#\r
# French base translation file\r
# Translated by Tripoli France\r
-\r
+# Should you need to add new logical keys here is the proposed method\r
+#\r
+# className.ComponentType.componentName\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
! Set to the name of the current translation file (used for debugging purposes)\r
debug.currentFile = messages_fr.properties\r
BasicFrame.tab.Rocketdesign = Projet fusée\r
BasicFrame.tab.Flightsim = Simulations de vol\r
BasicFrame.title.Addnewcomp = Ajouter une nouvelle pièce\r
-BasicFrame.item.Openrocketdesign = Ouvrir un projet fusée\r
-BasicFrame.item.Openexamplerocketdesign = Ouvrir un exemple de projet fusée\r
-BasicFrame.item.SavecurRocketdesign = Sauvegarder le projet fusée courant\r
-BasicFrame.item.SavecurRocketdesnewfile = Sauvegarder le projet fusée courant dans un nouveau fichier\r
-BasicFrame.item.Printpart = Imprimer la liste des pièces et les modèles d'ailerons\r
-BasicFrame.item.Closedesign = Fermer le projet fusée courant\r
-BasicFrame.item.Quitprogram = Quitter le programme\r
-BasicFrame.menu.Rocketedt = Modification de la fusée\r
+!BasicFrame.item.Openrocketdesign = Ouvrir un projet fusée\r
+!BasicFrame.item.Openexamplerocketdesign = Ouvrir un exemple de projet fusée\r
+!BasicFrame.item.SavecurRocketdesign = Sauvegarder le projet fusée courant\r
+!BasicFrame.item.SavecurRocketdesnewfile = Sauvegarder le projet fusée courant dans un nouveau fichier\r
+!BasicFrame.item.Printpart = Imprimer la liste des pièces et les modèles d'ailerons\r
+!BasicFrame.item.Closedesign = Fermer le projet fusée courant\r
+!BasicFrame.item.Quitprogram = Quitter le programme\r
+!BasicFrame.menu.Rocketedt = Modification de la fusée\r
BasicFrame.dlg.lbl1 = Le projet '\r
BasicFrame.dlg.lbl2 = ' N'a pas été sauvegardé.\r
BasicFrame.dlg.lbl3 = Voulez vous le sauvegarder?\r
BasicFrame.WarningDialog.txt2 = Certains elements du projet n'ont peut etre pas été chargé correctement.\r
BasicFrame.WarningDialog.title = Avertissement lors de l'ouverture du fichier\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
! Labels used in buttons of dialog windows\r
button.ok = OK\r
button.cancel = Annuler\r
dlg.but.cancel = Annuler\r
dlg.but.close = Fermer\r
\r
+\r
! General file type names\r
filetypes.pdf = PDF files\r
\r
+\r
! About Dialog\r
AboutDialog.lbl.version = Version\r
! The texts below provide additional credits for the translation maintainer\r
PrintDialog.error.preview.desc1 = Impossible d'ouvrir la prévisualisation PDF.\r
PrintDialog.error.preview.desc2 = S'il vous plait utilisez l'option "Sauvegarder en PDF" à la place.\r
\r
+\r
!PrintSettingsDialog\r
PrintSettingsDialog.title = Configuration impression\r
PrintSettingsDialog.lbl.Templatefillcolor = Couleur de remplissage du modele:\r
PrintSettingsDialog.but.Reset = Réinitialiser\r
PrintSettingsDialog.but.Close = Fermer\r
\r
+\r
! Bug Report dialog\r
bugreport.dlg.title = Rapport d'erreurs\r
bugreport.dlg.but.Sendbugreport = Envoyer un rapport d'erreurs\r
bugreport.dlg.failedmsg3 = Erreur d'envoi du rapport\r
bugreport.reportDialog.txt = <html><b>Vous pouvez signaler une erreur avec OpenRocket en remplissant et en envoyant le message ci-dessous.</b><br>Vous pouvez egalement signaler des erreurs et inclure des pieces jointes sur le site web du projet.\r
bugreport.reportDialog.txt2 = <html><b>S'il vous plait ajoutez une courte description de ce que vous faisiez lorsque l'erreur s'est produite.</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
\r
! Example design dialog\r
exdesigndlg.but.open = Ouvrir\r
-exdesigndlg.lbl.Selectexample = Chosir l'exemple de projet à ouvrir:\r
+exdesigndlg.lbl.Selectexample = Choisir l'exemple de projet à ouvrir:\r
exdesigndlg.lbl.Openexampledesign = Ouvrir un exemple de projet\r
exdesigndlg.lbl.Exampledesignsnotfound = Impossible de trouver les exemples de projets.\r
exdesigndlg.lbl.Examplesnotfound = Exemples non trouvés\r
\r
\r
-\r
! Material edit panel\r
matedtpan.but.new = Nouveau\r
matedtpan.but.edit = Editer\r
pref.dlg.lbl.Momentofinertia = Moment d'inertie:\r
pref.dlg.lbl.Pressure = Pression:\r
pref.dlg.lbl.Stability = Stabilité:\r
+pref.dlg.lbl.FlightTime = Durée du vol:\r
pref.dlg.lbl.effect1 = Les changements prendront effet la prochaine fois que vous ouvrirez une fenêtre.\r
pref.dlg.lbl.Checkingupdates = Recherche des mises à jour...\r
pref.dlg.lbl.msg1 = Une erreur est survenue durant la communication avec le serveur.\r
simedtdlg.lbl.Launchsite = Site de lancement\r
simedtdlg.lbl.Latitude = Latitude:\r
simedtdlg.lbl.ttip.Latitude = <html>La latitude du site de lancement affecte l'attraction gravitationnelle de la Terre.<br>> Les valeurs positives sont dans l'hémisphère Nord, les valeurs négatives sur l'hémisphère Sud.\r
+\r
+simedtdlg.lbl.Longitude = Longitude:\r
+simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.\r
+\r
simedtdlg.lbl.Altitude = Altitude:\r
simedtdlg.lbl.ttip.Altitude = <html>Altitude du site de lancement par rapport au niveau de la mer.<br>Cela affecte la position de la fusée dans le modèle atmosphérique.\r
simedtdlg.border.Launchrod = Rampe de lancement\r
simedtdlg.lbl.Simmethod = Méthode de Simulation:\r
simedtdlg.lbl.ttip.Simmethod1 = <html>Le simulateur de six degrés de liberté permet la liberté totale de fusée en vol.<br>\r
simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.\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 = Règlage du pas de temps:\r
simedtdlg.lbl.ttip.Timestep1 = <html>Le temps entre les étapes de la simulation.<br>Avec un pas de temps plus petit la simulation est plus lente mais également plus précise.<br>\r
simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of\r
simedtdlg.IntensityDesc.Veryhigh = Très haute\r
simedtdlg.IntensityDesc.Extreme = Extreme\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
SimuRunDlg.msg.unknownerror2 = Le programme peut être instable, vous devez enregistrer toutes vos créations et redémarrez OpenRocket maintenant!\r
\r
\r
+\r
! SimulationExportPanel\r
SimExpPan.desc = Fichiers dont les données sont séparées par une virgule (*.csv)\r
SimExpPan.border.Vartoexport = Variables à exporter\r
SimExpPan.Col.Variable = Variable\r
SimExpPan.Col.Unit = Unité\r
\r
+\r
+CsvOptionPanel.separator.space = SPACE\r
+CsvOptionPanel.separator.tab = TAB\r
+\r
+\r
+\r
! MotorPlot\r
MotorPlot.title.Motorplot = Courbe du moteur\r
MotorPlot.but.Select = Selection\r
simplotpanel.RIGHT_NAME = Droite\r
simplotpanel.CUSTOM = Personnalisé\r
\r
-\r
-\r
! Component add buttons\r
compaddbuttons.Bodycompandfinsets = Pièces du corps et ailerons\r
compaddbuttons.Nosecone = Cône\r
componentanalysisdlg.lbl.reflenght = Longueur de référence: \r
componentanalysisdlg.lbl.refarea = Aire de référence: \r
!componentanalysisdlg.but.close =Fermer\r
+componentanalysisdlg.TabStability.Col.Component = Pièce\r
\r
! Custom Material dialog\r
custmatdlg.title.Custommaterial = Matériau personnalisé\r
ringcompcfg.note.desc = A noter: Un tube interne n'affectera pas l'aerodynamisme de la fusée meme si il est situé en dehors du tube.\r
\r
\r
-\r
! Body Tube Config\r
BodyTubecfg.lbl.Bodytubelength = Longueur du tube:\r
BodyTubecfg.lbl.Outerdiameter = Diamètre externe:\r
RocketCompCfg.lbl.Thickness = Epaisseur:\r
RocketCompCfg.checkbox.Endcapped = Arrière clos \r
RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped.\r
-RocketCompCfg.title.Noseconeshoulder = accotement du cône\r
-RocketCompCfg.title.Aftshoulder = accotement arrière\r
-RocketCompCfg.border.Foreshoulder = Fore shoulder \r
+RocketCompCfg.title.Noseconeshoulder = Accotement du cône\r
+RocketCompCfg.title.Aftshoulder = Accotement arrière\r
+RocketCompCfg.border.Foreshoulder = Accotement avant \r
!RocketCompCfg.lbl.Length = Length:\r
\r
! BulkheadConfig\r
FreeformFinSetCfg.lbl.plus = plus\r
FreeformFinSetCfg.lbl.FincrossSection = Coupe de l'aileron:\r
FreeformFinSetCfg.lbl.Thickness = Epaisseur:\r
-FreeformFinSetCfg.lbl.Double-click = Double-click\r
-FreeformFinSetCfg.lbl.toedit = pour editer\r
-FreeformFinSetCfg.lbl.Clickdrag = Cliquer+déplacer: Ajouter et déplacer des points\r
-FreeformFinSetCfg.lbl.Ctrlclick = Ctrl+cliquer: Enlever un point\r
+! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle\r
+FreeformFinSetCfg.lbl.doubleClick1 = Double-click\r
+FreeformFinSetCfg.lbl.doubleClick2 = pour editer\r
+FreeformFinSetCfg.lbl.clickDrag = Cliquer+déplacer: Ajouter et déplacer des points\r
+FreeformFinSetCfg.lbl.ctrlClick = Ctrl+cliquer: Enlever un point\r
+\r
\r
!InnerTubeConfig\r
InnerTubeCfg.tab.Motor = Moteur\r
TCMotorSelPan.title.Thrust = Poussée\r
TCMotorSelPan.delayBox.None = Aucun\r
\r
+\r
! PlotDialog\r
PlotDialog.title.Flightdataplot = Tracé du vol\r
PlotDialog.Chart.Simulatedflight = Simulation du vol\r
PlotDialog.CheckBox.Showdatapoints = Afficher un point pour chaque valeur\r
PlotDialog.lbl.Chart = Cliquer+déplacer en bas +droite pour agrandir, haut+gauche pour rétrécir\r
\r
+\r
! "main" prefix is used for the main application dialog\r
\r
+# FIXME: Rename the description keys \r
+\r
main.menu.file = Fichier\r
+main.menu.file.desc = File-handling related tasks\r
main.menu.file.new = Nouveau\r
+main.menu.file.new.desc = Create a new rocket design\r
main.menu.file.open = Ouvrir...\r
+BasicFrame.item.Openrocketdesign = Open a rocket design\r
main.menu.file.openExample = Ouvrir exemple...\r
+BasicFrame.item.Openexamplerocketdesign = Open an example rocket design\r
main.menu.file.save = Sauvegarder\r
+BasicFrame.item.SavecurRocketdesign = Save the current rocket design\r
main.menu.file.saveAs = Sauvegarder sous...\r
-main.menu.file.print = Imprimer...\r
+BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file\r
+main.menu.file.print = Imprimer/Exporter en PDF...\r
+main.menu.file.print.desc = Print or save as PDF the parts list and fin templates\r
main.menu.file.close = Fermer\r
+BasicFrame.item.Closedesign = Ferme le projet fusée en cour\r
main.menu.file.quit = Quitter\r
+BasicFrame.item.Quitprogram = Quitte le programme\r
\r
main.menu.edit = Editer\r
+BasicFrame.menu.Rocketedt = Rocket editing\r
main.menu.edit.undo = Annuler modification\r
main.menu.edit.undo.desc = Annuler l'opération précédente\r
main.menu.edit.redo = Refaire modification\r
main.menu.edit.paste = Coller\r
main.menu.edit.delete = Effacer\r
main.menu.edit.resize = Redimensionner...\r
+main.menu.edit.resize.desc = Scale parts of the rocket design\r
main.menu.edit.preferences = Préférences\r
+main.menu.edit.preferences.desc = Setup the application preferences\r
\r
main.menu.analyze = Analyse\r
+main.menu.analyze.desc = Rocket analysis\r
main.menu.analyze.componentAnalysis = Analyse des Pièces\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 = Aide\r
+main.menu.help.desc = Information à propos d'OpenRocket\r
main.menu.help.license = Licence\r
+main.menu.help.license.desc = OpenRocket license information\r
main.menu.help.bugReport = Rapport d'erreurs\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 = A propos\r
+main.menu.help.about.desc = Copyright details about OpenRocket\r
\r
main.menu.debug = Debug\r
main.menu.debug.whatisthismenu = Quel est ce menu?\r
Databases.materials.StyrofoamgenericEPS = Polystyrène (générique EPS)\r
Databases.materials.StyrofoamBluefoamXPS = \"Mousse Bleue\" de polystyrène (XPS)\r
Databases.materials.Quantumtubing = Tube Quantum\r
+Databases.materials.BlueTube = Blue tube\r
!SURFACE_MATERIAL\r
Databases.materials.Ripstopnylon = Ripstop nylon\r
Databases.materials.Mylar = Mylar\r
Databases.materials.Polyethylenethin = Polyéthylène (fin)\r
Databases.materials.Polyethyleneheavy = Polyéthylène (lourd)\r
Databases.materials.Silk = Soie\r
-Databases.materials.Paperoffice1 = Papier (bureau)\r
+Databases.materials.Paperoffice = Papier (bureau)\r
Databases.materials.Cellophane = Cellophane\r
Databases.materials.Crepepaper = Cr\u00eape paper\r
! LINE_MATERIAL\r
ExternalComponent.Smoothpaint = Fine couche\r
ExternalComponent.Polished = Polie\r
\r
-\r
! LineStyle\r
LineStyle.Solid = Ligne pleine\r
LineStyle.Dashed = Tiret\r
RocketComponent.Position.AFTER = Après la pièce parent\r
RocketComponent.Position.ABSOLUTE = Pointe de l'ogive\r
\r
-\r
! LaunchLug\r
LaunchLug.Launchlug = Tube de guidage\r
! NoseCone\r
FlightDataType.TYPE_SPEED_OF_SOUND = Vitesse du son\r
FlightDataType.TYPE_TIME_STEP = Pas de simulation du temps\r
FlightDataType.TYPE_COMPUTATION_TIME = Temps de calcul\r
+FlightDataType.TYPE_LATITUDE = Latitude\r
+FlightDataType.TYPE_LONGITUDE = Longitude\r
+FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration\r
\r
! PlotConfiguration\r
PlotConfiguration.Verticalmotion = Mouvement vertical par rapport au temps\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 = Redimensionner\r
-\r
+ScaleDialog.undo.scaleRocket = Redimensionner la fusée\r
+ScaleDialog.undo.scaleComponent = Redimensionner une pièce\r
+ScaleDialog.undo.scaleComponents = Redimensionner les pièces\r
\r
!icons\r
Icons.Undo = Undo\r
\r
! Modifiers\r
\r
-optimization.modifier.nosecone.length = Longuer du cone\r
+optimization.modifier.nosecone.length = Longueur du cone\r
+optimization.modifier.nosecone.length.desc = Optimise la longueur du cone.\r
optimization.modifier.nosecone.diameter = Diamètre du Cone\r
+optimization.modifier.nosecone.diameter.desc = Optimise le diamètre du cone.\r
optimization.modifier.nosecone.thickness = Epaisseur du Cone\r
+optimization.modifier.nosecone.thickness.desc = Optimize l'epasseur des paroies du cone.\r
+optimization.modifier.nosecone.shapeparameter = Parametre de la forme\r
+optimization.modifier.nosecone.shapeparameter.desc = Optimise les parametres de forme du cone.\r
\r
optimization.modifier.transition.length = Longueur de la Transition\r
+optimization.modifier.transition.length.desc = Optimise la longueur de la transition.\r
optimization.modifier.transition.forediameter = Transition fore diameter\r
+optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.\r
optimization.modifier.transition.aftdiameter = Transition aft diameter\r
+optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.\r
optimization.modifier.transition.thickness = Epaisseur de la transition\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 = Longueur du tube du corps\r
+optimization.modifier.bodytube.length.desc = Optimise la longueur du tube.\r
optimization.modifier.bodytube.outerDiameter = Diamètre externe du tube du corps\r
+optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.\r
optimization.modifier.bodytube.innerDiameter = Body tube inner diameter\r
optimization.modifier.bodytube.thickness = Epaisseur du tube du corps\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 = Longueur\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 = Longueur\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 = Démarrer l'optimization\r
+GeneralOptimizationDialog.btn.stop = Terminer l'optimization\r
+GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:\r
+GeneralOptimizationDialog.btn.add = Ajouter\r
+GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization\r
+GeneralOptimizationDialog.btn.remove = Enlever\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 = Parametres disponible:\r
+GeneralOptimizationDialog.lbl.optimizationOpts = Options pour l'optimization\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 = Fermer\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 = Simulation simple\r
+GeneralOptimizationDialog.noSimulationName = Pas de 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 = Stabilité\r
+\r
+\r
+! Dialog for plotting optimization results\r
+OptimizationPlotDialog.title = Résultats de l'optimisation\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 = Stabilité:\r
+OptimizationPlotDialog.plot.label.optimum = Optimum\r
+\r
+! Optimization parameters\r
+MaximumAltitudeParameter.name = Altitude de l'apogée\r
+MaximumVelocityParameter.name = Maximum velocity\r
+MaximumAccelerationParameter.name = Accelération maximum\r
+StabilityParameter.name = Stabilité\r
+GroundHitVelocityParameter.name = Vitesse à l'atterrissage\r
+LandingDistanceParameter.name = Distance à l'attérrissage\r
+TotalFlightTimeParameter.name = Durée totale du vol\r
+DeploymentVelocityParameter.name = Velocity at parachute deployment\r
projects / debian / openrocket / commitdiff