+\r
+#\r
+# German base translation file\r
+#\r
+# Should you need to add new logical keys here is the proposed method\r
+#\r
+# className.ComponantType.componantName\r
+#\r
+#\r
+# Text tokens within braces should not be translated, e.g.\r
+# "The file '{filename}' exists."\r
+# They are pieces that are inserted dynamically.\r
+#\r
+\r
+\r
! Set to the name of the current translation file (used for debugging purposes)\r
debug.currentFile = messages_de.properties\r
\r
BasicFrame.tab.Rocketdesign = Raketendesign\r
BasicFrame.tab.Flightsim = Flugsimulation\r
BasicFrame.title.Addnewcomp = Neue Komponente hinzufügen\r
-BasicFrame.item.Openrocketdesign = Raketendesign öffnen\r
-BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen\r
-BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern\r
-BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern\r
-BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken\r
-BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen\r
-BasicFrame.item.Quitprogram = Programm beenden\r
-BasicFrame.menu.Rocketedt = Rakete bearbeiten\r
BasicFrame.dlg.lbl1 = Design '\r
-BasicFrame.dlg.lbl2 = ist nicht gespeichert.\r
+BasicFrame.dlg.lbl2 = ' ist nicht gespeichert.\r
BasicFrame.dlg.lbl3 = Möchten Sie es speichern?\r
BasicFrame.dlg.title = Design nicht gespeichert\r
-BasicFrame.StageName.Sustainer = Sustainer\r
+BasicFrame.StageName.Sustainer = Hauptstufe\r
BasicFrame.WarningDialog.txt1 = Die folgenden Probleme würden beim Öffnen festgestellt\r
BasicFrame.WarningDialog.txt2 = Einige Designeigenschaften wurde eventuell nicht korrekt geladen.\r
BasicFrame.WarningDialog.title = Warnungen während des Öffnens der Datei\r
\r
+\r
+! General error messages used in multiple contexts\r
+error.fileExists.title = File exists\r
+error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?\r
+\r
+error.writing.title = Error writing file\r
+error.writing.desc = An error occurred while writing to the file:\r
+\r
+\r
! Labels used in buttons of dialog windows\r
button.ok = OK\r
button.cancel = Abbrechen\r
dlg.but.cancel = Abbrechen\r
dlg.but.close = Schließen\r
\r
+\r
+! General file type names\r
+filetypes.pdf = PDF files\r
+\r
+\r
! About Dialog\r
-about.dlg.but.close = Schließen\r
-about.dlg.lbl.translation = Ins Deutsche übersetzt von Stefan Lobas (ERIG e.V.)\r
-about.dlg.lbl.transwebsite = http://www.er-ig.de/\r
+AboutDialog.lbl.version = Version\r
+! The texts below provide additional credits for the translation maintainer\r
+! - In AboutDialog.lbl.translation replace "English" with the current language.\r
+! - AboutDialog.lbl.translator is the translator / group name (may be empty)\r
+! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)\r
+! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)\r
+AboutDialog.lbl.translation = Ins Deutsche übersetzt von:\r
+AboutDialog.lbl.translator = Stefan Lobas (ERIG e.V.)\r
+AboutDialog.lbl.translatorWebsite = http://www.er-ig.de/\r
+AboutDialog.lbl.translatorIcon = ERIG_Logo-small.png\r
+\r
+\r
+! Print dialog\r
+PrintDialog.title = Drucken oder exportieren\r
+PrintDialog.but.previewAndPrint = Vorschau & Drucken\r
+PrintDialog.checkbox.showByStage = In Stufen anzeigen\r
+PrintDialog.lbl.selectElements = Elemente auswählen, die berücksichtigt werden sollen:\r
+printdlg.but.saveaspdf = Als PDF speichern\r
+printdlg.but.preview = Vorschau\r
+printdlg.but.settings = Einstellungen\r
+PrintDialog.error.preview.title = Vorschau kann nicht geöffnet werden\r
+PrintDialog.error.preview.desc1 = PDF-Vorschau kann nicht geöffnet werden\r
+PrintDialog.error.preview.desc2 = Bitte "Als PDF speichern" benutzen.\r
+\r
+\r
+!PrintSettingsDialog\r
+PrintSettingsDialog.title = Print settings\r
+PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:\r
+PrintSettingsDialog.lbl.Templatebordercolor = Template border color:\r
+PrintSettingsDialog.lbl.Papersize = Paper size:\r
+PrintSettingsDialog.lbl.Paperorientation = Paper orientation:\r
+PrintSettingsDialog.but.Reset = Reset\r
+PrintSettingsDialog.but.Close = Close\r
+\r
\r
! Bug Report dialog\r
bugreport.dlg.title = Fehlerbericht\r
bugreport.dlg.failedmsg3 = Fehler beim Versenden des Berichts\r
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.\r
bugreport.reportDialog.txt2 = Bitte beschreiben Sie kurz, was Sie getan haben, als der Fehler auftrat.</b>\r
+bugreport.dlg.provideDescription = Please provide a description of the bug first.\r
+bugreport.dlg.provideDescription.title = Bug description missing\r
\r
\r
! Debug log dialog\r
debuglogdlg.lbl.Loglinenbr = Log-Zeilennummer\r
debuglogdlg.lbl.Time = Zeit:\r
debuglogdlg.lbl.Level = Level:\r
+debuglogdlg.lbl.Location = Location:\r
+debuglogdlg.lbl.Logmessage = Log message:\r
+debuglogdlg.lbl.Stacktrace = Stack trace:\r
\r
\r
! Edit Motor configuration dialog\r
exdesigndlg.lbl.Exampledesignsnotfound = Beispieldesigns konnten nicht gefunden werden.\r
exdesigndlg.lbl.Examplesnotfound = Beispieldesign konnten nicht gefunden werden\r
\r
-! Print panel dialog\r
-printdlg.but.saveaspdf = Als PDF speichern\r
-printdlg.but.preview = Vorschau\r
-printdlg.but.settings = Einstellungen\r
\r
! Material edit panel\r
matedtpan.but.new = Neu\r
matedtpan.but.ttip.revertall = Alle benutzerdefinierten Materialien löschen\r
matedtpan.title.Deletealluser-defined = Alle benutzerdefinierten Materialien löschen?\r
matedtpan.title.Revertall = Alle löschen?\r
-matedtpan.lbl.edtmaterials = <html><i>Das Bearbeiten der Materialien beeinflusst keine bereits existierenden Raketendesigns.</i>\r
+matedtpan.lbl.edtmaterials = Das Bearbeiten der Materialien beeinflusst keine bereits existierenden Raketendesigns.\r
\r
!MaterialModel\r
MaterialModel.title.Material = Material\r
pref.dlg.lbl.Temperature = Temperatur:\r
pref.dlg.lbl.Momentofinertia = Trägheitsmoment:\r
pref.dlg.lbl.Pressure = Druck:\r
-pref.dlg.lbl.Stability = Stabilität\r
+pref.dlg.lbl.Stability = Stabilität:\r
+pref.dlg.lbl.FlightTime = Flight time:\r
pref.dlg.lbl.effect1 = Die Änderungen werden wirksam, wenn Sie das nächste Mal ein Fenster öffnen.\r
pref.dlg.lbl.Checkingupdates = Prüfe, ob Aktualisierungen verfügbar sind...\r
pref.dlg.lbl.msg1 = Ein Fehler trat bei der Kommunikation mit dem Server auf.\r
pref.dlg.lbl.msg4 = Keine Aktualisierungen verfügbar.\r
pref.dlg.PrefChoiseSelector1 = Immer fragen\r
pref.dlg.PrefChoiseSelector2 = in der Mitte einfügen\r
-a = an das Ende anhängen\r
+pref.dlg.PrefChoiseSelector3 = an das Ende anhängen\r
pref.dlg.PrefBooleanSelector1 = Löschen\r
pref.dlg.PrefBooleanSelector2 = Bestätigen\r
pref.dlg.Add = Hinzufügen\r
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.\r
\r
+PreferencesDialog.lbl.language = Interface language:\r
+PreferencesDialog.languages.default = System default\r
+PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.\r
\r
! Simulation edit dialog\r
simedtdlg.but.runsimulation = Simulation starten\r
simedtdlg.lbl.Launchsite = Startplatz\r
simedtdlg.lbl.Latitude = Breitengrad:\r
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.\r
+\r
+simedtdlg.lbl.Longitude = Longitude:\r
+simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.\r
+\r
simedtdlg.lbl.Altitude = Höhe:\r
simedtdlg.lbl.ttip.Altitude = <html>Die Höhe des Startplatzes über Meeresniveau.<br>Die Höhe des Startplatzes beeinflusst die Position der Rakete im atmosphärischen Modell.\r
simedtdlg.border.Launchrod = Startrampe\r
simedtdlg.lbl.Simmethod = Simulationsmethode:\r
simedtdlg.lbl.ttip.Simmethod1 = <html>Der Sechs-Freiheitsgradsimulator erlaubt der Rakete völlige Bewegungsfreiheit während des Fluges.<br>\r
simedtdlg.lbl.ttip.Simmethod2 = Das Integrieren wird nach dem numerischen Runge-Kutta-Verfahren 4. Ordnung durchgeführt.\r
+simedtdlg.lbl.GeodeticMethod = Geodetic calculations:\r
+simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.\r
simedtdlg.lbl.Timestep = Zeitschritt:\r
simedtdlg.lbl.ttip.Timestep1 = <html>Die Zeit zwischen den Simulationsschritten.<br>Kleinere Schritte ergeben genauere Ergebnisse, die Simulationen dauern aber länger.<br>\r
simedtdlg.lbl.ttip.Timestep2 = Die Berechnung der Simulation mit dem Verfahren 4. Ordnung liefert gute Ergebnisse mit Zeitschritten von\r
simedtdlg.IntensityDesc.Veryhigh = Sehr hoch\r
simedtdlg.IntensityDesc.Extreme = Extrem\r
\r
+GeodeticComputationStrategy.none.name = None\r
+GeodeticComputationStrategy.none.desc = Perform no geodetic computations.\r
+GeodeticComputationStrategy.spherical.name = Spherical approximation\r
+GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.\r
+GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid\r
+GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.\r
+\r
+\r
\r
\r
! Simulation Panel\r
SimExpPan.Col.Variable = Variable\r
SimExpPan.Col.Unit = Einheit\r
\r
+\r
+CsvOptionPanel.separator.space = SPACE\r
+CsvOptionPanel.separator.tab = TAB\r
+\r
+\r
+\r
! MotorPlot\r
MotorPlot.title.Motorplot = Motorkurve\r
MotorPlot.but.Select = Auswahl\r
compaddbuttons.Massobjects = Massenobjekte\r
compaddbuttons.Parachute = Fallschirm\r
compaddbuttons.Streamer = Strömer\r
-compaddbuttons.Shockcord = Gummiseil\r
+compaddbuttons.Shockcord = Gummiband\r
compaddbuttons.Masscomponent = Massen-\nobjekt\r
compaddbuttons.Donotaskmeagain = Nicht wieder fragen\r
compaddbuttons.Selectcomppos = Komponentenposition auswählen\r
componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>\r
componentanalysisdlg.dragTableModel.Col.friction = <html>Reibung C<sub>D</sub>\r
componentanalysisdlg.dragTableModel.Col.total = <html>Gesamt C<sub>D</sub>\r
-componentanalysisdlg.dragTabchar = Drag characteristics\r
-componentanalysisdlg.dragTabchar.ttip = Drag characteristics\r
+componentanalysisdlg.dragTabchar = Luftwiderstand\r
+componentanalysisdlg.dragTabchar.ttip = Luftwiderstands-Eigenschaften\r
componentanalysisdlg.rollTableModel.Col.component = Komponente\r
componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient\r
componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient\r
componentanalysisdlg.lbl.reflenght = Referenzlänge:\r
componentanalysisdlg.lbl.refarea = Referenzfläche:\r
!componentanalysisdlg.But.close =Close\r
+componentanalysisdlg.TabStability.Col.Component = Component\r
\r
! Custom Material dialog\r
custmatdlg.title.Custommaterial = Benutzerdefiniertes Material\r
RocketCfg.lbl.Material = Material:\r
\r
! ShockCordConfig\r
-ShockCordCfg.lbl.Shockcordlength = Gummiseillänge\r
+ShockCordCfg.lbl.Shockcordlength = Gummibandlänge\r
\r
! RocketComponentConfig\r
RocketCompCfg.lbl.Componentname = Komponentenname:\r
\r
!ComponentConfigDialog\r
ComponentCfgDlg.configuration = Konfiguration\r
+ComponentCfgDlg.configuration1 =\r
ComponentCfgDlg.Modify = Verändern\r
\r
!EllipticalFinSetConfig\r
FreeformFinSetCfg.lbl.plus = plus\r
FreeformFinSetCfg.lbl.FincrossSection = Querschnitt:\r
FreeformFinSetCfg.lbl.Thickness = Wandstärke:\r
+! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle\r
+FreeformFinSetConfig.lbl.doubleClick1 = Double-click\r
+FreeformFinSetConfig.lbl.doubleClick2 = to edit\r
+FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points\r
+FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point\r
+\r
\r
!InnerTubeConfig\r
InnerTubeCfg.tab.Motor = Motor\r
ParachuteCfg.lbl.Radialdistance = Radialer Abstand:\r
ParachuteCfg.lbl.Radialdirection = radiale Richtung:\r
ParachuteCfg.but.Reset = Zurücksetzen\r
+ParachuteCfg.lbl.plusdelay = plus\r
\r
! ShockCordConfig \r
-ShockCordCfg.lbl.Shockcordlength = Länge des Gummiseils\r
-ShockCordCfg.lbl.Shockcordmaterial = Material des Gummiseils:\r
+ShockCordCfg.lbl.Shockcordlength = Länge des Gummibands\r
+ShockCordCfg.lbl.Shockcordmaterial = Material des Gummibands:\r
ShockCordCfg.lbl.Posrelativeto = Position relativ zu:\r
ShockCordCfg.lbl.plus = plus\r
ShockCordCfg.lbl.Packedlength = gepackte Länge:\r
StreamerCfg.lbl.Radialdistance = Radialer Abstand:\r
StreamerCfg.lbl.Radialdirection = radiale Richtung:\r
StreamerCfg.but.Reset = Zurücksetzen\r
+StreamerCfg.lbl.plusdelay = plus\r
\r
! ThicknessRingComponentConfig\r
ThicknessRingCompCfg.tab.Outerdiam = Außendurchmesser:\r
TrapezoidFinSetCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
\r
!MotorConfigurationModel\r
-MotorCfgModel.Editcfg = Konfigurationen bearbeiten\r
+MotorCfgModel.Editcfg = Konfiguration bearbeiten\r
\r
! StorageOptionChooser\r
StorageOptChooser.lbl.Simdatatostore = Zu speichernde Simulationsdaten:\r
\r
! "main" prefix is used for the main application dialog\r
\r
+# FIXME: Rename the description keys \r
+\r
main.menu.file = Datei\r
+main.menu.file.desc = File-handling related tasks\r
main.menu.file.new = Neu\r
+main.menu.file.new.desc = Create a new rocket design\r
main.menu.file.open = Öffnen..\r
+BasicFrame.item.Openrocketdesign = Raketendesign öffnen\r
main.menu.file.openExample = Beispiel öffnen..\r
+BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen\r
main.menu.file.save = Speichern\r
+BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern\r
main.menu.file.saveAs = Speichern unter...\r
-main.menu.file.print = Drucken...\r
+BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern\r
+main.menu.file.print = Drucken / als PDF exportieren...\r
+BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken\r
main.menu.file.close = Schließen\r
+BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen\r
main.menu.file.quit = Beenden\r
+BasicFrame.item.Quitprogram = Programm beenden\r
\r
main.menu.edit = Bearbeiten\r
+BasicFrame.menu.Rocketedt = Rakete bearbeiten\r
main.menu.edit.undo = Rückgängig\r
+main.menu.edit.undo.desc = Undo the previous operation\r
main.menu.edit.redo = Wiederholen\r
+main.menu.edit.redo.desc = Redo the previously undone operation\r
main.menu.edit.cut = Ausschneiden\r
main.menu.edit.copy = Kopieren\r
main.menu.edit.paste = Einfügen\r
main.menu.edit.delete = Löschen\r
+main.menu.edit.resize = Scale...\r
+main.menu.edit.resize.desc = Scale parts of the rocket design\r
main.menu.edit.preferences = Einstellungen\r
+main.menu.edit.preferences.desc = Setup the application preferences\r
\r
main.menu.analyze = Analysieren\r
+main.menu.analyze.desc = Rocket analysis\r
main.menu.analyze.componentAnalysis = Komponente analysieren\r
+main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately\r
+main.menu.analyze.optimization = Rocket optimization\r
+main.menu.analyze.optimization.desc = General rocket design optimization\r
\r
main.menu.help = Hilfe\r
+main.menu.help.desc = Information about OpenRocket\r
main.menu.help.license = Lizenz\r
+main.menu.help.license.desc = OpenRocket license information\r
main.menu.help.bugReport = Fehlerbericht\r
+main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket\r
main.menu.help.debugLog = Debug-Log\r
+main.menu.help.debugLog.desc = View the OpenRocket debug log\r
main.menu.help.about = Über\r
+main.menu.help.about.desc = Copyright details about OpenRocket\r
\r
main.menu.debug = Debug\r
main.menu.debug.whatisthismenu = Was macht diese Menü?\r
Databases.materials.StyrofoamgenericEPS = Styropor (EPS)\r
Databases.materials.StyrofoamBluefoamXPS = Styrodur (XPS)\r
Databases.materials.Quantumtubing = Quantum tubing\r
+Databases.materials.BlueTube = Blue tube\r
!SURFACE_MATERIAL\r
Databases.materials.Ripstopnylon = Ripstop Nylon\r
Databases.materials.Mylar = Mylar\r
Shape.Ellipsoid.desc1 = Eine ellipsoide Spitze hat ein Profil einer Halbellipse mit der einer Hauptachsenlänge von 2×<i>Länge</i> und <i>Durchmesser</i> \r
Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius. \r
Shape.Powerseries = Power series\r
-Shape.Powerseries.descA1 = 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>\r
-Shape.Powerseries.descA2 = -power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\r
-Shape.Powerseries.descA3 = -power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.\r
-Shape.Powerseries.descB1 = 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>\r
-Shape.Powerseries.descB2 = -power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\r
-Shape.Powerseries.descB3 = -power</b>, and for <i>k</i>=1 <b>conical</b>.\r
+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.\r
+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>.\r
Shape.Parabolicseries = Parabolic series\r
Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.\r
Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.\r
! Parachute\r
Parachute.Parachute = Fallschirm\r
! ShockCord\r
-ShockCord.ShockCord = Gummiseil\r
+ShockCord.ShockCord = Gummiband\r
! Bulkhead\r
Bulkhead.Bulkhead = Schott\r
\r
ComponentIcons.Engineblock = Motorhalterung\r
ComponentIcons.Parachute = Fallschirm\r
ComponentIcons.Streamer = Strömer\r
-ComponentIcons.Shockcord = Gummiseil\r
+ComponentIcons.Shockcord = Gummiband\r
ComponentIcons.Masscomponent = Masse\r
ComponentIcons.disabled = (deaktiviert)\r
\r
FlightDataType.TYPE_AIR_TEMPERATURE = Lufttemperatur\r
FlightDataType.TYPE_AIR_PRESSURE = Luftdruck\r
FlightDataType.TYPE_SPEED_OF_SOUND = Schallgeschwindigkeit\r
-FlightDataType.TYPE_TIME_STEP = Simulationszeitschritt\r
+FlightDataType.TYPE_TIME_STEP = Simulationsintervall\r
FlightDataType.TYPE_COMPUTATION_TIME = Berechnnungszeit\r
+FlightDataType.TYPE_LATITUDE = Latitude\r
+FlightDataType.TYPE_LONGITUDE = Longitude\r
+FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration\r
\r
! PlotConfiguration\r
PlotConfiguration.Verticalmotion = Vertikale Bewegung über Zeit\r
Warning.LISTENERS_AFFECTED = Simulationsempfänger haben die Simulation beeinflusst.\r
Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Bergungssystem wurde ausgelöst während der Motor noch gebrannt hat.\r
Warning.FILE_INVALID_PARAMETER = Ignoriere ungültigen Parameter.\r
+\r
+\r
+! Scale dialog\r
+ScaleDialog.lbl.scaleRocket = Entire rocket\r
+ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents\r
+ScaleDialog.lbl.scaleSelection = Only selected component\r
+ScaleDialog.title = Scale design\r
+ScaleDialog.lbl.scale = Scale:\r
+ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component\r
+ScaleDialog.lbl.scaling = Scaling to apply:\r
+ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.\r
+! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"\r
+ScaleDialog.lbl.scaleFrom = Scale from\r
+ScaleDialog.lbl.scaleTo = to\r
+ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.\r
+ScaleDialog.checkbox.scaleMass = Update explicit mass values\r
+ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor\r
+ScaleDialog.button.scale = Scale\r
+ScaleDialog.undo.scaleRocket = Scale rocket\r
+ScaleDialog.undo.scaleComponent = Scale component\r
+ScaleDialog.undo.scaleComponents = Scale components\r
+\r
+!icons\r
+Icons.Undo = Undo\r
+Icons.Redo = Redo\r
+\r
+OpenRocketPrintable.Partsdetail = Parts detail\r
+OpenRocketPrintable.Fintemplates = Fin templates\r
+OpenRocketPrintable.DesignReport = Design Report\r
+\r
+OpenRocketDocument.Redo = Redo\r
+OpenRocketDocument.Undo = Undo\r
+\r
+!EllipticalFinSet\r
+EllipticalFinSet.Ellipticalfinset = Elliptical fin set\r
+\r
+! Optimization\r
+\r
+! Modifiers\r
+\r
+optimization.modifier.nosecone.length = Length\r
+optimization.modifier.nosecone.length.desc = Optimize the nose cone length.\r
+optimization.modifier.nosecone.diameter = Diameter\r
+optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.\r
+optimization.modifier.nosecone.thickness = Thickness\r
+optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.\r
+optimization.modifier.nosecone.shapeparameter = Shape parameter\r
+optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.\r
+\r
+optimization.modifier.transition.length = Length\r
+optimization.modifier.transition.length.desc = Optimize the transition length.\r
+optimization.modifier.transition.forediameter = Fore diameter\r
+optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.\r
+optimization.modifier.transition.aftdiameter = Aft diameter\r
+optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.\r
+optimization.modifier.transition.thickness = Thickness\r
+optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.\r
+optimization.modifier.transition.shapeparameter = Shape parameter\r
+optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.\r
+\r
+optimization.modifier.bodytube.length = Length\r
+optimization.modifier.bodytube.length.desc = Optimize the body tube length.\r
+optimization.modifier.bodytube.outerDiameter = Outer diameter\r
+optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.\r
+optimization.modifier.bodytube.thickness = Thickness\r
+optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.\r
+\r
+optimization.modifier.trapezoidfinset.rootChord = Root chord\r
+optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).\r
+optimization.modifier.trapezoidfinset.tipChord = Tip chord\r
+optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).\r
+optimization.modifier.trapezoidfinset.sweep = Sweep\r
+optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).\r
+optimization.modifier.trapezoidfinset.height = Height\r
+optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
+\r
+optimization.modifier.ellipticalfinset.length = Root chord\r
+optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.\r
+optimization.modifier.ellipticalfinset.height = Height\r
+optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
+\r
+optimization.modifier.finset.cant = Cant angle\r
+optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.\r
+optimization.modifier.finset.position = Position\r
+optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.\r
+\r
+optimization.modifier.launchlug.length = Length\r
+optimization.modifier.launchlug.length.desc = Optimize the launch lug length.\r
+optimization.modifier.launchlug.outerDiameter = Outer diameter\r
+optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.\r
+optimization.modifier.launchlug.thickness = Thickness\r
+optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.\r
+optimization.modifier.launchlug.position = Position\r
+optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.\r
+\r
+\r
+optimization.modifier.internalcomponent.position = Position\r
+optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.\r
+\r
+optimization.modifier.masscomponent.mass = Mass\r
+optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.\r
+\r
+optimization.modifier.parachute.diameter = Diameter\r
+optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.\r
+optimization.modifier.parachute.coefficient = Drag coefficient\r
+optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.\r
+\r
+optimization.modifier.streamer.length = Length\r
+optimization.modifier.streamer.length.desc = Optimize the length of the streamer.\r
+optimization.modifier.streamer.width = Width\r
+optimization.modifier.streamer.width.desc = Optimize the width of the streamer.\r
+optimization.modifier.streamer.aspectRatio = Aspect ratio\r
+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.\r
+optimization.modifier.streamer.coefficient = Drag coefficient\r
+optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.\r
+\r
+optimization.modifier.recoverydevice.deployDelay = Deployment delay\r
+optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.\r
+optimization.modifier.recoverydevice.deployAltitude = Deployment altitude\r
+optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.\r
+\r
+optimization.modifier.rocketcomponent.overrideMass = Override mass\r
+optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.\r
+optimization.modifier.rocketcomponent.overrideCG = Override CG\r
+optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.\r
+\r
+optimization.modifier.motormount.overhang = Motor overhang\r
+optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.\r
+optimization.modifier.motormount.delay = Motor ignition delay\r
+optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.\r
+\r
+\r
+\r
+\r
+! General rocket design optimization dialog\r
+\r
+GeneralOptimizationDialog.title = Rocket optimization\r
+GeneralOptimizationDialog.goal.maximize = Maximize value\r
+GeneralOptimizationDialog.goal.minimize = Minimize value\r
+GeneralOptimizationDialog.goal.seek = Seek value of\r
+GeneralOptimizationDialog.btn.start = Start optimization\r
+GeneralOptimizationDialog.btn.stop = Stop optimization\r
+GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:\r
+GeneralOptimizationDialog.btn.add = Add\r
+GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization\r
+GeneralOptimizationDialog.btn.remove = Remove\r
+GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization\r
+GeneralOptimizationDialog.btn.removeAll = Remove all\r
+GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization\r
+GeneralOptimizationDialog.lbl.availableParams = Available parameters:\r
+GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options\r
+GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:\r
+GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize\r
+GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:\r
+GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized\r
+GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:\r
+GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization\r
+GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek\r
+GeneralOptimizationDialog.lbl.requireStability = Required stability\r
+GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:\r
+GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design\r
+GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:\r
+GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design\r
+GeneralOptimizationDialog.status.bestValue = Best value:\r
+GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.\r
+GeneralOptimizationDialog.status.stepCount = Step count:\r
+GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.\r
+GeneralOptimizationDialog.status.evalCount = Evaluations:\r
+GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.\r
+GeneralOptimizationDialog.status.stepSize = Step size:\r
+GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)\r
+GeneralOptimizationDialog.btn.plotPath = Plot path\r
+GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)\r
+GeneralOptimizationDialog.btn.save = Save path\r
+GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.\r
+GeneralOptimizationDialog.btn.apply = Apply optimization\r
+GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design\r
+GeneralOptimizationDialog.btn.reset = Reset\r
+GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design\r
+GeneralOptimizationDialog.btn.close = Close\r
+GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design\r
+GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.\r
+GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters\r
+GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:\r
+GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed\r
+GeneralOptimizationDialog.undoText = Apply optimization\r
+GeneralOptimizationDialog.basicSimulationName = Basic simulation\r
+GeneralOptimizationDialog.noSimulationName = No simulation\r
+GeneralOptimizationDialog.table.col.parameter = Parameter\r
+GeneralOptimizationDialog.table.col.current = Current\r
+GeneralOptimizationDialog.table.col.min = Minimum\r
+GeneralOptimizationDialog.table.col.max = Maximum\r
+GeneralOptimizationDialog.export.header = Include header line\r
+GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.\r
+GeneralOptimizationDialog.export.stability = Stability\r
+\r
+\r
+! Dialog for plotting optimization results\r
+OptimizationPlotDialog.title = Optimization results\r
+OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out\r
+OptimizationPlotDialog.plot1d.title = Optimization result\r
+OptimizationPlotDialog.plot1d.series = Optimization result\r
+OptimizationPlotDialog.plot2d.title = Optimization path\r
+OptimizationPlotDialog.plot2d.path = Optimization path\r
+OptimizationPlotDialog.plot2d.evals = Evaluations\r
+OptimizationPlotDialog.plot.ttip.stability = Stability:\r
+OptimizationPlotDialog.plot.label.optimum = Optimum\r
+\r
+! Optimization parameters\r
+MaximumAltitudeParameter.name = Apogee altitude\r
+MaximumVelocityParameter.name = Maximum velocity\r
+MaximumAccelerationParameter.name = Maximum acceleration\r
+StabilityParameter.name = Stability\r
+GroundHitVelocityParameter.name = Ground hit speed\r
+LandingDistanceParameter.name = Landing distance\r
+TotalFlightTimeParameter.name = Total flight time\r
+DeploymentVelocityParameter.name = Velocity at parachute deployment\r
+\r
+\r
projects / debian / openrocket / blobdiff