Added string to translate
This commit is contained in:
Boris du Reau
parent
97d1f19cd6
commit
7b352c1f7c
@ -1,3 +1,4 @@
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#
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# German base translation file
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#
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@ -5,6 +6,12 @@
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#
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# className.ComponantType.componantName
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#
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#
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# Text tokens within braces should not be translated, e.g.
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# "The file '{filename}' exists."
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# They are pieces that are inserted dynamically.
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#
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! Set to the name of the current translation file (used for debugging purposes)
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debug.currentFile = messages_de.properties
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@ -53,14 +60,6 @@ BasicFrame.SimpleFileFilter3 = RockSim Designs (*.rkt)
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BasicFrame.tab.Rocketdesign = Raketendesign
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BasicFrame.tab.Flightsim = Flugsimulation
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BasicFrame.title.Addnewcomp = Neue Komponente hinzufügen
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BasicFrame.item.Openrocketdesign = Raketendesign öffnen
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BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen
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BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern
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BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern
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BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken
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BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen
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BasicFrame.item.Quitprogram = Programm beenden
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BasicFrame.menu.Rocketedt = Rakete bearbeiten
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BasicFrame.dlg.lbl1 = Design '
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BasicFrame.dlg.lbl2 = ' ist nicht gespeichert.
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BasicFrame.dlg.lbl3 = Möchten Sie es speichern?
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@ -70,6 +69,15 @@ BasicFrame.WarningDialog.txt1 = Die folgenden Probleme w
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BasicFrame.WarningDialog.txt2 = Einige Designeigenschaften wurde eventuell nicht korrekt geladen.
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BasicFrame.WarningDialog.title = Warnungen während des Öffnens der Datei
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! General error messages used in multiple contexts
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error.fileExists.title = File exists
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error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?
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error.writing.title = Error writing file
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error.writing.desc = An error occurred while writing to the file:
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! Labels used in buttons of dialog windows
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button.ok = OK
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button.cancel = Abbrechen
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@ -110,6 +118,7 @@ PrintDialog.error.preview.title = Vorschau kann nicht ge
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PrintDialog.error.preview.desc1 = PDF-Vorschau kann nicht geöffnet werden
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PrintDialog.error.preview.desc2 = Bitte "Als PDF speichern" benutzen.
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!PrintSettingsDialog
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PrintSettingsDialog.title = Print settings
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PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:
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@ -135,6 +144,8 @@ bugreport.dlg.failedmsg2 = Bitte senden Sie den Bericht manuell an
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bugreport.dlg.failedmsg3 = Fehler beim Versenden des Berichts
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bugreport.reportDialog.txt = <html><b>Sie können eine Fehler in OpenRocket mitteilen, indem Sie das unten stehende Formular ausfüllen und abschicken.</b><br>Sie können Fehler mit angehängten Dateien auch auf der Projekt-Website mitteilen.
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bugreport.reportDialog.txt2 = Bitte beschreiben Sie kurz, was Sie getan haben, als der Fehler auftrat.</b>
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bugreport.dlg.provideDescription = Please provide a description of the bug first.
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bugreport.dlg.provideDescription.title = Bug description missing
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! Debug log dialog
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@ -239,7 +250,8 @@ pref.dlg.lbl.Totalimpulse = Gesamtimpuls:
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pref.dlg.lbl.Temperature = Temperatur:
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pref.dlg.lbl.Momentofinertia = Trägheitsmoment:
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pref.dlg.lbl.Pressure = Druck:
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pref.dlg.lbl.Stability = Stabilität
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pref.dlg.lbl.Stability = Stabilität:
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pref.dlg.lbl.FlightTime = Flight time:
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pref.dlg.lbl.effect1 = Die Änderungen werden wirksam, wenn Sie das nächste Mal ein Fenster öffnen.
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pref.dlg.lbl.Checkingupdates = Prüfe, ob Aktualisierungen verfügbar sind...
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pref.dlg.lbl.msg1 = Ein Fehler trat bei der Kommunikation mit dem Server auf.
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@ -248,12 +260,15 @@ pref.dlg.lbl.msg3 = Sie benutzen die neueste Version von OpenRocket.
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pref.dlg.lbl.msg4 = Keine Aktualisierungen verfügbar.
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pref.dlg.PrefChoiseSelector1 = Immer fragen
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pref.dlg.PrefChoiseSelector2 = in der Mitte einfügen
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a = an das Ende anhängen
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pref.dlg.PrefChoiseSelector3 = an das Ende anhängen
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pref.dlg.PrefBooleanSelector1 = Löschen
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pref.dlg.PrefBooleanSelector2 = Bestätigen
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pref.dlg.Add = Hinzufügen
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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.
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PreferencesDialog.lbl.language = Interface language:
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PreferencesDialog.languages.default = System default
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PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.
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! Simulation edit dialog
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simedtdlg.but.runsimulation = Simulation starten
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@ -290,6 +305,10 @@ simedtdlg.lbl.ttip.Pressure = Der Luftdruck am Startplatz.
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simedtdlg.lbl.Launchsite = Startplatz
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simedtdlg.lbl.Latitude = Breitengrad:
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simedtdlg.lbl.ttip.Latitude = <html>Der Breitengrad des Startplatzes beeinflusst die wirksame Gravitationskraft.<br>Positive Werte liegen auf der Nordhalbkugel, negative Werte auf der Südhalbkugel.
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simedtdlg.lbl.Longitude = Longitude:
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simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.
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simedtdlg.lbl.Altitude = Höhe:
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simedtdlg.lbl.ttip.Altitude = <html>Die Höhe des Startplatzes über Meeresniveau.<br>Die Höhe des Startplatzes beeinflusst die Position der Rakete im atmosphärischen Modell.
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simedtdlg.border.Launchrod = Startrampe
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@ -308,6 +327,8 @@ simedtdlg.lbl.ExtBarrowman = Barrowman (erweitert)
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simedtdlg.lbl.Simmethod = Simulationsmethode:
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simedtdlg.lbl.ttip.Simmethod1 = <html>Der Sechs-Freiheitsgradsimulator erlaubt der Rakete völlige Bewegungsfreiheit während des Fluges.<br>
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simedtdlg.lbl.ttip.Simmethod2 = Das Integrieren wird nach dem numerischen Runge-Kutta-Verfahren 4. Ordnung durchgeführt.
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simedtdlg.lbl.GeodeticMethod = Geodetic calculations:
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simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.
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simedtdlg.lbl.Timestep = Zeitschritt:
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simedtdlg.lbl.ttip.Timestep1 = <html>Die Zeit zwischen den Simulationsschritten.<br>Kleinere Schritte ergeben genauere Ergebnisse, die Simulationen dauern aber länger.<br>
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simedtdlg.lbl.ttip.Timestep2 = Die Berechnung der Simulation mit dem Verfahren 4. Ordnung liefert gute Ergebnisse mit Zeitschritten von
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@ -329,6 +350,14 @@ simedtdlg.IntensityDesc.High = Hoch
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simedtdlg.IntensityDesc.Veryhigh = Sehr hoch
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simedtdlg.IntensityDesc.Extreme = Extrem
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GeodeticComputationStrategy.none.name = None
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GeodeticComputationStrategy.none.desc = Perform no geodetic computations.
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GeodeticComputationStrategy.spherical.name = Spherical approximation
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GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.
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GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid
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GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.
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! Simulation Panel
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@ -400,6 +429,12 @@ SimExpPan.ExportingVar.desc3 = Variablen aus
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SimExpPan.Col.Variable = Variable
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SimExpPan.Col.Unit = Einheit
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CsvOptionPanel.separator.space = SPACE
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CsvOptionPanel.separator.tab = TAB
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! MotorPlot
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MotorPlot.title.Motorplot = Motorkurve
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MotorPlot.but.Select = Auswahl
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@ -493,6 +528,7 @@ componentanalysisdlg.println.settingnam = SETTING NAN VALUES
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componentanalysisdlg.lbl.reflenght = Referenzlänge:
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componentanalysisdlg.lbl.refarea = Referenzfläche:
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!componentanalysisdlg.But.close =Close
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componentanalysisdlg.TabStability.Col.Component = Component
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! Custom Material dialog
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custmatdlg.title.Custommaterial = Benutzerdefiniertes Material
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@ -623,6 +659,7 @@ CenteringRingCfg.tab.Generalproperties = Allgemeine Eigenschaften
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!ComponentConfigDialog
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ComponentCfgDlg.configuration = Konfiguration
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ComponentCfgDlg.configuration1 =
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ComponentCfgDlg.Modify = Verändern
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!EllipticalFinSetConfig
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@ -652,10 +689,12 @@ FreeformFinSetCfg.lbl.Posrelativeto = Position relativ zu:
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FreeformFinSetCfg.lbl.plus = plus
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FreeformFinSetCfg.lbl.FincrossSection = Querschnitt:
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FreeformFinSetCfg.lbl.Thickness = Wandstärke:
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FreeformFinSetCfg.lbl.Double-click = Double-click
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FreeformFinSetCfg.lbl.toedit = to edit
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FreeformFinSetCfg.lbl.Clickdrag = Click+drag: Add and move points
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FreeformFinSetCfg.lbl.Ctrlclick = Ctrl+click: Remove point
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! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
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FreeformFinSetConfig.lbl.doubleClick1 = Double-click
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FreeformFinSetConfig.lbl.doubleClick2 = to edit
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FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points
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FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point
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!InnerTubeConfig
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InnerTubeCfg.tab.Motor = Motor
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@ -905,33 +944,59 @@ PlotDialog.lbl.Chart = Klicken+ziehen: runter+rechts um hinein zu zoomen, hoch+l
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! "main" prefix is used for the main application dialog
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# FIXME: Rename the description keys
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main.menu.file = Datei
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main.menu.file.desc = File-handling related tasks
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main.menu.file.new = Neu
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main.menu.file.new.desc = Create a new rocket design
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main.menu.file.open = Öffnen..
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BasicFrame.item.Openrocketdesign = Raketendesign öffnen
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main.menu.file.openExample = Beispiel öffnen..
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BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen
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main.menu.file.save = Speichern
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BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern
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main.menu.file.saveAs = Speichern unter...
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BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern
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main.menu.file.print = Drucken / als PDF exportieren...
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BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken
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main.menu.file.close = Schließen
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BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen
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main.menu.file.quit = Beenden
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BasicFrame.item.Quitprogram = Programm beenden
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main.menu.edit = Bearbeiten
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BasicFrame.menu.Rocketedt = Rakete bearbeiten
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main.menu.edit.undo = Rückgängig
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main.menu.edit.undo.desc = Undo the previous operation
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main.menu.edit.redo = Wiederholen
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main.menu.edit.redo.desc = Redo the previously undone operation
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main.menu.edit.cut = Ausschneiden
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main.menu.edit.copy = Kopieren
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main.menu.edit.paste = Einfügen
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main.menu.edit.delete = Löschen
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main.menu.edit.resize = Scale...
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main.menu.edit.resize.desc = Scale parts of the rocket design
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main.menu.edit.preferences = Einstellungen
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main.menu.edit.preferences.desc = Setup the application preferences
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main.menu.analyze = Analysieren
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main.menu.analyze.desc = Rocket analysis
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main.menu.analyze.componentAnalysis = Komponente analysieren
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main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately
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main.menu.analyze.optimization = Rocket optimization
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main.menu.analyze.optimization.desc = General rocket design optimization
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main.menu.help = Hilfe
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main.menu.help.desc = Information about OpenRocket
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main.menu.help.license = Lizenz
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main.menu.help.license.desc = OpenRocket license information
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main.menu.help.bugReport = Fehlerbericht
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main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket
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main.menu.help.debugLog = Debug-Log
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main.menu.help.debugLog.desc = View the OpenRocket debug log
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main.menu.help.about = Über
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main.menu.help.about.desc = Copyright details about OpenRocket
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main.menu.debug = Debug
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main.menu.debug.whatisthismenu = Was macht diese Menü?
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@ -963,6 +1028,7 @@ Databases.materials.Spruce = Fichte
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Databases.materials.StyrofoamgenericEPS = Styropor (EPS)
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Databases.materials.StyrofoamBluefoamXPS = Styrodur (XPS)
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Databases.materials.Quantumtubing = Quantum tubing
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Databases.materials.BlueTube = Blue tube
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!SURFACE_MATERIAL
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Databases.materials.Ripstopnylon = Ripstop Nylon
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Databases.materials.Mylar = Mylar
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@ -1193,6 +1259,9 @@ FlightDataType.TYPE_AIR_PRESSURE = Luftdruck
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FlightDataType.TYPE_SPEED_OF_SOUND = Schallgeschwindigkeit
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FlightDataType.TYPE_TIME_STEP = Simulationsintervall
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FlightDataType.TYPE_COMPUTATION_TIME = Berechnnungszeit
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FlightDataType.TYPE_LATITUDE = Latitude
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FlightDataType.TYPE_LONGITUDE = Longitude
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FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration
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! PlotConfiguration
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PlotConfiguration.Verticalmotion = Vertikale Bewegung über Zeit
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@ -1214,6 +1283,27 @@ Warning.LISTENERS_AFFECTED = Simulationsempf
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Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Bergungssystem wurde ausgelöst während der Motor noch gebrannt hat.
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Warning.FILE_INVALID_PARAMETER = Ignoriere ungültigen Parameter.
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! Scale dialog
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ScaleDialog.lbl.scaleRocket = Entire rocket
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ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents
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ScaleDialog.lbl.scaleSelection = Only selected component
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ScaleDialog.title = Scale design
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ScaleDialog.lbl.scale = Scale:
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ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component
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ScaleDialog.lbl.scaling = Scaling to apply:
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ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.
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! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
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ScaleDialog.lbl.scaleFrom = Scale from
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ScaleDialog.lbl.scaleTo = to
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ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.
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ScaleDialog.checkbox.scaleMass = Update explicit mass values
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ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor
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ScaleDialog.button.scale = Scale
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ScaleDialog.undo.scaleRocket = Scale rocket
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ScaleDialog.undo.scaleComponent = Scale component
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ScaleDialog.undo.scaleComponents = Scale components
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!icons
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Icons.Undo = Undo
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Icons.Redo = Redo
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@ -1224,3 +1314,190 @@ OpenRocketPrintable.DesignReport = Design Report
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OpenRocketDocument.Redo = Redo
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OpenRocketDocument.Undo = Undo
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!EllipticalFinSet
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EllipticalFinSet.Ellipticalfinset = Elliptical fin set
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! Optimization
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! Modifiers
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optimization.modifier.nosecone.length = Length
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optimization.modifier.nosecone.length.desc = Optimize the nose cone length.
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optimization.modifier.nosecone.diameter = Diameter
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optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.
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optimization.modifier.nosecone.thickness = Thickness
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optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.
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optimization.modifier.nosecone.shapeparameter = Shape parameter
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optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.
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optimization.modifier.transition.length = Length
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optimization.modifier.transition.length.desc = Optimize the transition length.
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optimization.modifier.transition.forediameter = Fore diameter
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optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.
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optimization.modifier.transition.aftdiameter = Aft diameter
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optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.
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optimization.modifier.transition.thickness = Thickness
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optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.
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optimization.modifier.transition.shapeparameter = Shape parameter
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optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.
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optimization.modifier.bodytube.length = Length
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optimization.modifier.bodytube.length.desc = Optimize the body tube length.
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optimization.modifier.bodytube.outerDiameter = Outer diameter
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optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.
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optimization.modifier.bodytube.thickness = Thickness
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optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.
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optimization.modifier.trapezoidfinset.rootChord = Root chord
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optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).
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optimization.modifier.trapezoidfinset.tipChord = Tip chord
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optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).
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optimization.modifier.trapezoidfinset.sweep = Sweep
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optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).
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optimization.modifier.trapezoidfinset.height = Height
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optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.
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optimization.modifier.ellipticalfinset.length = Root chord
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optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.
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optimization.modifier.ellipticalfinset.height = Height
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optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.
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optimization.modifier.finset.cant = Cant angle
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optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.
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optimization.modifier.finset.position = Position
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optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.
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optimization.modifier.launchlug.length = Length
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optimization.modifier.launchlug.length.desc = Optimize the launch lug length.
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optimization.modifier.launchlug.outerDiameter = Outer diameter
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optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.
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optimization.modifier.launchlug.thickness = Thickness
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optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.
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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
|
||||
|
||||
|
||||
|
||||
@ -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 = <html><b>Puede realizar un informe de errores escribiendo en el formulario de abajo y enviándolo.</b><br>También puede informar de los errores adjuntando el archivo de su proyecto por email.
|
||||
!<html><b>Puede enviar un report de error en OpenRocket rellenando el formulario de abajo y enviándolo.</b><br>También puede reportar errores e incluir adjuntos sobre el proyecto de Web.
|
||||
bugreport.reportDialog.txt2 = <html><b>Por favor incluya una breve descripción de lo que estaba haciendo cuando ocurrió la excepción.</b>
|
||||
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 = <html>La latitud del lugar de lanzamiento afecta la atracción terrestre.<br>Los valores positivos se dan en el hemisferio Norte, los negativos en el hemisferio Sur.
|
||||
|
||||
simedtdlg.lbl.Longitude = Longitude:
|
||||
simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.
|
||||
|
||||
simedtdlg.lbl.Altitude = Altitud:
|
||||
simedtdlg.lbl.ttip.Altitude = <html>Los valores por encima del nivel del mar.<br>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 = <html>El simulador de seis-grados-de-libertad permite al cohete una total libertad durante el vuelo.<br>
|
||||
simedtdlg.lbl.ttip.Simmethod2 = La integración mejora usando un 4<sup>th</sup> 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 = <html>Tiempo entre etapas de simulación.<br>Un tiempo mas corto de etapa origina una simulación mas exacta pero mas lenta.<br>
|
||||
simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> 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 = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.
|
||||
GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid
|
||||
GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>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 = <html>La masa elegida no incluye los motores.<br>
|
||||
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 <b>Ojiva tangente</b>, mientras que un valor inferior a 1 produce una <b>Ojiva secante</b> con un perfil más afilado.
|
||||
Shape.Ogive.desc2 = Ojiva con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una <b>Ojiva tangente</b>, mientras que un valor inferior a 1 produce una <b>Ojiva secante</b> con un perfil más afilado.
|
||||
!Una ojiva con perfil de arco de circunferencia. El parámetro de forma de valor 1 produce una <b>Tangente a la ojiva</b>, Que tiene una transición suave al fuselaje, produce un valor menor que 1 <b>Secante a la ojiva</b>.
|
||||
Shape.Ellipsoid = Elipsoide
|
||||
Shape.Ellipsoid.desc1 = Ojiva con perfil de media elipse. Por defecto, una elipse de <i>longitud</i> igual al triple de su <i>diámetro</i>.
|
||||
!Una ojiva elipsoidal tiene un perfil de media elipse con el eje mayor de longitud 2&veces;<i>Longitud</i> y <i>Diámetro</i>.
|
||||
Shape.Ellipsoid.desc2 = Ojiva con perfil de media elipse. Por defecto, una elipse de <i>longitud</i> igual al triple de su <i>diámetro</i>.
|
||||
!Una ojiva elipsoidal tiene un perfil de media elipse con el eje mayor de longitud 2&veces;<i>Longitud</i> y <i>Diámetro</i>. 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 <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
|
||||
!Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.
|
||||
|
||||
Shape.Powerseries.desc1 = Ojiva cuyo perfil es una curva obtenida a partir de una función potencial f(<i>x</i>)<sup><i>k</i></sup>. Un valor de forma k=0.5 produce una ojiva con perfil de parábola, para k=0.75 se produce una ojiva con <b>perfil potencial</b>, y para k=1 se produce una ojiva con perfil recto u <b>Ojiva cónica</b>.
|
||||
!Shape.Powerseries.desc1 = Una serie de ojivas potentes tiene un perfil de<i>Radio</i> &veces; (<i>x</i> / <i>Longitud</i>)<sup><i>k</i></sup> donde <i>k</i> es el parámetro de forma. Para <i>k</i>=0.5 este es un <b>\u00BD-potencia</b> o <b>parabólico</b> ojiva, para <i>k</i>=0.75 un <b>\u00BE-potencia</b>, y para <i>k</i>=1 a <b>cónica</b> ojiva.
|
||||
Shape.Powerseries.desc2 = Una serie de transiciones potentes tiene un perfil de <i>Radio</i> &veces; (<i>x</i> / <i>Longitud</i>)<sup><i>k</i></sup> donde <i>k</i> es el parámetro de forma. Para <i>k</i>=0.5 la transición es <b>\u00BD-potencia</b> o <b>parabólica</b>, para <i>k</i>=0.75 a <b>\u00BE-potencia</b>, y para <i>k</i>=1 <b>cónica</b>.
|
||||
Shape.Parabolicseries = Serie parabólica
|
||||
Shape.Parabolicseries.desc1 = Ojiva con perfil de arco de parábola. Un valor de forma igual a 1 produce una <b>Ojiva tangente</b>, un valor igual a 0.75 produce una <b>parábola de 3/4</b>, un valor igual a 0.5 produce una <b>parábola de 1/2</b>, y un valor igual a 0 produce una perfil recto u <b>Ojiva cónica</b>.
|
||||
!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 <b>full parábola</b> que es tangente a el body tubo, 0.75 produces a <b>3/4 parábola</b>, 0.5 procudes a <b>1/2 parábola</b> y 0 produces a <b>cónico</b> 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 <b>full parábola</b> que es tangente a el body tubo at el aft extremo, 0.75 produces a <b>3/4 parábola</b>, 0.5 procudes a <b>1/2 parábola</b> y 0 produces a <b>cónico</b> 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 <b>Ojiva LD Haack</b> u <b>Ojiva Von Karman</b> que minimiza el arrastre aerodinámico para una determinada longitud y diámetro de la base, mientras que un valor igual a 0.333 produce una <b>Ojiva LV-Haack</b> 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 <b>LD-Haack</b> o <b>Von Karman</b> ojiva , que minimizas drag para fijado longitud y diámetro, mientras a valor de 0.333 produces un <b>LV-Haack</b> ojiva , que minimizas drag para fijado longitud y volumen.
|
||||
Shape.Haackseries.desc2 = The Haack series <i>ojiva </i> 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 <b>LD-Haack</b> o <b>Von Karman</b> forma, mientras a valor de 0.333 produces un <b>LV-Haack</b> 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
|
||||
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
|
||||
|
||||
|
||||
|
||||
Loading…
x
Reference in New Issue
Block a user