591 0.18422132432552532 0.04272023217963688; 0.11466184077416293 0.3079055688420129 0.008827434981649196; 0.030850502559811713 0.10710583581109685 -0.0392443866311469; 0.12842405226198722 0.13471500586493157 -0.046470788171139685; 0.022178550605493758 0.08362899413062866 0.012804941168562645; 0.12528977866442487 0.07930598418341506 0.05523752701719965; 0.11036663197880708 0.06908833586375046 0.030544670010797404; 0.2621885557666051 0.017745488649470693 -0.043256804103609825; 0.32712194273437595 0.3540199595758462 -0.06793264883835635; -0.12456921081136497 0.30022659769281007 0.011877569185517847; -0.111118550048934 -0.0012849144456734945 0.0618346466936284; 0.0664475480767869 -0.20857672555247925 0.05232162118008461; 0.4674741919141163 -0.27665818135554127 -0.010294403145171388; 0.6235722276862998 0.33893717906065446 -0.08396785235072478; 0.06141376840855648 0.6645340284197009 -0.04540915059549516; -0.4950753135059394 0.4265532645880646 0.04403645965499313; -0.4790065958792388 -0.05470792785400573 0.08950665085522541; -0.31489858710635427 -0.3741453611976776 0.10307557908026614] % Phase 2: Planet: Jupiter - 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] % + V∞_in: [0.38917010093640664, -4.172653280725571, -0.38172849726338637] km/s + V∞_out: [-0.19079117316696953, -0.697272265566823, -3.556895184028567] km/s + time of flight: 9.204480003834815e7 seconds + arrival date: 2033-11-08T19:17:34.631 + thrust profile: [-0.28696988915862254 -0.5466775279353076 0.0161784825048141; -0.05201138624094085 -0.5103548545163037 0.022399691416144073; 0.09258223397854948 -0.42700369632306956 0.02864531312701303; 0.1544195747765251 -0.3175042943871396 0.03319962132309101; 0.16629852231537434 -0.20372710365454566 0.033385847516108444; 0.14766618426707362 -0.10862149045095645 0.026893053884926972; 0.10680433249395786 -0.047590669692367006 0.013917994143247845; 0.05372607652222386 -0.024738666039118885 0.004540404069389168; 0.0454652164291245 -0.03203318353562152 0.003800593821863827; 0.06019445610850742 -0.07020561382583693 -0.0007266034614935319; 0.031747954241254955 -0.05399780408669305 0.0026705429420879126; 0.008868957922568855 -0.0550458335463559 0.003204913050222715; -0.0001325460641792178 -0.0009815769471698307 -0.0004937922234238575; -0.0006857531267272214 -0.007291536557149579 -0.0032616756502396376; -0.002795903533707593 -0.01051173235400901 -0.00025468873326567386; -0.0011701726557658773 0.007181885264360277 0.019496153473968613; -0.00244282675331443 -0.004315368336196475 -0.00303667834001964; -0.005725948352347262 -0.005635872428339283 -0.003961276803316091; -0.017216802798993906 -0.013717525082576966 -0.016160860429875766; -0.026100664086817275 -0.009712024123055465 -0.043657502180151124] % -Mass Used: 1283.6554577493703 kg -Launch C3: 5.845788213962862 km²/s² -||V∞_in||: 2.687082661129041 km/s +Mass Used: 1804.5751392877032 kg +Launch C3: 9.48025660266455 km²/s² +||V∞_in||: 4.208111858569789 km/s diff --git a/julia/test/missions/mbh_2_phase_best b/julia/test/missions/mbh_2_phase_best index 4dc35a3..9bb0c21 100644 --- a/julia/test/missions/mbh_2_phase_best +++ b/julia/test/missions/mbh_2_phase_best @@ -7,23 +7,23 @@ Spacecraft: bepi num_thrusters: 2 duty_cycle: 0.9 Launch Mass: 4000.0 kg -Launch Date: 2024-03-01T19:28:21.132 -Launch V∞: [-1.4933474839937355, -1.896757005945588, 0.1342176084154792] km/s +Launch Date: 2027-07-20T13:17:34.631 +Launch V∞: [-2.3530089890058954, 1.806546373465246, -0.8246183971035168] km/s Phase 1: Planet: Mars - 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] % + V∞_in: [-3.557079179490031, 2.2348168420384456, 1.4054671292663363] km/s + V∞_out: [-4.074087303045588, -1.0849670349142753, 1.3593729379381074] km/s + time of flight: 1.0695600026560412e8 seconds + arrival date: 2030-12-09T11:17:34.631 + thrust profile: [-0.0022189023782523748 0.023365002143236557 -0.010993409331132617; 0.2153019288203301 -0.16440845543934793 0.012979033551565024; 0.3639464079118591 0.18422132432552532 0.04272023217963688; 0.11466184077416293 0.3079055688420129 0.008827434981649196; 0.030850502559811713 0.10710583581109685 -0.0392443866311469; 0.12842405226198722 0.13471500586493157 -0.046470788171139685; 0.022178550605493758 0.08362899413062866 0.012804941168562645; 0.12528977866442487 0.07930598418341506 0.05523752701719965; 0.11036663197880708 0.06908833586375046 0.030544670010797404; 0.2621885557666051 0.017745488649470693 -0.043256804103609825; 0.32712194273437595 0.3540199595758462 -0.06793264883835635; -0.12456921081136497 0.30022659769281007 0.011877569185517847; -0.111118550048934 -0.0012849144456734945 0.0618346466936284; 0.0664475480767869 -0.20857672555247925 0.05232162118008461; 0.4674741919141163 -0.27665818135554127 -0.010294403145171388; 0.6235722276862998 0.33893717906065446 -0.08396785235072478; 0.06141376840855648 0.6645340284197009 -0.04540915059549516; -0.4950753135059394 0.4265532645880646 0.04403645965499313; -0.4790065958792388 -0.05470792785400573 0.08950665085522541; -0.31489858710635427 -0.3741453611976776 0.10307557908026614] % Phase 2: Planet: Jupiter - 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] % + V∞_in: [0.38917010093640664, -4.172653280725571, -0.38172849726338637] km/s + V∞_out: [-0.19079117316696953, -0.697272265566823, -3.556895184028567] km/s + time of flight: 9.204480003834815e7 seconds + arrival date: 2033-11-08T19:17:34.631 + thrust profile: [-0.28696988915862254 -0.5466775279353076 0.0161784825048141; -0.05201138624094085 -0.5103548545163037 0.022399691416144073; 0.09258223397854948 -0.42700369632306956 0.02864531312701303; 0.1544195747765251 -0.3175042943871396 0.03319962132309101; 0.16629852231537434 -0.20372710365454566 0.033385847516108444; 0.14766618426707362 -0.10862149045095645 0.026893053884926972; 0.10680433249395786 -0.047590669692367006 0.013917994143247845; 0.05372607652222386 -0.024738666039118885 0.004540404069389168; 0.0454652164291245 -0.03203318353562152 0.003800593821863827; 0.06019445610850742 -0.07020561382583693 -0.0007266034614935319; 0.031747954241254955 -0.05399780408669305 0.0026705429420879126; 0.008868957922568855 -0.0550458335463559 0.003204913050222715; -0.0001325460641792178 -0.0009815769471698307 -0.0004937922234238575; -0.0006857531267272214 -0.007291536557149579 -0.0032616756502396376; -0.002795903533707593 -0.01051173235400901 -0.00025468873326567386; -0.0011701726557658773 0.007181885264360277 0.019496153473968613; -0.00244282675331443 -0.004315368336196475 -0.00303667834001964; -0.005725948352347262 -0.005635872428339283 -0.003961276803316091; -0.017216802798993906 -0.013717525082576966 -0.016160860429875766; -0.026100664086817275 -0.009712024123055465 -0.043657502180151124] % -Mass Used: 1283.6554577493703 kg -Launch C3: 5.845788213962862 km²/s² -||V∞_in||: 2.687082661129041 km/s +Mass Used: 1804.5751392877032 kg +Launch C3: 9.48025660266455 km²/s² +||V∞_in||: 4.208111858569789 km/s diff --git a/julia/test/missions/mbh_3_phase_archive b/julia/test/missions/mbh_3_phase_archive index 6c1f8da..12fa0ac 100644 --- a/julia/test/missions/mbh_3_phase_archive +++ b/julia/test/missions/mbh_3_phase_archive @@ -7,33 +7,33 @@ Spacecraft: bepi num_thrusters: 2 duty_cycle: 0.9 Launch Mass: 4000.0 kg -Launch Date: 2023-12-30T19:31:02.262 -Launch V∞: [-2.336381310504302, 0.6611197671240502, 0.515368333819228] km/s +Launch Date: 2027-02-01T18:33:11.110 +Launch V∞: [-3.150497013090804, -2.3173169584138944, 0.341495631383101] km/s Phase 1: Planet: Mars - V∞_in: [-0.11272517963886579, -0.16302256252244926, 0.06378439538637051] km/s - V∞_out: [0.002792969304201863, -0.057484436403284406, -0.20003704249209486] km/s - time of flight: 1.2592311667092939e8 seconds - arrival date: 2027-12-27T06:09:38.262 - thrust profile: [-0.07359577344803886 -0.07004965985121933 -0.007807619171823321; 0.043716940115367385 -0.09696906663391322 -0.021035291284121637; 0.15053759331935357 -0.05794230926871806 -0.033866112736962925; 0.20610926006237767 0.0511534113841768 -0.013824814864455921; 0.14247998895987612 0.14895648069233977 0.016465691502639254; 0.033899970899824765 0.1413760732743736 0.033765822767487075; -0.031462663876756475 0.08723970741502689 0.022622665389646173; -0.060921211293504925 -0.026583703906071718 0.0072028126267209116; 0.05521899481152132 -0.05572354743233738 -0.03803266067329364; 0.06591230227849648 -0.0432693147820068 -0.028739472872060776; 0.16269932997793765 -0.016462438801152977 -0.026172416179982023; 0.20013411233717715 0.06074950755811254 0.022311277118381843; 0.14518787703981562 0.12065447079680057 0.05879531725301626; 0.09613845629727286 0.10922616684423382 0.06199408068784226; 0.08625318486313252 0.06478405529977578 0.0023557163450004174; 0.045240171138954385 0.04567139475192793 -0.021769604477046758; 0.04592748677552667 0.060844875114399566 -0.035619737179444874; 0.0804407212683229 -0.03642329187878312 -0.05296002481971273; 0.21331847937323517 0.00896049803861686 -0.05753325446312421; 0.34299417343430333 0.12023007248386997 0.0322957005600654] % + V∞_in: [-0.7086971873088551, -0.10655494257324054, 0.11988806590713104] km/s + V∞_out: [0.2238809651804253, -0.3118676174457644, 0.6168980985050387] km/s + time of flight: 8.953200023401788e7 seconds + arrival date: 2029-12-04T00:33:11.110 + thrust profile: [-0.12186870505136849 0.09462644883825748 -0.05810534392839175; -0.030639242847821345 -0.04245910692035197 -0.0894052455624086; 0.14113718480937812 -0.11440231644835337 -0.08324956933880284; 0.2837902510213314 -0.06260096981677356 -0.0550413035881179; 0.35855908041409906 0.04073648975482989 -0.020180975564470557; 0.3729359388901653 0.15239321939968276 0.016136485697739962; 0.3362801729367708 0.23639200487749643 0.047870876871699004; 0.26251183204522277 0.2735012454673692 0.06987761022138216; 0.17815253145241594 0.2588190065709617 0.07748014522346204; 0.11663205314604401 0.2103183053176405 0.07202476138100809; 0.11053399149833462 0.17008886355865674 0.06219240053201351; 0.16138151083151792 0.16508258430710807 0.0517839189038665; 0.21005359977761767 0.21368458752750677 0.0315693543261013; 0.19623229223435448 0.2814455053854785 0.001570447612348246; 0.12163118057275962 0.3027077944605196 -0.0304471015663471; 0.050711982127557564 0.25718214500209285 -0.05394847268359673; 0.02648153137529395 0.16832831911941415 -0.05881608102540833; 0.04710479095848209 0.08697307038303437 -0.03899890258876461; 0.07958628725681302 0.06854595922468731 -0.009001942082726883; 0.08605410384534219 0.09736430380889433 0.020673442685919103] % Phase 2: Planet: Mars - V∞_in: [-0.014005019530324568, 0.13244612304375988, 0.08290914548187793] km/s - V∞_out: [-0.02364353280263756, 0.15444781952015216, -0.014432031974666977] km/s - time of flight: 1.0032265935562963e7 seconds - arrival date: 2028-04-21T08:54:03.262 - thrust profile: [-0.06468087317083572 0.01713477843818517 0.2072497145223751; -0.06817090268272546 0.022379474456103943 0.19523352237764163; -0.06466190699633262 0.0255932195152017 0.18504680757190148; -0.059342730861904634 0.029426412259887014 0.174021131351099; -0.054114404138384406 0.03235714045889413 0.16225743506965892; -0.04807653805996071 0.036042427078759764 0.1512460952152207; -0.04315764467216101 0.039938588900136185 0.1389467642307416; -0.038786939336882924 0.043008565514191716 0.12722354156375004; -0.03526577678074072 0.04925516219030345 0.11470911008101983; -0.03235044927513134 0.053149635505385665 0.10206946252525144; -0.03014670486994729 0.05684341793213379 0.0896246734207876; -0.028977404396851786 0.0652163530384282 0.07587210971138804; -0.027859643135747448 0.06761679131619418 0.06285226422798801; -0.02857790492958968 0.07811006965735094 0.04913666457443533; -0.02775839545031727 0.07678583628850277 0.035998823265238046; -0.028406280241582614 0.08254699374408436 0.022094948949750847; -0.029302358791746728 0.0852924409615851 0.008263056211369075; -0.030759783119304784 0.0935582591653256 -0.006356164301183838; -0.03225647939083259 0.09688810501349754 -0.020305695435992848; -0.03332559746608383 0.10297737446211802 -0.035147079795216106] % + V∞_in: [-0.86775765928764, 0.239785321439957, -0.2793440299073699] km/s + V∞_out: [-0.728269228104112, 0.22205886592425675, -0.5557724748024003] km/s + time of flight: 1.9774800534204435e7 seconds + arrival date: 2030-07-20T21:33:11.110 + thrust profile: [-0.030570769176673163 0.011978049730521367 -0.1686311146776997; -0.03734362480961287 0.018449018456192904 -0.17005264964682357; -0.04542948419070008 0.025365372398860525 -0.16992835340263743; -0.05521690145245066 0.03285244672122282 -0.16774923049721527; -0.06706930468913055 0.04078685922552811 -0.16334874802709573; -0.08131104167653695 0.04884139923754264 -0.15672575498494773; -0.09819592248044624 0.05655952543787853 -0.1479650657154312; -0.11787873911002066 0.06337920264640957 -0.13717350608484466; -0.14034999306643528 0.06867765983804668 -0.12442413309677075; -0.16539190427907322 0.07179396518491549 -0.10977409185801229; -0.1925589065058879 0.07205624162537454 -0.09328712290120528; -0.22119886531630267 0.06885264399706031 -0.07507799161161761; -0.2505343015720731 0.061677462874266016 -0.05534950074382844; -0.2797189023307287 0.05017836496163492 -0.03436640779599943; -0.3079203344948388 0.03418116061894368 -0.012445205871944063; -0.334368663091996 0.013690266374333697 0.010060492482634029; -0.35838748770071316 -0.011093871325495122 0.03277754892305918; -0.37942569771654455 -0.039796379505630045 0.055325239511752944; -0.3970806444181828 -0.07189338316019264 0.07733706717380652; -0.4112725932874617 -0.10674559801233943 0.098568724917307] % Phase 3: Planet: Jupiter - V∞_in: [-1.5533855349488477, -0.54933117824406, 0.1996303316277416] km/s - V∞_out: [-1.7570559978767255, 1.1363153583675671, -0.43717528976600273] km/s - time of flight: 1.4637789443152088e8 seconds - arrival date: 2032-12-10T13:25:37.262 - thrust profile: [-0.6645141202842072 0.6423371395484379 0.013751042498263796; -0.6671395131717702 -0.09924157003588908 0.004659679865807528; -0.44003790930216125 -0.3664663119690856 0.010688442625863746; -0.18891454451890152 -0.313514318687638 0.015602936100725717; -0.07725712172807717 -0.2160815424379723 0.015975909063353555; -0.024837854243774205 -0.15122812373661867 0.013850214915260109; 0.003917627641656827 -0.1085248645279647 0.010371457271638237; 0.02201996644065442 -0.08454038372778747 0.009321989004990271; 0.03388845898003741 -0.06745670404324332 0.008856982967798533; 0.04309282117740803 -0.053386654501724744 0.008719256737668418; 0.05160359506780744 -0.04166179990240016 0.008149701990869269; 0.05175963695335609 -0.026857606206935496 0.007776339351354358; 0.038796656264694244 -0.008231506041670077 0.005319243332846338; 0.030477068690802474 -0.0005391678971376555 0.002805208510592914; 0.021902353489560968 0.007139818756776372 0.00129759746267181; 0.023229339517858272 0.009106625479845766 -0.0009346891747994962; 0.04577321246719308 -0.011464605937068278 0.004192845438408305; 0.017603006711693223 0.027784064222860144 -0.002885487605696617; 0.05029298986098882 0.03435916705436917 -0.002619919338002586; 0.12026613656214907 0.17439044082372335 -0.003745065383345971] % + V∞_in: [3.096628165859758, -5.54752603323759, 0.16307349334680107] km/s + V∞_out: [-0.10793078996383877, 0.0924800512858945, -0.022459388754450135] km/s + time of flight: 8.654760001509127e7 seconds + arrival date: 2033-04-17T14:33:11.110 + thrust profile: [-0.5212124178884477 -0.24272925296458728 0.016173224831160182; -0.48041901371361273 -0.42824969367860183 0.03503551018937675; -0.35657251411134105 -0.5210283603639988 0.03882674235576436; -0.18159148927663898 -0.5413874907790582 0.03142458257784628; -0.021760680952925514 -0.5187437230839083 0.020044129391221313; 0.08815802808124944 -0.468755585771906 0.008811701650286144; 0.14996577274874454 -0.39950153509190717 -0.0006374540546909846; 0.1756826332108901 -0.31843613205645516 -0.007389149611688129; 0.17606438164463012 -0.23381194273364414 -0.01163475824093298; 0.159181144560096 -0.15334688886711978 -0.013041705195263514; 0.13078599845765138 -0.08380131179134265 -0.011046703931163082; 0.09565122980609836 -0.03262766659535713 -0.006008779003864255; 0.06498733257355833 -0.009875081025971531 -0.0018112250669574325; 0.057070637186324664 -0.005117739296306144 -0.0016028113399474964; 0.06624558635734848 0.0072126749803919175 -0.0040159232988713255; 0.05783875168815469 0.01498693837279799 -0.003335562522287042; 0.04729181899024323 0.02021996828138974 -0.0030204665772785907; 0.057434402651546965 0.035842653333588784 -0.00310080378363583; 0.053208582397478485 0.046380716067435886 -0.0063431045982933485; 0.02806058144310276 0.03766447626177584 -0.005388583041760812] % -Mass Used: 1755.9134038194406 kg -Launch C3: 6.161361494059565 km²/s² -||V∞_in||: 1.6597058874647421 km/s +Mass Used: 1879.386292887199 kg +Launch C3: 15.412208581500444 km²/s² +||V∞_in||: 6.355371275643704 km/s diff --git a/julia/test/missions/mbh_3_phase_best b/julia/test/missions/mbh_3_phase_best index 5807b51..14cd0c6 100644 --- a/julia/test/missions/mbh_3_phase_best +++ b/julia/test/missions/mbh_3_phase_best @@ -7,30 +7,30 @@ Spacecraft: bepi num_thrusters: 2 duty_cycle: 0.9 Launch Mass: 4000.0 kg -Launch Date: 2023-12-30T19:31:02.262 -Launch V∞: [-2.336381310504302, 0.6611197671240502, 0.515368333819228] km/s +Launch Date: 2027-02-01T18:33:11.110 +Launch V∞: [-3.150497013090804, -2.3173169584138944, 0.341495631383101] km/s Phase 1: Planet: Mars - V∞_in: [-0.11272517963886579, -0.16302256252244926, 0.06378439538637051] km/s - V∞_out: [0.002792969304201863, -0.057484436403284406, -0.20003704249209486] km/s - time of flight: 1.2592311667092939e8 seconds - arrival date: 2027-12-27T06:09:38.262 - thrust profile: [-0.07359577344803886 -0.07004965985121933 -0.007807619171823321; 0.043716940115367385 -0.09696906663391322 -0.021035291284121637; 0.15053759331935357 -0.05794230926871806 -0.033866112736962925; 0.20610926006237767 0.0511534113841768 -0.013824814864455921; 0.14247998895987612 0.14895648069233977 0.016465691502639254; 0.033899970899824765 0.1413760732743736 0.033765822767487075; -0.031462663876756475 0.08723970741502689 0.022622665389646173; -0.060921211293504925 -0.026583703906071718 0.0072028126267209116; 0.05521899481152132 -0.05572354743233738 -0.03803266067329364; 0.06591230227849648 -0.0432693147820068 -0.028739472872060776; 0.16269932997793765 -0.016462438801152977 -0.026172416179982023; 0.20013411233717715 0.06074950755811254 0.022311277118381843; 0.14518787703981562 0.12065447079680057 0.05879531725301626; 0.09613845629727286 0.10922616684423382 0.06199408068784226; 0.08625318486313252 0.06478405529977578 0.0023557163450004174; 0.045240171138954385 0.04567139475192793 -0.021769604477046758; 0.04592748677552667 0.060844875114399566 -0.035619737179444874; 0.0804407212683229 -0.03642329187878312 -0.05296002481971273; 0.21331847937323517 0.00896049803861686 -0.05753325446312421; 0.34299417343430333 0.12023007248386997 0.0322957005600654] % + V∞_in: [-0.7086971873088551, -0.10655494257324054, 0.11988806590713104] km/s + V∞_out: [0.2238809651804253, -0.3118676174457644, 0.6168980985050387] km/s + time of flight: 8.953200023401788e7 seconds + arrival date: 2029-12-04T00:33:11.110 + thrust profile: [-0.12186870505136849 0.09462644883825748 -0.05810534392839175; -0.030639242847821345 -0.04245910692035197 -0.0894052455624086; 0.14113718480937812 -0.11440231644835337 -0.08324956933880284; 0.2837902510213314 -0.06260096981677356 -0.0550413035881179; 0.35855908041409906 0.04073648975482989 -0.020180975564470557; 0.3729359388901653 0.15239321939968276 0.016136485697739962; 0.3362801729367708 0.23639200487749643 0.047870876871699004; 0.26251183204522277 0.2735012454673692 0.06987761022138216; 0.17815253145241594 0.2588190065709617 0.07748014522346204; 0.11663205314604401 0.2103183053176405 0.07202476138100809; 0.11053399149833462 0.17008886355865674 0.06219240053201351; 0.16138151083151792 0.16508258430710807 0.0517839189038665; 0.21005359977761767 0.21368458752750677 0.0315693543261013; 0.19623229223435448 0.2814455053854785 0.001570447612348246; 0.12163118057275962 0.3027077944605196 -0.0304471015663471; 0.050711982127557564 0.25718214500209285 -0.05394847268359673; 0.02648153137529395 0.16832831911941415 -0.05881608102540833; 0.04710479095848209 0.08697307038303437 -0.03899890258876461; 0.07958628725681302 0.06854595922468731 -0.009001942082726883; 0.08605410384534219 0.09736430380889433 0.020673442685919103] % Phase 2: Planet: Mars - V∞_in: [-0.014005019530324568, 0.13244612304375988, 0.08290914548187793] km/s - V∞_out: [-0.02364353280263756, 0.15444781952015216, -0.014432031974666977] km/s - time of flight: 1.0032265935562963e7 seconds - arrival date: 2028-04-21T08:54:03.262 - thrust profile: [-0.06468087317083572 0.01713477843818517 0.2072497145223751; -0.06817090268272546 0.022379474456103943 0.19523352237764163; -0.06466190699633262 0.0255932195152017 0.18504680757190148; -0.059342730861904634 0.029426412259887014 0.174021131351099; -0.054114404138384406 0.03235714045889413 0.16225743506965892; -0.04807653805996071 0.036042427078759764 0.1512460952152207; -0.04315764467216101 0.039938588900136185 0.1389467642307416; -0.038786939336882924 0.043008565514191716 0.12722354156375004; -0.03526577678074072 0.04925516219030345 0.11470911008101983; -0.03235044927513134 0.053149635505385665 0.10206946252525144; -0.03014670486994729 0.05684341793213379 0.0896246734207876; -0.028977404396851786 0.0652163530384282 0.07587210971138804; -0.027859643135747448 0.06761679131619418 0.06285226422798801; -0.02857790492958968 0.07811006965735094 0.04913666457443533; -0.02775839545031727 0.07678583628850277 0.035998823265238046; -0.028406280241582614 0.08254699374408436 0.022094948949750847; -0.029302358791746728 0.0852924409615851 0.008263056211369075; -0.030759783119304784 0.0935582591653256 -0.006356164301183838; -0.03225647939083259 0.09688810501349754 -0.020305695435992848; -0.03332559746608383 0.10297737446211802 -0.035147079795216106] % + V∞_in: [-0.86775765928764, 0.239785321439957, -0.2793440299073699] km/s + V∞_out: [-0.728269228104112, 0.22205886592425675, -0.5557724748024003] km/s + time of flight: 1.9774800534204435e7 seconds + arrival date: 2030-07-20T21:33:11.110 + thrust profile: [-0.030570769176673163 0.011978049730521367 -0.1686311146776997; -0.03734362480961287 0.018449018456192904 -0.17005264964682357; -0.04542948419070008 0.025365372398860525 -0.16992835340263743; -0.05521690145245066 0.03285244672122282 -0.16774923049721527; -0.06706930468913055 0.04078685922552811 -0.16334874802709573; -0.08131104167653695 0.04884139923754264 -0.15672575498494773; -0.09819592248044624 0.05655952543787853 -0.1479650657154312; -0.11787873911002066 0.06337920264640957 -0.13717350608484466; -0.14034999306643528 0.06867765983804668 -0.12442413309677075; -0.16539190427907322 0.07179396518491549 -0.10977409185801229; -0.1925589065058879 0.07205624162537454 -0.09328712290120528; -0.22119886531630267 0.06885264399706031 -0.07507799161161761; -0.2505343015720731 0.061677462874266016 -0.05534950074382844; -0.2797189023307287 0.05017836496163492 -0.03436640779599943; -0.3079203344948388 0.03418116061894368 -0.012445205871944063; -0.334368663091996 0.013690266374333697 0.010060492482634029; -0.35838748770071316 -0.011093871325495122 0.03277754892305918; -0.37942569771654455 -0.039796379505630045 0.055325239511752944; -0.3970806444181828 -0.07189338316019264 0.07733706717380652; -0.4112725932874617 -0.10674559801233943 0.098568724917307] % Phase 3: Planet: Jupiter - V∞_in: [-1.5533855349488477, -0.54933117824406, 0.1996303316277416] km/s - V∞_out: [-1.7570559978767255, 1.1363153583675671, -0.43717528976600273] km/s - time of flight: 1.4637789443152088e8 seconds - arrival date: 2032-12-10T13:25:37.262 - thrust profile: [-0.6645141202842072 0.6423371395484379 0.013751042498263796; -0.6671395131717702 -0.09924157003588908 0.004659679865807528; -0.44003790930216125 -0.3664663119690856 0.010688442625863746; -0.18891454451890152 -0.313514318687638 0.015602936100725717; -0.07725712172807717 -0.2160815424379723 0.015975909063353555; -0.024837854243774205 -0.15122812373661867 0.013850214915260109; 0.003917627641656827 -0.1085248645279647 0.010371457271638237; 0.02201996644065442 -0.08454038372778747 0.009321989004990271; 0.03388845898003741 -0.06745670404324332 0.008856982967798533; 0.04309282117740803 -0.053386654501724744 0.008719256737668418; 0.05160359506780744 -0.04166179990240016 0.008149701990869269; 0.05175963695335609 -0.026857606206935496 0.007776339351354358; 0.038796656264694244 -0.008231506041670077 0.005319243332846338; 0.030477068690802474 -0.0005391678971376555 0.002805208510592914; 0.021902353489560968 0.007139818756776372 0.00129759746267181; 0.023229339517858272 0.009106625479845766 -0.0009346891747994962; 0.04577321246719308 -0.011464605937068278 0.004192845438408305; 0.017603006711693223 0.027784064222860144 -0.002885487605696617; 0.05029298986098882 0.03435916705436917 -0.002619919338002586; 0.12026613656214907 0.17439044082372335 -0.003745065383345971] % + V∞_in: [3.096628165859758, -5.54752603323759, 0.16307349334680107] km/s + V∞_out: [-0.10793078996383877, 0.0924800512858945, -0.022459388754450135] km/s + time of flight: 8.654760001509127e7 seconds + arrival date: 2033-04-17T14:33:11.110 + thrust profile: [-0.5212124178884477 -0.24272925296458728 0.016173224831160182; -0.48041901371361273 -0.42824969367860183 0.03503551018937675; -0.35657251411134105 -0.5210283603639988 0.03882674235576436; -0.18159148927663898 -0.5413874907790582 0.03142458257784628; -0.021760680952925514 -0.5187437230839083 0.020044129391221313; 0.08815802808124944 -0.468755585771906 0.008811701650286144; 0.14996577274874454 -0.39950153509190717 -0.0006374540546909846; 0.1756826332108901 -0.31843613205645516 -0.007389149611688129; 0.17606438164463012 -0.23381194273364414 -0.01163475824093298; 0.159181144560096 -0.15334688886711978 -0.013041705195263514; 0.13078599845765138 -0.08380131179134265 -0.011046703931163082; 0.09565122980609836 -0.03262766659535713 -0.006008779003864255; 0.06498733257355833 -0.009875081025971531 -0.0018112250669574325; 0.057070637186324664 -0.005117739296306144 -0.0016028113399474964; 0.06624558635734848 0.0072126749803919175 -0.0040159232988713255; 0.05783875168815469 0.01498693837279799 -0.003335562522287042; 0.04729181899024323 0.02021996828138974 -0.0030204665772785907; 0.057434402651546965 0.035842653333588784 -0.00310080378363583; 0.053208582397478485 0.046380716067435886 -0.0063431045982933485; 0.02806058144310276 0.03766447626177584 -0.005388583041760812] % -Mass Used: 1755.9134038194406 kg -Launch C3: 6.161361494059565 km²/s² -||V∞_in||: 1.6597058874647421 km/s +Mass Used: 1879.386292887199 kg +Launch C3: 15.412208581500444 km²/s² +||V∞_in||: 6.355371275643704 km/s diff --git a/julia/test/missions/nlp_1_phase b/julia/test/missions/nlp_1_phase index 6c71053..89a1e08 100644 --- a/julia/test/missions/nlp_1_phase +++ b/julia/test/missions/nlp_1_phase @@ -7,16 +7,16 @@ Spacecraft: bepi num_thrusters: 2 duty_cycle: 0.9 Launch Mass: 3600.0 kg -Launch Date: 1992-11-12T00:00:00.013 -Launch V∞: [9.695409643750917, 1.230412386785293, 1.5011804102426267] km/s +Launch Date: 1992-11-12T00:00:00.012 +Launch V∞: [9.677342245913248, 1.2148911343904845, 1.4770002664775748] km/s Phase 1: Planet: Venus - V∞_in: [9.994449927209848, -4.805887921122601, -1.7920512221893674] km/s - V∞_out: [4.259960619082596, 0.11640502561369129, -0.5256309278562422] km/s - time of flight: 1.0342080020964487e7 seconds - arrival date: 1993-03-11T16:48:00.013 - thrust profile: [-0.07885937833013125 0.22082346279052664 0.22422618119726967; -0.6387970581030095 0.0823441238202798 0.08742955630508423; -0.8174616778872149 0.032772077981831405 0.048108011372234014; -0.883356063802344 -0.009816430786569194 0.029466362717018645; -0.9090289869704303 -0.06412247350619477 0.01579427507721176; -0.9229025007601358 -0.1348848870891437 0.0038074996913229635; -0.9323419038216932 -0.22247834673542874 -0.007553280139873255; -0.9393524504557308 -0.3233146674906946 -0.018599372537661026; -0.9447442065007597 -0.4307195557715542 -0.02948583920082983; -0.948951862234041 -0.5355674747579858 -0.040180510105645155; -0.9522429476394983 -0.6288580191320197 -0.05048177408167433; -0.9547920892312391 -0.704185334520697 -0.060067918029030234; -0.9567196352746482 -0.7592160354782643 -0.06849167659927999; -0.9581161960060807 -0.79533985266094 -0.0750231011768658; -0.959058595284678 -0.8151694427669934 -0.07867130196153184; -0.959627487063727 -0.8196811744278104 -0.07803378433478286; -0.959931461581211 -0.8044527869739441 -0.07118021416582515; -0.9601423578460804 -0.7501732041729071 -0.05552220537456991; -0.9605351740691301 -0.596546633077274 -0.027695673262336473; -0.9614858974879196 -0.22563892811165903 0.016331234996720147] % + V∞_in: [9.995477533479665, -4.770529222466886, -1.7643262560938888] km/s + V∞_out: [4.542216161608705, 0.1169383121147722, -0.5297547896681116] km/s + time of flight: 1.0342080018919956e7 seconds + arrival date: 1993-03-11T16:48:00.012 + thrust profile: [-0.06827956587597055 0.2189651579368032 0.22260889586646854; -0.5657492453559373 0.08687547481531692 0.09138393271069822; -0.7627133026838161 0.04522025084077273 0.06051223750173192; -0.8694853207917537 0.004020122983347096 0.04412034762690886; -0.9156699467684505 -0.05071240769308274 0.03110069387793629; -0.9307669202914396 -0.1219964600790567 0.01923669861767808; -0.9342334366509295 -0.20780403813377482 0.0078030080771221266; -0.9355559722321648 -0.30276368006072857 -0.0035345858246075956; -0.938210990244296 -0.39973779814825156 -0.014841057433864407; -0.9428326748546626 -0.4922801244635121 -0.025964447511107023; -0.948952802856955 -0.5759010541594941 -0.036681448092579935; -0.9557798460559065 -0.6474598520145747 -0.04675072941621921; -0.962549888811903 -0.7047205371292298 -0.055638699294433915; -0.9686622563853547 -0.7463664783144444 -0.0625857936749166; -0.9737612697271567 -0.7715231321565172 -0.06659149605871661; -0.9777967996020939 -0.7783020776379241 -0.06623218175189496; -0.9810653384331429 -0.7604447108250885 -0.0594729767608653; -0.9842857104464896 -0.7004371830045492 -0.04358728653836779; -0.9887220681198762 -0.5548364920968362 -0.01489473159954481; -0.9966878745813371 -0.2184651547964285 0.03090315333337913] % -Mass Used: 386.3550491309211 kg -Launch C3: 97.76842542578919 km²/s² -||V∞_in||: 11.233745396832147 km/s +Mass Used: 380.34886252983915 kg +Launch C3: 97.30844320013269 km²/s² +||V∞_in||: 11.215184676261444 km/s diff --git a/julia/test/missions/nlp_2_phase b/julia/test/missions/nlp_2_phase index 10f01ae..86788f8 100644 --- a/julia/test/missions/nlp_2_phase +++ b/julia/test/missions/nlp_2_phase @@ -7,23 +7,23 @@ Spacecraft: bepi num_thrusters: 2 duty_cycle: 0.9 Launch Mass: 3600.0 kg -Launch Date: 2021-10-31T23:59:59.740 -Launch V∞: [1.0519139174671255, -2.532396776578504, -2.3181056242189095] km/s +Launch Date: 2021-10-31T23:59:59.769 +Launch V∞: [1.0462564431708832, -2.520754077506101, -2.301043507881933] km/s Phase 1: Planet: Venus - V∞_in: [0.4221053576448278, -3.5275571377673485, 4.891092995284791] km/s - V∞_out: [2.663171797047433, -4.912541295851552, 2.3063442275330837] km/s - time of flight: 1.2614399648580924e7 seconds - arrival date: 2022-03-26T23:59:58.740 - thrust profile: [0.07998955511503905 0.014645901175208607 0.032059542365265536; 0.061271963308267355 0.010496084457312739 0.06456227213436845; 0.03653858968490382 0.004095269984271039 0.08778809213169904; 0.012597606226571892 -0.0035843497513941024 0.10156429358711754; -0.007823696996985706 -0.012212563689391798 0.1092387978999297; -0.024470397395360978 -0.022164965343914263 0.11328387576041525; -0.03764018531138568 -0.03305106575614711 0.11485841832796724; -0.046956531921797474 -0.04462741732738438 0.1147527426828988; -0.052986295209290435 -0.056908842131396964 0.11331606017641183; -0.05501214840088177 -0.0698229298399496 0.11102391517980509; -0.0539274775951607 -0.08225923304281293 0.1080571865577752; -0.04900248855811753 -0.09498380663479362 0.10399629481809765; -0.040344197913873656 -0.10681215838405833 0.09912867572917736; -0.028118935327375093 -0.11715254048024237 0.09312311669260512; -0.012343877715426374 -0.12544654901191046 0.08544366039001013; 0.006110502843051679 -0.1305027433772816 0.07629177701281903; 0.026362754169644998 -0.13201279652190237 0.06480681138449274; 0.046333885834596335 -0.129332099528906 0.05156965147459962; 0.06457348912678001 -0.12274635759961078 0.036509818421423236; 0.07952353937438418 -0.11313097843352427 0.019798449229470383] % + V∞_in: [0.4205842845952983, -3.5241183574614556, 4.879873784266574] km/s + V∞_out: [2.657685712690303, -4.920354075306563, 2.266369032728228] km/s + time of flight: 1.2614399691127092e7 seconds + arrival date: 2022-03-26T23:59:58.769 + thrust profile: [0.08791530712557315 -0.009101317973001748 0.010254083007822207; 0.07287521745776969 -0.011381949725375708 0.051332448819202944; 0.04543116258472458 -0.01531732267940295 0.08273458014460809; 0.011034188560216448 -0.020310595889307323 0.10100599446320643; -0.009607377273254756 -0.02382633371411493 0.1081982710061048; -0.028510355701058584 -0.030611944159923403 0.11101434996597628; -0.039048295910837236 -0.03820244320795566 0.11279184708362161; -0.048252651406879885 -0.04651039104792323 0.11301481830933677; -0.05288674350674192 -0.0561882917884983 0.11293454239992265; -0.05458628096513579 -0.06643801004024381 0.11223764822140121; -0.053564283975236535 -0.07751051107973227 0.11061646758637526; -0.049500823222769094 -0.0891415249668692 0.10769319474620971; -0.04185476746663511 -0.10066361474827486 0.10355236756997019; -0.03087924291992901 -0.1112479139000727 0.09781871133696314; -0.015564164113106642 -0.11996802006040436 0.09064682025194883; 0.001781758545597473 -0.12613079909578606 0.0809801955196938; 0.021345925406049154 -0.12876486287710442 0.06930029766487243; 0.041502826765638504 -0.12763804654948588 0.054677487677216745; 0.06024411885991524 -0.12236183464053872 0.038231302757203295; 0.07560839256024353 -0.114157581119008 0.018886579096999003] % Phase 2: Planet: Mars - V∞_in: [3.880922081076609, -3.8756380279560982, -1.179545632109947] km/s - V∞_out: [-0.006991844594378784, 0.007675557473077985, 0.0017824029323501372] km/s - time of flight: 1.330560006563769e7 seconds - arrival date: 2022-08-27T23:59:58.740 - thrust profile: [0.12305856757522188 -0.14464704712095547 -0.01690236351704525; 0.13429815673794188 -0.1195285218500703 -0.023483980378131736; 0.1396586011579744 -0.09516174490601491 -0.0293944316107087; 0.1405117586368446 -0.07304441529598331 -0.03420656443020225; 0.13837132835970684 -0.05371429903466249 -0.03776391678703145; 0.13446436956407476 -0.03753581708426115 -0.04027955684165351; 0.12971675491549636 -0.02368494568417238 -0.041313837916754456; 0.12476791885955194 -0.011918609837526017 -0.04089459243732129; 0.11990410375769957 -0.0013599111496390207 -0.039013892415853124; 0.11535184137947554 0.008625420550911504 -0.03547549318320644; 0.11060362891923352 0.01858862039347281 -0.03026382720393468; 0.1051121620536058 0.02900798484914558 -0.02356021862070372; 0.09847113469008412 0.040066844453614206 -0.014965931800162527; 0.08971089782921067 0.051422184661349964 -0.005111452945431483; 0.07802582953613077 0.06259376060544532 0.0051850295654957725; 0.06311411546227669 0.07276616262027279 0.015795273832386957; 0.04546470094052957 0.08070053397671015 0.025466309765173768; 0.026472095432748317 0.08567894187220633 0.03355591354621125; 0.006854607387209108 0.08788158299954184 0.03976962429050834; -0.011956529938837489 0.08738091721577941 0.04450602440724739] % + V∞_in: [3.866657617879469, -3.8561104436565112, -1.1528388074396114] km/s + V∞_out: [-0.04156826938628659, 0.04537147320396694, 0.010962101613372877] km/s + time of flight: 1.3305600070108933e7 seconds + arrival date: 2022-08-27T23:59:58.769 + thrust profile: [0.12294683695617006 -0.14210501591303906 -0.015953927996763824; 0.1346036754636979 -0.11703322342276389 -0.02118233265872474; 0.14035562458965456 -0.09253436643679969 -0.026037109750586127; 0.14159974389839877 -0.07034252588185486 -0.02965559917950358; 0.13983758574258884 -0.0508280123903436 -0.03226072974284784; 0.13628355001371623 -0.03381714643542805 -0.033706183284138075; 0.13174907912062978 -0.01944710462973476 -0.03378159713957984; 0.12690191547644916 -0.006666552590772735 -0.032314321099804075; 0.12190989012800546 0.005350412631176013 -0.02896415432946389; 0.11640547480173373 0.01766009561198736 -0.024295908236754368; 0.11004779022898785 0.029624240108957346 -0.018629744776725948; 0.10255142565747595 0.041391197147168296 -0.011260773047897207; 0.09257939116538691 0.054055648527399226 -0.0018819573006649628; 0.07862129598678515 0.06762185940978795 0.006827208192964654; 0.06184044671572194 0.07873199678299247 0.015671300335402687; 0.04256729407158805 0.08711502955932304 0.023547740065060118; 0.022644089962366266 0.0922573542104121 0.029300773045221138; 0.0012772594401787602 0.09453861142625342 0.0335188440659034; -0.017213511457067864 0.09403439603239908 0.036105272081528195; -0.03466637624188391 0.0910940423628138 0.03867124120601387] % -Mass Used: 121.82108539595492 kg -Launch C3: 12.893170008821572 km²/s² -||V∞_in||: 5.6101206957923 km/s +Mass Used: 121.86921799846004 kg +Launch C3: 12.743654889305812 km²/s² +||V∞_in||: 5.58118860132149 km/s diff --git a/julia/test/nlp_solver.jl b/julia/test/nlp_solver.jl index 46f570e..a6f78ad 100644 --- a/julia/test/nlp_solver.jl +++ b/julia/test/nlp_solver.jl @@ -16,7 +16,7 @@ # We can get the thrust profile and tof pretty wrong and still be ok phase = Phase(Venus, 1.1v∞_in, v∞_in, 0.9*tof, 0.1*ones(20,3)) guess = Mission_Guess(bepi, 3_600., test_leave, 0.9*v∞_out, [phase]) - m = solve_mission(guess, launch_window, latest_arrival, verbose=true) + m = solve_mission(guess, launch_window, latest_arrival, 200., 20., verbose=true) @test typeof(m) == Mission # Now we can plot the results to check visually @@ -39,7 +39,7 @@ v∞_out, v∞_in, tof = Thesis.lamberts(flybys[end-1], flybys[end], dates[end-1], dates[end]) push!(phases, Phase(flybys[end], v∞_in, v∞_in, tof, 0.01*ones(20,3))) guess = Mission_Guess(bepi, 3_600., dates[1], launch_v∞, phases) - m = solve_mission(guess, launch_window, latest_arrival, verbose=true) + m = solve_mission(guess, launch_window, latest_arrival, 200., 20., verbose=true) @test typeof(m) == Mission p = plot(m, title="NLP Test Solution (2 Phases)") savefig(p,"../plots/nlp_test_2_phase.html") @@ -66,7 +66,7 @@ # v∞_out, v∞_in, tof = Thesis.lamberts(flybys[end-1], flybys[end], dates[end-1], dates[end]) # push!(phases, Phase(flybys[end], v∞_in, v∞_in, tof, 0.01*ones(20,3))) # guess = Mission_Guess(bepi, 3_600., dates[1], launch_v∞, phases) - # m = solve_mission(guess, launch_window, latest_arrival, verbose=true) + # m = solve_mission(guess, launch_window, latest_arrival, 200., 20., verbose=true) # @test typeof(m) == Mission # p = plot(m, title="NLP Test Solution (5 Phases)") # savefig(p,"../plots/nlp_test_5_phase.html") diff --git a/test.html b/test.html new file mode 100644 index 0000000..d860ff1 --- /dev/null +++ b/test.html @@ -0,0 +1,30 @@ + + + + + + + + +