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Created with Raphaël 2.2.09Jul5329Jun24222016151430May2928526Apr24212019181126Mar2417163122Feb2029Dec2827231811229Nov2614329Oct232221186Aug5125Jul211131May302928252316141110765432130Apr292827262423222120191716151312108654331Mar30292827232019161312111096543229Feb2725232018171610Dec[unique-event-function] Introduce initial version of combined event function (apogee, landing)[alpha-phi][bugfix] Fixed a bug where ballistic would crash when no wind was input[fins-trim] Updated trimmed fins and updated coefficientsedit README.mdedit README.mdedit README.md[updates] Converted motor pressure to Pa[alpha-phi] created new coefficient's matrices and removed a comment[alpha-phi] fixed a bug where n would in the wrong range (in Coefficient's class) and Handle AoA matrix usage in alphaTotPhi cases (in ballistic)[alpha-phi] Updated aerodynamic matrices[alpha-phi][Rocket] Added option to not load highAOA matrices[alpha-phi][Coefficient] Implemented coefficient transport[alpha-phi] Improved checks[alpha-phi] Implementing coefficient type enum and symmetry flag[alpha-phi] Moved enums to dedicated folder[static-fire] Added SFT7 and SFT8 motors and updated coefficients[preliminary-sims] Updated RCS bay length[preliminary-sims][motor] Added modified SFT3 motors[coefficients-cvs] Edit coefficientToCvs.mCoefficientCsvCoefficientCsv[ode-tests] Added time's vector flagode-testsode-tests[weather-forecast-analysis] added stand position in the euroc geoplot[prp-integration] modified chamber pressure if statements[prp-integration] Fixed Gemini and Lyra rocket instancesAggiunto file coefficientToCsv[weather-forecast-analysis] Introduced a weather station in "euroc" case and made other related changes[weather-forecast-analysis] Fixed "gaussianDistribution" function[coefficients-fixes] Modified motor and added[coefficients-fixes] Added aerodynamic matrices[coefficients-fixes] Added cl_alpha to parachute[coefficients-fixes] Fixed stagesInertia used[coefficients-fixes] Added arm also to parafoil[coefficient-fixes] Fixed loadMass calculation[coefficient-fixes] modified momentumArm calculation[coefficients-fixes] Added momentum arm as Para property, moved paraToStruct function to miscellanous[to-struct-updates] Improved overload for toStruct methods[to-struct-updates] Added ovverloads for toStruct in Airbrakes and Wind[to-struct-updates] Removed ParaLoader[to-struct-updates] Implemented type conversion for unsupported simulink types[to-struct-conversion] Fixed a bugwhere toStruct would not work with object array fields[to-struct-updates] Made Para Strucutred