diff --git a/l10n/messages_de.properties b/l10n/messages_de.properties index 055f0518f..50d4c4081 100644 --- a/l10n/messages_de.properties +++ b/l10n/messages_de.properties @@ -1,3 +1,4 @@ + # # German base translation file # @@ -5,6 +6,12 @@ # # className.ComponantType.componantName # +# +# Text tokens within braces should not be translated, e.g. +# "The file '{filename}' exists." +# They are pieces that are inserted dynamically. +# + ! Set to the name of the current translation file (used for debugging purposes) debug.currentFile = messages_de.properties @@ -53,14 +60,6 @@ BasicFrame.SimpleFileFilter3 = RockSim Designs (*.rkt) BasicFrame.tab.Rocketdesign = Raketendesign BasicFrame.tab.Flightsim = Flugsimulation BasicFrame.title.Addnewcomp = Neue Komponente hinzufügen -BasicFrame.item.Openrocketdesign = Raketendesign öffnen -BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen -BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern -BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern -BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken -BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen -BasicFrame.item.Quitprogram = Programm beenden -BasicFrame.menu.Rocketedt = Rakete bearbeiten BasicFrame.dlg.lbl1 = Design ' BasicFrame.dlg.lbl2 = ' ist nicht gespeichert. BasicFrame.dlg.lbl3 = Möchten Sie es speichern? @@ -70,6 +69,15 @@ BasicFrame.WarningDialog.txt1 = Die folgenden Probleme w BasicFrame.WarningDialog.txt2 = Einige Designeigenschaften wurde eventuell nicht korrekt geladen. BasicFrame.WarningDialog.title = Warnungen während des Öffnens der Datei + +! General error messages used in multiple contexts +error.fileExists.title = File exists +error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it? + +error.writing.title = Error writing file +error.writing.desc = An error occurred while writing to the file: + + ! Labels used in buttons of dialog windows button.ok = OK button.cancel = Abbrechen @@ -110,6 +118,7 @@ PrintDialog.error.preview.title = Vorschau kann nicht ge PrintDialog.error.preview.desc1 = PDF-Vorschau kann nicht geöffnet werden PrintDialog.error.preview.desc2 = Bitte "Als PDF speichern" benutzen. + !PrintSettingsDialog PrintSettingsDialog.title = Print settings PrintSettingsDialog.lbl.Templatefillcolor = Template fill color: @@ -135,6 +144,8 @@ bugreport.dlg.failedmsg2 = Bitte senden Sie den Bericht manuell an bugreport.dlg.failedmsg3 = Fehler beim Versenden des Berichts bugreport.reportDialog.txt = Sie können eine Fehler in OpenRocket mitteilen, indem Sie das unten stehende Formular ausfüllen und abschicken.
Sie können Fehler mit angehängten Dateien auch auf der Projekt-Website mitteilen. bugreport.reportDialog.txt2 = Bitte beschreiben Sie kurz, was Sie getan haben, als der Fehler auftrat. +bugreport.dlg.provideDescription = Please provide a description of the bug first. +bugreport.dlg.provideDescription.title = Bug description missing ! Debug log dialog @@ -239,7 +250,8 @@ pref.dlg.lbl.Totalimpulse = Gesamtimpuls: pref.dlg.lbl.Temperature = Temperatur: pref.dlg.lbl.Momentofinertia = Trägheitsmoment: pref.dlg.lbl.Pressure = Druck: -pref.dlg.lbl.Stability = Stabilität +pref.dlg.lbl.Stability = Stabilität: +pref.dlg.lbl.FlightTime = Flight time: pref.dlg.lbl.effect1 = Die Änderungen werden wirksam, wenn Sie das nächste Mal ein Fenster öffnen. pref.dlg.lbl.Checkingupdates = Prüfe, ob Aktualisierungen verfügbar sind... pref.dlg.lbl.msg1 = Ein Fehler trat bei der Kommunikation mit dem Server auf. @@ -248,12 +260,15 @@ pref.dlg.lbl.msg3 = Sie benutzen die neueste Version von OpenRocket. pref.dlg.lbl.msg4 = Keine Aktualisierungen verfügbar. pref.dlg.PrefChoiseSelector1 = Immer fragen pref.dlg.PrefChoiseSelector2 = in der Mitte einfügen -a = an das Ende anhängen +pref.dlg.PrefChoiseSelector3 = an das Ende anhängen pref.dlg.PrefBooleanSelector1 = Löschen pref.dlg.PrefBooleanSelector2 = Bestätigen pref.dlg.Add = Hinzufügen pref.dlg.DescriptionArea.Adddirectories = Um eigene Schubkurven zu laden, Verzeichnisse, RASP-Motordateien (*.eng), RockSim-Motordateien (*.rse) oder ZIP-Archive mit Semikolon getrennt eingeben. Änderungen werden beim nächsten Neustart von OpenRocket übernommen. +PreferencesDialog.lbl.language = Interface language: +PreferencesDialog.languages.default = System default +PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket. ! Simulation edit dialog simedtdlg.but.runsimulation = Simulation starten @@ -290,6 +305,10 @@ simedtdlg.lbl.ttip.Pressure = Der Luftdruck am Startplatz. simedtdlg.lbl.Launchsite = Startplatz simedtdlg.lbl.Latitude = Breitengrad: simedtdlg.lbl.ttip.Latitude = Der Breitengrad des Startplatzes beeinflusst die wirksame Gravitationskraft.
Positive Werte liegen auf der Nordhalbkugel, negative Werte auf der Südhalbkugel. + +simedtdlg.lbl.Longitude = Longitude: +simedtdlg.lbl.ttip.Longitude = Required for weather prediction and elevation models. + simedtdlg.lbl.Altitude = Höhe: simedtdlg.lbl.ttip.Altitude = Die Höhe des Startplatzes über Meeresniveau.
Die Höhe des Startplatzes beeinflusst die Position der Rakete im atmosphärischen Modell. simedtdlg.border.Launchrod = Startrampe @@ -308,6 +327,8 @@ simedtdlg.lbl.ExtBarrowman = Barrowman (erweitert) simedtdlg.lbl.Simmethod = Simulationsmethode: simedtdlg.lbl.ttip.Simmethod1 = Der Sechs-Freiheitsgradsimulator erlaubt der Rakete völlige Bewegungsfreiheit während des Fluges.
simedtdlg.lbl.ttip.Simmethod2 = Das Integrieren wird nach dem numerischen Runge-Kutta-Verfahren 4. Ordnung durchgeführt. +simedtdlg.lbl.GeodeticMethod = Geodetic calculations: +simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations. simedtdlg.lbl.Timestep = Zeitschritt: simedtdlg.lbl.ttip.Timestep1 = Die Zeit zwischen den Simulationsschritten.
Kleinere Schritte ergeben genauere Ergebnisse, die Simulationen dauern aber länger.
simedtdlg.lbl.ttip.Timestep2 = Die Berechnung der Simulation mit dem Verfahren 4. Ordnung liefert gute Ergebnisse mit Zeitschritten von @@ -329,6 +350,14 @@ simedtdlg.IntensityDesc.High = Hoch simedtdlg.IntensityDesc.Veryhigh = Sehr hoch simedtdlg.IntensityDesc.Extreme = Extrem +GeodeticComputationStrategy.none.name = None +GeodeticComputationStrategy.none.desc = Perform no geodetic computations. +GeodeticComputationStrategy.spherical.name = Spherical approximation +GeodeticComputationStrategy.spherical.desc = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. +GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid +GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
Slower and unnecessary in most cases. + + ! Simulation Panel @@ -400,6 +429,12 @@ SimExpPan.ExportingVar.desc3 = Variablen aus SimExpPan.Col.Variable = Variable SimExpPan.Col.Unit = Einheit + +CsvOptionPanel.separator.space = SPACE +CsvOptionPanel.separator.tab = TAB + + + ! MotorPlot MotorPlot.title.Motorplot = Motorkurve MotorPlot.but.Select = Auswahl @@ -493,6 +528,7 @@ componentanalysisdlg.println.settingnam = SETTING NAN VALUES componentanalysisdlg.lbl.reflenght = Referenzlänge: componentanalysisdlg.lbl.refarea = Referenzfläche: !componentanalysisdlg.But.close =Close +componentanalysisdlg.TabStability.Col.Component = Component ! Custom Material dialog custmatdlg.title.Custommaterial = Benutzerdefiniertes Material @@ -623,6 +659,7 @@ CenteringRingCfg.tab.Generalproperties = Allgemeine Eigenschaften !ComponentConfigDialog ComponentCfgDlg.configuration = Konfiguration +ComponentCfgDlg.configuration1 = ComponentCfgDlg.Modify = Verändern !EllipticalFinSetConfig @@ -652,10 +689,12 @@ FreeformFinSetCfg.lbl.Posrelativeto = Position relativ zu: FreeformFinSetCfg.lbl.plus = plus FreeformFinSetCfg.lbl.FincrossSection = Querschnitt: FreeformFinSetCfg.lbl.Thickness = Wandstärke: -FreeformFinSetCfg.lbl.Double-click = Double-click -FreeformFinSetCfg.lbl.toedit = to edit -FreeformFinSetCfg.lbl.Clickdrag = Click+drag: Add and move points -FreeformFinSetCfg.lbl.Ctrlclick = Ctrl+click: Remove point +! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle +FreeformFinSetConfig.lbl.doubleClick1 = Double-click +FreeformFinSetConfig.lbl.doubleClick2 = to edit +FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points +FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point + !InnerTubeConfig InnerTubeCfg.tab.Motor = Motor @@ -905,33 +944,59 @@ PlotDialog.lbl.Chart = Klicken+ziehen: runter+rechts um hinein zu zoomen, hoch+l ! "main" prefix is used for the main application dialog +# FIXME: Rename the description keys + main.menu.file = Datei +main.menu.file.desc = File-handling related tasks main.menu.file.new = Neu +main.menu.file.new.desc = Create a new rocket design main.menu.file.open = Öffnen.. +BasicFrame.item.Openrocketdesign = Raketendesign öffnen main.menu.file.openExample = Beispiel öffnen.. +BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen main.menu.file.save = Speichern +BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern main.menu.file.saveAs = Speichern unter... +BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern main.menu.file.print = Drucken / als PDF exportieren... +BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken main.menu.file.close = Schließen +BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen main.menu.file.quit = Beenden +BasicFrame.item.Quitprogram = Programm beenden main.menu.edit = Bearbeiten +BasicFrame.menu.Rocketedt = Rakete bearbeiten main.menu.edit.undo = Rückgängig +main.menu.edit.undo.desc = Undo the previous operation main.menu.edit.redo = Wiederholen +main.menu.edit.redo.desc = Redo the previously undone operation main.menu.edit.cut = Ausschneiden main.menu.edit.copy = Kopieren main.menu.edit.paste = Einfügen main.menu.edit.delete = Löschen +main.menu.edit.resize = Scale... +main.menu.edit.resize.desc = Scale parts of the rocket design main.menu.edit.preferences = Einstellungen +main.menu.edit.preferences.desc = Setup the application preferences main.menu.analyze = Analysieren +main.menu.analyze.desc = Rocket analysis main.menu.analyze.componentAnalysis = Komponente analysieren +main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately +main.menu.analyze.optimization = Rocket optimization +main.menu.analyze.optimization.desc = General rocket design optimization main.menu.help = Hilfe +main.menu.help.desc = Information about OpenRocket main.menu.help.license = Lizenz +main.menu.help.license.desc = OpenRocket license information main.menu.help.bugReport = Fehlerbericht +main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket main.menu.help.debugLog = Debug-Log +main.menu.help.debugLog.desc = View the OpenRocket debug log main.menu.help.about = Über +main.menu.help.about.desc = Copyright details about OpenRocket main.menu.debug = Debug main.menu.debug.whatisthismenu = Was macht diese Menü? @@ -963,6 +1028,7 @@ Databases.materials.Spruce = Fichte Databases.materials.StyrofoamgenericEPS = Styropor (EPS) Databases.materials.StyrofoamBluefoamXPS = Styrodur (XPS) Databases.materials.Quantumtubing = Quantum tubing +Databases.materials.BlueTube = Blue tube !SURFACE_MATERIAL Databases.materials.Ripstopnylon = Ripstop Nylon Databases.materials.Mylar = Mylar @@ -1193,6 +1259,9 @@ FlightDataType.TYPE_AIR_PRESSURE = Luftdruck FlightDataType.TYPE_SPEED_OF_SOUND = Schallgeschwindigkeit FlightDataType.TYPE_TIME_STEP = Simulationsintervall FlightDataType.TYPE_COMPUTATION_TIME = Berechnnungszeit +FlightDataType.TYPE_LATITUDE = Latitude +FlightDataType.TYPE_LONGITUDE = Longitude +FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration ! PlotConfiguration PlotConfiguration.Verticalmotion = Vertikale Bewegung über Zeit @@ -1214,6 +1283,27 @@ Warning.LISTENERS_AFFECTED = Simulationsempf Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Bergungssystem wurde ausgelöst während der Motor noch gebrannt hat. Warning.FILE_INVALID_PARAMETER = Ignoriere ungültigen Parameter. + +! Scale dialog +ScaleDialog.lbl.scaleRocket = Entire rocket +ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents +ScaleDialog.lbl.scaleSelection = Only selected component +ScaleDialog.title = Scale design +ScaleDialog.lbl.scale = Scale: +ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component +ScaleDialog.lbl.scaling = Scaling to apply: +ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design. +! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]" +ScaleDialog.lbl.scaleFrom = Scale from +ScaleDialog.lbl.scaleTo = to +ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length. +ScaleDialog.checkbox.scaleMass = Update explicit mass values +ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor +ScaleDialog.button.scale = Scale +ScaleDialog.undo.scaleRocket = Scale rocket +ScaleDialog.undo.scaleComponent = Scale component +ScaleDialog.undo.scaleComponents = Scale components + !icons Icons.Undo = Undo Icons.Redo = Redo @@ -1224,3 +1314,190 @@ OpenRocketPrintable.DesignReport = Design Report OpenRocketDocument.Redo = Redo OpenRocketDocument.Undo = Undo + +!EllipticalFinSet +EllipticalFinSet.Ellipticalfinset = Elliptical fin set + +! Optimization + +! Modifiers + +optimization.modifier.nosecone.length = Length +optimization.modifier.nosecone.length.desc = Optimize the nose cone length. +optimization.modifier.nosecone.diameter = Diameter +optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter. +optimization.modifier.nosecone.thickness = Thickness +optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness. +optimization.modifier.nosecone.shapeparameter = Shape parameter +optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter. + +optimization.modifier.transition.length = Length +optimization.modifier.transition.length.desc = Optimize the transition length. +optimization.modifier.transition.forediameter = Fore diameter +optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter. +optimization.modifier.transition.aftdiameter = Aft diameter +optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter. +optimization.modifier.transition.thickness = Thickness +optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness. +optimization.modifier.transition.shapeparameter = Shape parameter +optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter. + +optimization.modifier.bodytube.length = Length +optimization.modifier.bodytube.length.desc = Optimize the body tube length. +optimization.modifier.bodytube.outerDiameter = Outer diameter +optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness. +optimization.modifier.bodytube.thickness = Thickness +optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness. + +optimization.modifier.trapezoidfinset.rootChord = Root chord +optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body). +optimization.modifier.trapezoidfinset.tipChord = Tip chord +optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge). +optimization.modifier.trapezoidfinset.sweep = Sweep +optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards). +optimization.modifier.trapezoidfinset.height = Height +optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set. + +optimization.modifier.ellipticalfinset.length = Root chord +optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set. +optimization.modifier.ellipticalfinset.height = Height +optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set. + +optimization.modifier.finset.cant = Cant angle +optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set. +optimization.modifier.finset.position = Position +optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body. + +optimization.modifier.launchlug.length = Length +optimization.modifier.launchlug.length.desc = Optimize the launch lug length. +optimization.modifier.launchlug.outerDiameter = Outer diameter +optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug. +optimization.modifier.launchlug.thickness = Thickness +optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant. +optimization.modifier.launchlug.position = Position +optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body. + + +optimization.modifier.internalcomponent.position = Position +optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component. + +optimization.modifier.masscomponent.mass = Mass +optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component. + +optimization.modifier.parachute.diameter = Diameter +optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter. +optimization.modifier.parachute.coefficient = Drag coefficient +optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8. + +optimization.modifier.streamer.length = Length +optimization.modifier.streamer.length.desc = Optimize the length of the streamer. +optimization.modifier.streamer.width = Width +optimization.modifier.streamer.width.desc = Optimize the width of the streamer. +optimization.modifier.streamer.aspectRatio = Aspect ratio +optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio. +optimization.modifier.streamer.coefficient = Drag coefficient +optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer. + +optimization.modifier.recoverydevice.deployDelay = Deployment delay +optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device. +optimization.modifier.recoverydevice.deployAltitude = Deployment altitude +optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device. + +optimization.modifier.rocketcomponent.overrideMass = Override mass +optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component. +optimization.modifier.rocketcomponent.overrideCG = Override CG +optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component. + +optimization.modifier.motormount.overhang = Motor overhang +optimization.modifier.motormount.overhang.desc = Optimize the motor overhang. +optimization.modifier.motormount.delay = Motor ignition delay +optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay. + + + + +! General rocket design optimization dialog + +GeneralOptimizationDialog.title = Rocket optimization +GeneralOptimizationDialog.goal.maximize = Maximize value +GeneralOptimizationDialog.goal.minimize = Minimize value +GeneralOptimizationDialog.goal.seek = Seek value of +GeneralOptimizationDialog.btn.start = Start optimization +GeneralOptimizationDialog.btn.stop = Stop optimization +GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize: +GeneralOptimizationDialog.btn.add = Add +GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization +GeneralOptimizationDialog.btn.remove = Remove +GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization +GeneralOptimizationDialog.btn.removeAll = Remove all +GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization +GeneralOptimizationDialog.lbl.availableParams = Available parameters: +GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options +GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation: +GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize +GeneralOptimizationDialog.lbl.optimizeValue = Optimized value: +GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized +GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal: +GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization +GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek +GeneralOptimizationDialog.lbl.requireStability = Required stability +GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability: +GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design +GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability: +GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design +GeneralOptimizationDialog.status.bestValue = Best value: +GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far. +GeneralOptimizationDialog.status.stepCount = Step count: +GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed. +GeneralOptimizationDialog.status.evalCount = Evaluations: +GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed. +GeneralOptimizationDialog.status.stepSize = Step size: +GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges) +GeneralOptimizationDialog.btn.plotPath = Plot path +GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only) +GeneralOptimizationDialog.btn.save = Save path +GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file. +GeneralOptimizationDialog.btn.apply = Apply optimization +GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design +GeneralOptimizationDialog.btn.reset = Reset +GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design +GeneralOptimizationDialog.btn.close = Close +GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design +GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters. +GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters +GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run: +GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed +GeneralOptimizationDialog.undoText = Apply optimization +GeneralOptimizationDialog.basicSimulationName = Basic simulation +GeneralOptimizationDialog.noSimulationName = No simulation +GeneralOptimizationDialog.table.col.parameter = Parameter +GeneralOptimizationDialog.table.col.current = Current +GeneralOptimizationDialog.table.col.min = Minimum +GeneralOptimizationDialog.table.col.max = Maximum +GeneralOptimizationDialog.export.header = Include header line +GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions. +GeneralOptimizationDialog.export.stability = Stability + + +! Dialog for plotting optimization results +OptimizationPlotDialog.title = Optimization results +OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out +OptimizationPlotDialog.plot1d.title = Optimization result +OptimizationPlotDialog.plot1d.series = Optimization result +OptimizationPlotDialog.plot2d.title = Optimization path +OptimizationPlotDialog.plot2d.path = Optimization path +OptimizationPlotDialog.plot2d.evals = Evaluations +OptimizationPlotDialog.plot.ttip.stability = Stability: +OptimizationPlotDialog.plot.label.optimum = Optimum + +! Optimization parameters +MaximumAltitudeParameter.name = Apogee altitude +MaximumVelocityParameter.name = Maximum velocity +MaximumAccelerationParameter.name = Maximum acceleration +StabilityParameter.name = Stability +GroundHitVelocityParameter.name = Ground hit speed +LandingDistanceParameter.name = Landing distance +TotalFlightTimeParameter.name = Total flight time +DeploymentVelocityParameter.name = Velocity at parachute deployment + + diff --git a/l10n/messages_es.properties b/l10n/messages_es.properties index 36d368e8f..1dadb61c9 100644 --- a/l10n/messages_es.properties +++ b/l10n/messages_es.properties @@ -6,7 +6,11 @@ # # className.ComponantType.componantName # - +# +# Text tokens within braces should not be translated, e.g. +# "The file '{filename}' exists." +# They are pieces that are inserted dynamically. +# ! Set to the name of the current translation file (used for debugging purposes) @@ -31,7 +35,6 @@ RocketActions.CopyAct.ttip.Copy = Copiar este componente (y subcomponentes) a la RocketActions.PasteAct.Paste = Pegar RocketActions.PasteAct.ttip.Paste = Pegar el componente o simulación de la libreta de notas al diseño. RocketActions.EditAct.Edit = Editar componente -!Mostrar RocketActions.EditAct.ttip.Edit = Mostrar el componente seleccionado RocketActions.NewStageAct.Newstage = Nueva etapa RocketActions.NewStageAct.ttip.Newstage = Añadir una nueva etapa al diseño del cohete @@ -55,17 +58,16 @@ BasicFrame.SimpleFileFilter1 = Todos los dise BasicFrame.SimpleFileFilter2 = Diseños OpenRocket (*.ork) BasicFrame.SimpleFileFilter3 = Diseños RockSim (*.rkt) BasicFrame.tab.Rocketdesign = Diseño del cohete -!Diseños de cohete BasicFrame.tab.Flightsim = Simulaciones de vuelo BasicFrame.title.Addnewcomp = Añadir un nuevo componente -BasicFrame.item.Openrocketdesign = Abrir un diseño de cohete -BasicFrame.item.Openexamplerocketdesign = Abrir un ejemplo de diseño de cohete -BasicFrame.item.SavecurRocketdesign = Guardar el diseño actual -BasicFrame.item.SavecurRocketdesnewfile = Guardar el diseño actual como un nuevo documento -BasicFrame.item.Printpart = Imprimir un listado de componentes y un esquema de aleta -BasicFrame.item.Closedesign = Cerrar el diseño actual -BasicFrame.item.Quitprogram = Abandonar el programa -BasicFrame.menu.Rocketedt = Mostrando el cohete +!BasicFrame.item.Openrocketdesign = Abrir un diseño de cohete +!BasicFrame.item.Openexamplerocketdesign = Abrir un ejemplo de diseño de cohete +!BasicFrame.item.SavecurRocketdesign = Guardar el diseño actual +!BasicFrame.item.SavecurRocketdesnewfile = Guardar el diseño actual como un nuevo documento +!BasicFrame.item.Printpart = Imprimir un listado de componentes y un esquema de aleta +!BasicFrame.item.Closedesign = Cerrar el diseño actual +!BasicFrame.item.Quitprogram = Abandonar el programa +!BasicFrame.menu.Rocketedt = Mostrando el cohete BasicFrame.dlg.lbl1 = Diseño BasicFrame.dlg.lbl2 = No se ha guardado BasicFrame.dlg.lbl3 = ¿Quiere guardarlo? @@ -75,7 +77,17 @@ BasicFrame.WarningDialog.txt1 = Mientras se abr BasicFrame.WarningDialog.txt2 = Algunas configuraciones de diseño no pudieron cargarse correctamente. BasicFrame.WarningDialog.title = Precauciones mientras se abre el archivo + +! General error messages used in multiple contexts +error.fileExists.title = File exists +error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it? + +error.writing.title = Error writing file +error.writing.desc = An error occurred while writing to the file: + + ! Labels used in buttons of dialog windows +# TODO: Rename these to "btn.xxx" button.ok = OK button.cancel = Borrar button.close = Cerrar @@ -88,6 +100,7 @@ dlg.but.close = Cerrar ! General file type names filetypes.pdf = PDF files + ! About Dialog AboutDialog.lbl.version = Version ! The texts below provide additional credits for the translation maintainer @@ -100,6 +113,7 @@ AboutDialog.lbl.translator = Tripoli Spain AboutDialog.lbl.translatorWebsite = http://www.tripoli-spain.org/ AboutDialog.lbl.translatorIcon = logoTripoliSpain.png + ! Print dialog PrintDialog.title = Imprimir o exportar PrintDialog.but.previewAndPrint = Vista previa & Imprimir @@ -112,6 +126,7 @@ PrintDialog.error.preview.title = Imposible abrir vista previa PrintDialog.error.preview.desc1 = Imposible abrir vista previa en PDF. PrintDialog.error.preview.desc2 = Por favour usar la opción Guardar como PDF. + !PrintSettingsDialog PrintSettingsDialog.title = Imprimir puesta a punto PrintSettingsDialog.lbl.Templatefillcolor = Plantilla de colores: @@ -121,9 +136,9 @@ PrintSettingsDialog.lbl.Paperorientation = Orientaci PrintSettingsDialog.but.Reset = Reinicializar PrintSettingsDialog.but.Close = Cerrar + ! Bug Report dialog bugreport.dlg.title = Informe de errores -!Report de error bugreport.dlg.but.Sendbugreport = Enviar un report de error bugreport.dlg.but.Sendbugreport.Ttip = Enviar automáticamente un report de error a los creadores de Open Rocket bugreport.dlg.successmsg1 = Report de error enviado con éxito @@ -136,14 +151,14 @@ bugreport.dlg.failedmsg1 = OpenRocket fue incapaz de enviar el report de error: bugreport.dlg.failedmsg2 = Por favor envíe manualmente el report a bugreport.dlg.failedmsg3 = Error enviando el report bugreport.reportDialog.txt = Puede realizar un informe de errores escribiendo en el formulario de abajo y enviándolo.
También puede informar de los errores adjuntando el archivo de su proyecto por email. -!Puede enviar un report de error en OpenRocket rellenando el formulario de abajo y enviándolo.
También puede reportar errores e incluir adjuntos sobre el proyecto de Web. bugreport.reportDialog.txt2 = Por favor incluya una breve descripción de lo que estaba haciendo cuando ocurrió la excepción. +bugreport.dlg.provideDescription = Please provide a description of the bug first. +bugreport.dlg.provideDescription.title = Bug description missing ! Debug log dialog debuglogdlg.but.clear = Limpiar debuglogdlg.OpenRocketdebuglog = Registro de sucesos -!Fichero de error de Open Rocket debuglogdlg.Displayloglines = Mostrar líneas de registro: debuglogdlg.Follow = Seguir debuglogdlg.col.Time = Hora @@ -244,6 +259,7 @@ pref.dlg.lbl.Temperature = Temperatura: pref.dlg.lbl.Momentofinertia = Momento de inercia: pref.dlg.lbl.Pressure = Presión: pref.dlg.lbl.Stability = Estabilidad: +pref.dlg.lbl.FlightTime = Flight time: pref.dlg.lbl.effect1 = Los cambios tendrán efecto cuando se abra nuevamente una ventana. pref.dlg.lbl.Checkingupdates = Comprobando actualizaciones... pref.dlg.lbl.msg1 = Ocurrió un error mientras se comunicaba con el servidor. @@ -258,6 +274,9 @@ pref.dlg.PrefBooleanSelector2 = Confirmar pref.dlg.Add = Añadir pref.dlg.DescriptionArea.Adddirectories = Añadir directorios, RASP archivos de motor (*.eng), RockSim archivos de motor (*.rse) o ZIP archivos separados por punto y coma (;) para cargar curvas de empuje externas. Los cambios tendrán efecto la próxima vez que abra OpenRocket. +PreferencesDialog.lbl.language = Interface language: +PreferencesDialog.languages.default = System default +PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket. ! Simulation edit dialog simedtdlg.but.runsimulation = Lanzar la simulación @@ -294,6 +313,10 @@ simedtdlg.lbl.ttip.Pressure = Presi simedtdlg.lbl.Launchsite = Lugar del lanzamiento simedtdlg.lbl.Latitude = Latitud: simedtdlg.lbl.ttip.Latitude = La latitud del lugar de lanzamiento afecta la atracción terrestre.
Los valores positivos se dan en el hemisferio Norte, los negativos en el hemisferio Sur. + +simedtdlg.lbl.Longitude = Longitude: +simedtdlg.lbl.ttip.Longitude = Required for weather prediction and elevation models. + simedtdlg.lbl.Altitude = Altitud: simedtdlg.lbl.ttip.Altitude = Los valores por encima del nivel del mar.
Esto afecta la posición del modelo atmosférico. simedtdlg.border.Launchrod = Varilla para lanzar @@ -312,6 +335,8 @@ simedtdlg.lbl.ExtBarrowman = Barrowman Extendido simedtdlg.lbl.Simmethod = Método de simulación: simedtdlg.lbl.ttip.Simmethod1 = El simulador de seis-grados-de-libertad permite al cohete una total libertad durante el vuelo.
simedtdlg.lbl.ttip.Simmethod2 = La integración mejora usando un 4th ordenar Runge-Kutta 4 integración numérica. +simedtdlg.lbl.GeodeticMethod = Geodetic calculations: +simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations. simedtdlg.lbl.Timestep = Duración de la etapa simedtdlg.lbl.ttip.Timestep1 = Tiempo entre etapas de simulación.
Un tiempo mas corto de etapa origina una simulación mas exacta pero mas lenta.
simedtdlg.lbl.ttip.Timestep2 = The 4th ordenar el método de simulación es bastante preciso con un tiempo de etapa de @@ -333,6 +358,14 @@ simedtdlg.IntensityDesc.High = Alto simedtdlg.IntensityDesc.Veryhigh = Muy alto simedtdlg.IntensityDesc.Extreme = Extremo +GeodeticComputationStrategy.none.name = None +GeodeticComputationStrategy.none.desc = Perform no geodetic computations. +GeodeticComputationStrategy.spherical.name = Spherical approximation +GeodeticComputationStrategy.spherical.desc = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. +GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid +GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
Slower and unnecessary in most cases. + + ! Simulation Panel @@ -404,6 +437,12 @@ SimExpPan.ExportingVar.desc3 = variables fuera de SimExpPan.Col.Variable = Variable SimExpPan.Col.Unit = Unidad + +CsvOptionPanel.separator.space = SPACE +CsvOptionPanel.separator.tab = TAB + + + ! MotorPlot MotorPlot.title.Motorplot = Curva del motor MotorPlot.but.Select = Seleccionar la configuración del motor a usar @@ -476,7 +515,7 @@ componentanalysisdlg.lbl.machnumber = N componentanalysisdlg.lbl.rollrate = Valor de giro: componentanalysisdlg.lbl.activestages = Etapas activas: componentanalysisdlg.lbl.motorconf = Configuración del Motor: -componentanalysisdlg.TabStability.Col.Component = Componente +componentanalysisdlg.TabStability.Col = Componente componentanalysisdlg.TabStability = Estabilidad componentanalysisdlg.TabStability.ttip = Información de Estabilidad componentanalysisdlg.dragTableModel.Col.Component = Componente @@ -497,6 +536,7 @@ componentanalysisdlg.println.settingnam = CONFIGURANDO VALORES NAN componentanalysisdlg.lbl.reflenght = Longitud de referencia: componentanalysisdlg.lbl.refarea = Área de referencia: !componentanalysisdlg.But.close =Close +componentanalysisdlg.TabStability.Col.Component = Component ! Custom Material dialog custmatdlg.title.Custommaterial = Material hecho en casa @@ -514,7 +554,6 @@ ringcompcfg.Thickness = Espesor ringcompcfg.Length = Longitud ringcompcfg.Positionrelativeto = Posición relativa a: ringcompcfg.plus = Localización -!plus ringcompcfg.PositionValue = Valor de posición ringcompcfg.Radialdistance = Distancia radial: ringcompcfg.Distancefrom = Distancia desde la línea central del cohete @@ -537,7 +576,6 @@ BodyTubecfg.tab.Motor = Motor BodyTubecfg.tab.Motormountconf = Configuración del porta motor BodyTubecfg.checkbox.Automatic = Automático BodyTubecfg.checkbox.Filled = Sólido -!Archivado ! FinSetConfig FinSetConfig.tab.Fintabs = Raíz de aleta @@ -574,10 +612,8 @@ ShockCordCfg.lbl.Shockcordlength = Longitud del tirante de suspensi RocketCompCfg.lbl.Componentname = Nombre del componente: RocketCompCfg.ttip.Thecomponentname = El nombre del componente. RocketCompCfg.tab.Override = Especificar -!Elegir RocketCompCfg.tab.MassandCGoverride = Elección de estimación de Masa y CG RocketCompCfg.tab.Figure = Estilo -!Figura RocketCompCfg.tab.Figstyleopt = Opciones de estilo de la figura RocketCompCfg.tab.Comment = Comentarios RocketCompCfg.tab.Specifyacomment = Especifique un comentario para el componente @@ -594,23 +630,18 @@ RocketCompCfg.lbl.longA2 = El valor indicado es el promedio de la rugosidad en a RocketCompCfg.but.Setforall = Aplicar a todos RocketCompCfg.but.ttip.Setforall = Aplicar este acabado a todos los componentes del cohete. RocketCompCfg.lbl.Overridemassorcenter = Especificar la masa y el CG de la ojiva -!Elegir la masa o el CG del RocketCompCfg.checkbox.Overridemass = Elegir la masa: RocketCompCfg.checkbox.Overridecenterofgrav = Elegir el CG: RocketCompCfg.checkbox.OverridemassandCG = Elegir la masa y el CG de todos los subcomponentes RocketCompCfg.lbl.longB1 = La masa elegida no incluye los motores.
RocketCompCfg.lbl.longB2 = El CG se mide desde el extremo frontal de la -!El CG se mide desde el extremo frontal del RocketCompCfg.lbl.Commentsonthe = Comentarios sobre RocketCompCfg.lbl.Figurestyle = Estilo de dibujo: -!Estilo de figura: RocketCompCfg.lbl.Componentcolor = Color del componente: RocketCompCfg.lbl.Choosecolor = Elija color RocketCompCfg.checkbox.Usedefaultcolor = Usar color por defecto -!Use color por defecto RocketCompCfg.lbl.Complinestyle = Estilo de línea del componente: RocketCompCfg.but.Saveasdefstyle = Guardar como estilo por defecto -!Guarde como estilo por defecto RocketCompCfg.lbl.Diameter = Diámetro: RocketCompCfg.lbl.Length = Longitud: RocketCompCfg.lbl.Thickness = Espesor: @@ -622,7 +653,7 @@ RocketCompCfg.border.Foreshoulder = Hombro visible !RocketCompCfg.lbl.Length = Length: ! BulkheadConfig -BulkheadCfg.tab.Radius = Radio: +BulkheadCfg.tab.Diameter = Diámetro: BulkheadCfg.tab.Thickness = Espesor: BulkheadCfg.tab.General = General BulkheadCfg.tab.Generalproperties = Propiedades generales @@ -643,13 +674,10 @@ ComponentCfgDlg.Modify = Modificar EllipticalFinSetCfg.Nbroffins = Número de aletas: EllipticalFinSetCfg.Rotation = Rotación: EllipticalFinSetCfg.Fincant = Giro de las aletas: -!Canto de aleta: EllipticalFinSetCfg.Rootchord = Longitud línea base: -!Anclaje de la raíz: EllipticalFinSetCfg.Height = Altura: EllipticalFinSetCfg.Positionrelativeto = Posición relativa a: EllipticalFinSetCfg.plus = Localización -!plus EllipticalFinSetCfg.FincrossSection = Sección de corte de la aleta: EllipticalFinSetCfg.Thickness = Espesor: EllipticalFinSetCfg.General = General @@ -664,17 +692,17 @@ FreeformFinSetCfg.tab.ttip.Finshape = Forma de la aleta FreeformFinSetCfg.lbl.Numberoffins = Número de aletas: FreeformFinSetCfg.lbl.Finrotation = Rotación de las aletas: FreeformFinSetCfg.lbl.Fincant = Giro de las aletas -!Canto de la aleta: FreeformFinSetCfg.lbl.ttip.Fincant = Angulo que el canto de las aletas forman con respecto al fuselaje. FreeformFinSetCfg.lbl.Posrelativeto = Posición relativa a: FreeformFinSetCfg.lbl.plus = Localización -!plus FreeformFinSetCfg.lbl.FincrossSection = Sección de la aleta: FreeformFinSetCfg.lbl.Thickness = Espesor: -FreeformFinSetCfg.lbl.Double-click = Doble clic en la lista -FreeformFinSetCfg.lbl.toedit = para editar -FreeformFinSetCfg.lbl.Clickdrag = Clic (sobre línea)+arrastrar: Agregar punto -FreeformFinSetCfg.lbl.Ctrlclick = Control+Clic (sobre punto): Eliminar punto +! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle +FreeformFinSetCfg.lbl.doubleClick1 = Doble clic en la lista +FreeformFinSetCfg.lbl.doubleClick2 = para editar +FreeformFinSetCfg.lbl.clickDrag = Clic (sobre línea)+arrastrar: Agregar punto +FreeformFinSetCfg.lbl.ctrlClick = Control+Clic (sobre punto): Eliminar punto + !InnerTubeConfig InnerTubeCfg.tab.Motor = Motor @@ -703,7 +731,6 @@ LaunchLugCfg.lbl.Thickness = Espesor: LaunchLugCfg.lbl.Radialpos = Posición radial: LaunchLugCfg.lbl.Posrelativeto = Posición relativa a: LaunchLugCfg.lbl.plus = Localización -!plus LaunchLugCfg.tab.General = General LaunchLugCfg.tab.Generalprop = Propiedades generales @@ -713,7 +740,6 @@ MassComponentCfg.lbl.Length = Longitud MassComponentCfg.lbl.Diameter = Diámetro MassComponentCfg.lbl.PosRelativeto = Posición relativa a: MassComponentCfg.lbl.plus = Localización -!plus MassComponentCfg.tab.General = General MassComponentCfg.tab.ttip.General = Propiedades generales MassComponentCfg.tab.Radialpos = Posición radial @@ -730,7 +756,6 @@ MotorCfg.lbl.Currentmotor = Motor actual: MotorCfg.lbl.Motoroverhang = Sobresalida del motor: MotorCfg.lbl.Ignitionat = Encendido en: MotorCfg.lbl.plus = Localización -!plus MotorCfg.lbl.seconds = segundos MotorCfg.lbl.longA1 = El diseño actual tiene solo una etapa. MotorCfg.lbl.longA2 = Pueden agregarse etapas haciendo clic \"Nueva etapa\". @@ -743,22 +768,18 @@ MotorCfg.lbl.motorLabel = Ninguno ! NoseConeConfig NoseConeCfg.lbl.Noseconeshape = Forma de la ojiva: NoseConeCfg.lbl.Shapeparam = Valor de forma: -!Parámetros de la forma: NoseConeCfg.lbl.Noseconelength = Longitud de la ojiva: NoseConeCfg.lbl.Basediam = Diámetro de la base: NoseConeCfg.checkbox.Automatic = Automático NoseConeCfg.lbl.Wallthickness = Espesor de la pared: NoseConeCfg.checkbox.Filled = Sólido -!Archivado NoseConeCfg.tab.General = General NoseConeCfg.tab.ttip.General = Propiedades generales NoseConeCfg.tab.Shoulder = Acoplamiento -!Hombro NoseConeCfg.tab.ttip.Shoulder = Propiedades del hombro ! ParachuteConfig ParachuteCfg.lbl.Canopy = Pabellón -!Campana: ParachuteCfg.lbl.Diameter = Diámetro: ParachuteCfg.lbl.Material = Material: ParachuteCfg.combo.MaterialModel = El material del componente afecta su peso. @@ -773,9 +794,6 @@ ParachuteCfg.lbl.Linelength = Longitud de cuerda: ParachuteCfg.lbl.Material = Material: ParachuteCfg.lbl.Posrelativeto = Posición relativa a: ParachuteCfg.lbl.plus = Localización -ParachuteCfg.lbl.plusdelay = Retardo - -!plus ParachuteCfg.lbl.Packedlength = Longitud empaquetado: ParachuteCfg.lbl.Packeddiam = Diámetro del empaquetado: ParachuteCfg.lbl.Deploysat = Despliegue en: @@ -788,13 +806,14 @@ ParachuteCfg.tab.ttip.Radialpos = Configuraci ParachuteCfg.lbl.Radialdistance = Distancia radial: ParachuteCfg.lbl.Radialdirection = Dirección radial: ParachuteCfg.but.Reset = Reiniciar +ParachuteCfg.lbl.plusdelay = Retardo + ! ShockCordConfig ShockCordCfg.lbl.Shockcordlength = Longitud del tirante de suspensión ShockCordCfg.lbl.Shockcordmaterial = Material del tirante de suspensión: ShockCordCfg.lbl.Posrelativeto = Posición relativa a: ShockCordCfg.lbl.plus = Localización -!plus ShockCordCfg.lbl.Packedlength = Longitud del empaquetado: ShockCordCfg.lbl.Packeddiam = Diámetro del empaquetado: ShockCordCfg.tab.General = General @@ -822,7 +841,6 @@ StreamerCfg.lbl.Automatic = Autom StreamerCfg.lbl.longC1 = El coeficiente de Fricción es relativo al área de la banderola. StreamerCfg.lbl.Posrelativeto = Posición relativa a: StreamerCfg.lbl.plus = Localización -!plus StreamerCfg.lbl.Packedlength = Longitud de empaquetado: StreamerCfg.lbl.Packeddiam = Diámetro de empaquetado: StreamerCfg.lbl.Deploysat = Despliegue a: @@ -849,18 +867,15 @@ ThicknessRingCompCfg.tab.Generalprop = Propiedades generales TransitionCfg.lbl.Transitionshape = Forma de la transición: TransitionCfg.checkbox.Clipped = Acortado TransitionCfg.lbl.Shapeparam = Valor de forma: -!Parámetro de forma: TransitionCfg.lbl.Transitionlength = Longitud de la transición: TransitionCfg.lbl.Forediam = Diámetro delantero: TransitionCfg.checkbox.Automatic = Automático TransitionCfg.lbl.Aftdiam = Diámetro trasero: TransitionCfg.lbl.Wallthickness = Espesor de la pared: TransitionCfg.checkbox.Filled = Sólido -!Archivado TransitionCfg.tab.General = General TransitionCfg.tab.Generalproperties = Propiedades generales TransitionCfg.tab.Shoulder = Acoplamiento -!Hombro TransitionCfg.tab.Shoulderproperties = Propiedades del hombro ! TrapezoidFinSetConfig @@ -871,19 +886,14 @@ TrapezoidFinSetCfg.lbl.ttip.Finrotation = TrapezoidFinSetCfg.lbl.Fincant = Canto de aleta: TrapezoidFinSetCfg.lbl.ttip.Fincant = El ángulo del canto de las aletas respecto al fuselaje. TrapezoidFinSetCfg.lbl.Rootchord = Longitud línea base: -!Anclaje de la raíz: TrapezoidFinSetCfg.lbl.Tipchord = Longitud borde superior: -!Forma de la extremidad: TrapezoidFinSetCfg.lbl.Height = Altura: TrapezoidFinSetCfg.lbl.Sweeplength = Desplazamiento borde superior: -!Longitud del barrido: TrapezoidFinSetCfg.lbl.Sweepangle = Angulo de ataque: -!Ángulo de barrido: TrapezoidFinSetCfg.lbl.FincrossSection = Sección de la aleta: TrapezoidFinSetCfg.lbl.Thickness = Espesor: TrapezoidFinSetCfg.lbl.Posrelativeto = Posición relativa a: TrapezoidFinSetCfg.lbl.plus = Localización -!plus TrapezoidFinSetCfg.tab.General = General TrapezoidFinSetCfg.tab.Generalproperties = Propiedades generales @@ -943,37 +953,59 @@ PlotDialog.lbl.Chart = Click+bajar el rozamiento+derecha ampliar, arriba+izquier ! "main" prefix is used for the main application dialog +# FIXME: Rename the description keys + main.menu.file = Archivo +main.menu.file.desc = File-handling related tasks main.menu.file.new = Nuevo +main.menu.file.new.desc = Create a new rocket design main.menu.file.open = Abrir ... +BasicFrame.item.Openrocketdesign = Abrir un diseño de cohete main.menu.file.openExample = Abrir ejemplo ... +BasicFrame.item.Openexamplerocketdesign = Abrir un ejemplo de diseño de cohete main.menu.file.save = Guardar +BasicFrame.item.SavecurRocketdesign = Guardar el diseño actual main.menu.file.saveAs = Guardar como ... +BasicFrame.item.SavecurRocketdesnewfile = Guardar el diseño actual como un nuevo documento main.menu.file.print = Imprimir ... +BasicFrame.item.Printpart = Imprimir un listado de componentes y un esquema de aleta main.menu.file.close = Cerrar +BasicFrame.item.Closedesign = Cerrar el diseño actual main.menu.file.quit = Salir -!Silenciar +BasicFrame.item.Quitprogram = Abandonar el programa main.menu.edit = Edición -!Representar +BasicFrame.menu.Rocketedt = Mostrando el cohete main.menu.edit.undo = Invertir +main.menu.edit.undo.desc = Undo the previous operation main.menu.edit.redo = Rehacer +main.menu.edit.redo.desc = Redo the previously undone operation main.menu.edit.cut = Cortar main.menu.edit.copy = Copiar main.menu.edit.paste = Pegar main.menu.edit.delete = Borrar +main.menu.edit.resize = Scale... +main.menu.edit.resize.desc = Scale parts of the rocket design main.menu.edit.preferences = Preferencias +main.menu.edit.preferences.desc = Setup the application preferences main.menu.analyze = Analizar +main.menu.analyze.desc = Rocket analysis main.menu.analyze.componentAnalysis = Análisis de componentes +main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately +main.menu.analyze.optimization = Rocket optimization +main.menu.analyze.optimization.desc = General rocket design optimization main.menu.help = Ayuda +main.menu.help.desc = Information about OpenRocket main.menu.help.license = Licencia +main.menu.help.license.desc = OpenRocket license information main.menu.help.bugReport = Informe de errores -!Report de supresiones +main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket main.menu.help.debugLog = Registro de sucesos -!Registro de recuperaciones +main.menu.help.debugLog.desc = View the OpenRocket debug log main.menu.help.about = Acerca de +main.menu.help.about.desc = Copyright details about OpenRocket main.menu.debug = Recuperación main.menu.debug.whatisthismenu = ¿Que es este menú? @@ -1005,6 +1037,7 @@ Databases.materials.Spruce = Pulido Databases.materials.StyrofoamgenericEPS = Porex (generico EPS) Databases.materials.StyrofoamBluefoamXPS = Porex \"Foam azul\" (XPS) Databases.materials.Quantumtubing = Quantum tubing +Databases.materials.BlueTube = Blue tube !SURFACE_MATERIAL Databases.materials.Ripstopnylon = Ripstop nylon Databases.materials.Mylar = Mylar @@ -1037,10 +1070,8 @@ ExternalComponent.Polished = Pulido ! LineStyle LineStyle.Solid = Sólido LineStyle.Dashed = Discontinuo -!Pulverizado LineStyle.Dotted = Punteado LineStyle.Dash-dotted = Discontinuo con puntos -!Pulverizado con puntos LineStyle.Defaultstyle = Estilo por defecto ! Shape @@ -1050,27 +1081,17 @@ Shape.Conical.desc2 = Transici Shape.Ogive = Ojiva Shape.Ogive.desc1 = Ojiva con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una Ojiva tangente, mientras que un valor inferior a 1 produce una Ojiva secante con un perfil más afilado. Shape.Ogive.desc2 = Ojiva con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una Ojiva tangente, mientras que un valor inferior a 1 produce una Ojiva secante con un perfil más afilado. -!Una ojiva con perfil de arco de circunferencia. El parámetro de forma de valor 1 produce una Tangente a la ojiva, Que tiene una transición suave al fuselaje, produce un valor menor que 1 Secante a la ojiva. Shape.Ellipsoid = Elipsoide Shape.Ellipsoid.desc1 = Ojiva con perfil de media elipse. Por defecto, una elipse de longitud igual al triple de su diámetro. -!Una ojiva elipsoidal tiene un perfil de media elipse con el eje mayor de longitud 2&veces;Longitud y Diámetro. Shape.Ellipsoid.desc2 = Ojiva con perfil de media elipse. Por defecto, una elipse de longitud igual al triple de su diámetro. -!Una ojiva elipsoidal tiene un perfil de media elipse con el eje mayor de longitud 2&veces;Longitud y Diámetro. Si la transición no se interrumpe, entonces el perfil se extiende al centro con el correspondiente radio. Shape.Powerseries = Serie potencial -!Series potentes -!Shape.Powerseries.desc1 = A power series nose cone has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 this is a \u00BD-power or parabolic nose cone, for k=0.75 a \u00BE-power, and for k=1 a conical nose cone. -!Shape.Powerseries.desc2 = A power series transition has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 the transition is \u00BD-power or parabolic, for k=0.75 a \u00BE-power, and for k=1 conical. - Shape.Powerseries.desc1 = Ojiva cuyo perfil es una curva obtenida a partir de una función potencial f(x)k. Un valor de forma k=0.5 produce una ojiva con perfil de parábola, para k=0.75 se produce una ojiva con perfil potencial, y para k=1 se produce una ojiva con perfil recto u Ojiva cónica. -!Shape.Powerseries.desc1 = Una serie de ojivas potentes tiene un perfil deRadio &veces; (x / Longitud)k donde k es el parámetro de forma. Para k=0.5 este es un \u00BD-potencia o parabólico ojiva, para k=0.75 un \u00BE-potencia, y para k=1 a cónica ojiva. Shape.Powerseries.desc2 = Una serie de transiciones potentes tiene un perfil de Radio &veces; (x / Longitud)k donde k es el parámetro de forma. Para k=0.5 la transición es \u00BD-potencia o parabólica, para k=0.75 a \u00BE-potencia, y para k=1 cónica. Shape.Parabolicseries = Serie parabólica Shape.Parabolicseries.desc1 = Ojiva con perfil de arco de parábola. Un valor de forma igual a 1 produce una Ojiva tangente, un valor igual a 0.75 produce una parábola de 3/4, un valor igual a 0.5 produce una parábola de 1/2, y un valor igual a 0 produce una perfil recto u Ojiva cónica. -!Shape.Parabolicseries.desc1 = A parabólica series ojiva Cone has a perfil de a parábola. The forma parámetro defines el segmento de el parábola a utilice. The forma parámetro 1.0 produces a full parábola que es tangente a el body tubo, 0.75 produces a 3/4 parábola, 0.5 procudes a 1/2 parábola y 0 produces a cónico ojiva . Shape.Parabolicseries.desc2 = A parabólica series transición has a perfil de a parábola. The forma parámetro defines el segmento de el parábola a utilice. The forma parámetro 1.0 produces a full parábola que es tangente a el body tubo at el aft extremo, 0.75 produces a 3/4 parábola, 0.5 procudes a 1/2 parábola y 0 produces a cónico transición. Shape.Haackseries = Haack series Shape.Haackseries.desc1 = Ojiva con perfil de mínimo arrastre aerodinámico recomendado para vuelos supersónicos. Un valor de forma igual a 0 produce una Ojiva LD Haack u Ojiva Von Karman que minimiza el arrastre aerodinámico para una determinada longitud y diámetro de la base, mientras que un valor igual a 0.333 produce una Ojiva LV-Haack que minimiza el arrastre aerodinámico para una determinada longitud y volumen de la ojiva. -!The Haack series ojiva are designado a minimizar drag. The forma parámetro 0 produces un LD-Haack o Von Karman ojiva , que minimizas drag para fijado longitud y diámetro, mientras a valor de 0.333 produces un LV-Haack ojiva , que minimizas drag para fijado longitud y volumen. Shape.Haackseries.desc2 = The Haack series ojiva are designado a minimizar drag. estas transición formas are sus equivalentes, pero do no necesariamente produce optima drag para transiciones. The forma parámetro 0 produces un LD-Haack o Von Karman forma, mientras a valor de 0.333 produces un LV-Haack shape. @@ -1192,7 +1213,6 @@ RocketInfo.accelerationValue = N/A FinSet.CrossSection.SQUARE = Cuadrado FinSet.CrossSection.ROUNDED = Redondo FinSet.CrossSection.AIRFOIL = Aerodinámico -!Superficie de sustentación FinSet.TabRelativePosition.FRONT = Borde principal del extremo de anclaje FinSet.TabRelativePosition.CENTER = Borde principal del anclaje FinSet.TabRelativePosition.END = Borde principal de tracción @@ -1248,6 +1268,9 @@ FlightDataType.TYPE_AIR_PRESSURE = Presi FlightDataType.TYPE_SPEED_OF_SOUND = Velocidad del sonido FlightDataType.TYPE_TIME_STEP = Simulación del tiempo de etapa FlightDataType.TYPE_COMPUTATION_TIME = Cálculo del tiempo +FlightDataType.TYPE_LATITUDE = Latitude +FlightDataType.TYPE_LONGITUDE = Longitude +FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration ! PlotConfiguration PlotConfiguration.Verticalmotion = Movimiento vertical vs. Tiempo @@ -1269,6 +1292,27 @@ Warning.LISTENERS_AFFECTED = Los oyentes modificaron la simulaci Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Sistema de recuperación abierto mientras el motor todavía empujaba Warning.FILE_INVALID_PARAMETER = Parámetro no válido encontrado. Ignorarlo. + +! Scale dialog +ScaleDialog.lbl.scaleRocket = Entire rocket +ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents +ScaleDialog.lbl.scaleSelection = Only selected component +ScaleDialog.title = Scale design +ScaleDialog.lbl.scale = Scale: +ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component +ScaleDialog.lbl.scaling = Scaling to apply: +ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design. +! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]" +ScaleDialog.lbl.scaleFrom = Scale from +ScaleDialog.lbl.scaleTo = to +ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length. +ScaleDialog.checkbox.scaleMass = Update explicit mass values +ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor +ScaleDialog.button.scale = Scale +ScaleDialog.undo.scaleRocket = Scale rocket +ScaleDialog.undo.scaleComponent = Scale component +ScaleDialog.undo.scaleComponents = Scale components + !icons Icons.Undo = Undo Icons.Redo = Redo @@ -1278,4 +1322,191 @@ OpenRocketPrintable.Fintemplates = Fin templates OpenRocketPrintable.DesignReport = Design Report OpenRocketDocument.Redo = Rehacer -OpenRocketDocument.Undo = Deshacer \ No newline at end of file +OpenRocketDocument.Undo = Deshacer + +!EllipticalFinSet +EllipticalFinSet.Ellipticalfinset = Elliptical fin set + +! Optimization + +! Modifiers + +optimization.modifier.nosecone.length = Nose cone length +optimization.modifier.nosecone.length.desc = Optimize the nose cone length. +optimization.modifier.nosecone.diameter = Nose cone diameter +optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter. +optimization.modifier.nosecone.thickness = Nose cone thickness +optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness. +optimization.modifier.nosecone.shapeparameter = Shape parameter +optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter. + +optimization.modifier.transition.length = Length +optimization.modifier.transition.length.desc = Optimize the transition length. +optimization.modifier.transition.forediameter = Fore diameter +optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter. +optimization.modifier.transition.aftdiameter = Aft diameter +optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter. +optimization.modifier.transition.thickness = Thickness +optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness. +optimization.modifier.transition.shapeparameter = Shape parameter +optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter. + +optimization.modifier.bodytube.length = Length +optimization.modifier.bodytube.length.desc = Optimize the body tube length. +optimization.modifier.bodytube.outerDiameter = Outer diameter +optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness. +optimization.modifier.bodytube.thickness = Thickness +optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness. + +optimization.modifier.trapezoidfinset.rootChord = Root chord +optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body). +optimization.modifier.trapezoidfinset.tipChord = Tip chord +optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge). +optimization.modifier.trapezoidfinset.sweep = Sweep +optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards). +optimization.modifier.trapezoidfinset.height = Height +optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set. + +optimization.modifier.ellipticalfinset.length = Root chord +optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set. +optimization.modifier.ellipticalfinset.height = Height +optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set. + +optimization.modifier.finset.cant = Cant angle +optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set. +optimization.modifier.finset.position = Position +optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body. + +optimization.modifier.launchlug.length = Length +optimization.modifier.launchlug.length.desc = Optimize the launch lug length. +optimization.modifier.launchlug.outerDiameter = Outer diameter +optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug. +optimization.modifier.launchlug.thickness = Thickness +optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant. +optimization.modifier.launchlug.position = Position +optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body. + + +optimization.modifier.internalcomponent.position = Position +optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component. + +optimization.modifier.masscomponent.mass = Mass +optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component. + +optimization.modifier.parachute.diameter = Diameter +optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter. +optimization.modifier.parachute.coefficient = Drag coefficient +optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8. + +optimization.modifier.streamer.length = Length +optimization.modifier.streamer.length.desc = Optimize the length of the streamer. +optimization.modifier.streamer.width = Width +optimization.modifier.streamer.width.desc = Optimize the width of the streamer. +optimization.modifier.streamer.aspectRatio = Aspect ratio +optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio. +optimization.modifier.streamer.coefficient = Drag coefficient +optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer. + +optimization.modifier.recoverydevice.deployDelay = Deployment delay +optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device. +optimization.modifier.recoverydevice.deployAltitude = Deployment altitude +optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device. + +optimization.modifier.rocketcomponent.overrideMass = Override mass +optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component. +optimization.modifier.rocketcomponent.overrideCG = Override CG +optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component. + +optimization.modifier.motormount.overhang = Motor overhang +optimization.modifier.motormount.overhang.desc = Optimize the motor overhang. +optimization.modifier.motormount.delay = Motor ignition delay +optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay. + + + + +! General rocket design optimization dialog + +GeneralOptimizationDialog.title = Rocket optimization +GeneralOptimizationDialog.goal.maximize = Maximize value +GeneralOptimizationDialog.goal.minimize = Minimize value +GeneralOptimizationDialog.goal.seek = Seek value of +GeneralOptimizationDialog.btn.start = Start optimization +GeneralOptimizationDialog.btn.stop = Stop optimization +GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize: +GeneralOptimizationDialog.btn.add = Add +GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization +GeneralOptimizationDialog.btn.remove = Remove +GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization +GeneralOptimizationDialog.btn.removeAll = Remove all +GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization +GeneralOptimizationDialog.lbl.availableParams = Available parameters: +GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options +GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation: +GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize +GeneralOptimizationDialog.lbl.optimizeValue = Optimized value: +GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized +GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal: +GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization +GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek +GeneralOptimizationDialog.lbl.requireStability = Required stability +GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability: +GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design +GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability: +GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design +GeneralOptimizationDialog.status.bestValue = Best value: +GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far. +GeneralOptimizationDialog.status.stepCount = Step count: +GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed. +GeneralOptimizationDialog.status.evalCount = Evaluations: +GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed. +GeneralOptimizationDialog.status.stepSize = Step size: +GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges) +GeneralOptimizationDialog.btn.plotPath = Plot path +GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only) +GeneralOptimizationDialog.btn.save = Save path +GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file. +GeneralOptimizationDialog.btn.apply = Apply optimization +GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design +GeneralOptimizationDialog.btn.reset = Reset +GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design +GeneralOptimizationDialog.btn.close = Close +GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design +GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters. +GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters +GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run: +GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed +GeneralOptimizationDialog.undoText = Apply optimization +GeneralOptimizationDialog.basicSimulationName = Basic simulation +GeneralOptimizationDialog.noSimulationName = No simulation +GeneralOptimizationDialog.table.col.parameter = Parameter +GeneralOptimizationDialog.table.col.current = Current +GeneralOptimizationDialog.table.col.min = Minimum +GeneralOptimizationDialog.table.col.max = Maximum +GeneralOptimizationDialog.export.header = Include header line +GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions. +GeneralOptimizationDialog.export.stability = Stability + + +! Dialog for plotting optimization results +OptimizationPlotDialog.title = Optimization results +OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out +OptimizationPlotDialog.plot1d.title = Optimization result +OptimizationPlotDialog.plot1d.series = Optimization result +OptimizationPlotDialog.plot2d.title = Optimization path +OptimizationPlotDialog.plot2d.path = Optimization path +OptimizationPlotDialog.plot2d.evals = Evaluations +OptimizationPlotDialog.plot.ttip.stability = Stability: +OptimizationPlotDialog.plot.label.optimum = Optimum + +! Optimization parameters +MaximumAltitudeParameter.name = Apogee altitude +MaximumVelocityParameter.name = Maximum velocity +MaximumAccelerationParameter.name = Maximum acceleration +StabilityParameter.name = Stability +GroundHitVelocityParameter.name = Ground hit speed +LandingDistanceParameter.name = Landing distance +TotalFlightTimeParameter.name = Total flight time +DeploymentVelocityParameter.name = Velocity at parachute deployment + +