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  • CoefficientCsv
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Created with Raphaël 2.2.09Aug65429Jul161095329Jun24222016151430May2928526Apr24212019181126Mar2417163122Feb2029Dec2827231811229Nov2614329Oct232221186Aug5125Jul211131May302928252316141110765432130Apr292827262423222120191716151312108654331Mar30292827232019161312111096543229Feb2725232018171610Dec[montecarlo-config] Added stochastic configmontecarlo-configmontecarlo-config[montecarlo-config] Moved stochParameters from MSA-toolkit[updates] Added SFT11 Motor and updated configmainmain[updates] Added SFT10 motor[updates] Changed rear mass to 1.3kg[updates] Changed parafoil mass to 3.9kg[fixes] Fixed wrong data in environmentConfig Roccaraso[fixes] Made configs runnable up to gemini[fixes] Updated Roccaraso configuration to match EuRoC[usabillity-improvements] Changed other classes from CONSTANT_CASE to camelCase_usability-impro…usability-improvements[usability-improvements] Converted rocket properties from CONSTANT_CASE to camelCase_[usability-improvements] Adding effective ramp calculation to ode[usability-improvements] Updated environment configs[usability-improvements] Moved pinsDistance from Environment to Rocket[prp-integration] Working saveData[prp-integration] Working fromEngineDatasolved issuesFixed variable names, applied code changes, translatedApply 1 suggestion(s) to 1 file(s)Edit Motor Added fromEngineData and saveData methods to Motor class[prp-integration] modified chamber pressure if statements[wind-forecast-fixes] Renamed print to prints to prevent shadowing[unique-event-function] Add help sectionsunique-event-fu…unique-event-function[unique-event-function] Create two separate event functions: eventBallistic and eventParachute[unique-event-function] Add launchpad exit event[unique-event-function] Add cutoff event[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