diff --git a/l10n/messages_fr.properties b/l10n/messages_fr.properties index 07fd91665..bb6254906 100644 --- a/l10n/messages_fr.properties +++ b/l10n/messages_fr.properties @@ -2,7 +2,15 @@ # # French base translation file # Translated by Tripoli France - +# Should you need to add new logical keys here is the proposed method +# +# className.ComponentType.componentName +# +# +# Text tokens within braces should not be translated, e.g. +# "The file '{filename}' exists." +# They are pieces that are inserted dynamically. +# ! Set to the name of the current translation file (used for debugging purposes) debug.currentFile = messages_fr.properties @@ -51,14 +59,14 @@ BasicFrame.SimpleFileFilter3 = Fichiers RockSim (*.rkt) BasicFrame.tab.Rocketdesign = Projet fusée BasicFrame.tab.Flightsim = Simulations de vol BasicFrame.title.Addnewcomp = Ajouter une nouvelle pièce -BasicFrame.item.Openrocketdesign = Ouvrir un projet fusée -BasicFrame.item.Openexamplerocketdesign = Ouvrir un exemple de projet fusée -BasicFrame.item.SavecurRocketdesign = Sauvegarder le projet fusée courant -BasicFrame.item.SavecurRocketdesnewfile = Sauvegarder le projet fusée courant dans un nouveau fichier -BasicFrame.item.Printpart = Imprimer la liste des pièces et les modèles d'ailerons -BasicFrame.item.Closedesign = Fermer le projet fusée courant -BasicFrame.item.Quitprogram = Quitter le programme -BasicFrame.menu.Rocketedt = Modification de la fusée +!BasicFrame.item.Openrocketdesign = Ouvrir un projet fusée +!BasicFrame.item.Openexamplerocketdesign = Ouvrir un exemple de projet fusée +!BasicFrame.item.SavecurRocketdesign = Sauvegarder le projet fusée courant +!BasicFrame.item.SavecurRocketdesnewfile = Sauvegarder le projet fusée courant dans un nouveau fichier +!BasicFrame.item.Printpart = Imprimer la liste des pièces et les modèles d'ailerons +!BasicFrame.item.Closedesign = Fermer le projet fusée courant +!BasicFrame.item.Quitprogram = Quitter le programme +!BasicFrame.menu.Rocketedt = Modification de la fusée BasicFrame.dlg.lbl1 = Le projet ' BasicFrame.dlg.lbl2 = ' N'a pas été sauvegardé. BasicFrame.dlg.lbl3 = Voulez vous le sauvegarder? @@ -68,6 +76,13 @@ BasicFrame.WarningDialog.txt1 = Les problemes suivant sont survenus lors de l'ou BasicFrame.WarningDialog.txt2 = Certains elements du projet n'ont peut etre pas été chargé correctement. BasicFrame.WarningDialog.title = Avertissement lors de l'ouverture du fichier +! General error messages used in multiple contexts +error.fileExists.title = File exists +error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it? + +error.writing.title = Error writing file +error.writing.desc = An error occurred while writing to the file: + ! Labels used in buttons of dialog windows button.ok = OK button.cancel = Annuler @@ -78,9 +93,11 @@ dlg.but.ok = Accepter dlg.but.cancel = Annuler dlg.but.close = Fermer + ! General file type names filetypes.pdf = PDF files + ! About Dialog AboutDialog.lbl.version = Version ! The texts below provide additional credits for the translation maintainer @@ -105,6 +122,7 @@ PrintDialog.error.preview.title = Impossible d'ouvrir la pr PrintDialog.error.preview.desc1 = Impossible d'ouvrir la prévisualisation PDF. PrintDialog.error.preview.desc2 = S'il vous plait utilisez l'option "Sauvegarder en PDF" à la place. + !PrintSettingsDialog PrintSettingsDialog.title = Configuration impression PrintSettingsDialog.lbl.Templatefillcolor = Couleur de remplissage du modele: @@ -114,6 +132,7 @@ PrintSettingsDialog.lbl.Paperorientation = Orientation du papier: PrintSettingsDialog.but.Reset = Réinitialiser PrintSettingsDialog.but.Close = Fermer + ! Bug Report dialog bugreport.dlg.title = Rapport d'erreurs bugreport.dlg.but.Sendbugreport = Envoyer un rapport d'erreurs @@ -129,6 +148,8 @@ bugreport.dlg.failedmsg2 = S'il vous plait envoyez le rapport manuellement bugreport.dlg.failedmsg3 = Erreur d'envoi du rapport bugreport.reportDialog.txt = Vous pouvez signaler une erreur avec OpenRocket en remplissant et en envoyant le message ci-dessous.
Vous pouvez egalement signaler des erreurs et inclure des pieces jointes sur le site web du projet. bugreport.reportDialog.txt2 = S'il vous plait ajoutez une courte description de ce que vous faisiez lorsque l'erreur s'est produite. +bugreport.dlg.provideDescription = Please provide a description of the bug first. +bugreport.dlg.provideDescription.title = Bug description missing ! Debug log dialog @@ -162,13 +183,12 @@ edtmotorconfdlg.lbl.Leavenamedefault = Laisser le champ vide par d ! Example design dialog exdesigndlg.but.open = Ouvrir -exdesigndlg.lbl.Selectexample = Chosir l'exemple de projet à ouvrir: +exdesigndlg.lbl.Selectexample = Choisir l'exemple de projet à ouvrir: exdesigndlg.lbl.Openexampledesign = Ouvrir un exemple de projet exdesigndlg.lbl.Exampledesignsnotfound = Impossible de trouver les exemples de projets. exdesigndlg.lbl.Examplesnotfound = Exemples non trouvés - ! Material edit panel matedtpan.but.new = Nouveau matedtpan.but.edit = Editer @@ -235,6 +255,7 @@ pref.dlg.lbl.Temperature = Temp pref.dlg.lbl.Momentofinertia = Moment d'inertie: pref.dlg.lbl.Pressure = Pression: pref.dlg.lbl.Stability = Stabilité: +pref.dlg.lbl.FlightTime = Durée du vol: pref.dlg.lbl.effect1 = Les changements prendront effet la prochaine fois que vous ouvrirez une fenêtre. pref.dlg.lbl.Checkingupdates = Recherche des mises à jour... pref.dlg.lbl.msg1 = Une erreur est survenue durant la communication avec le serveur. @@ -288,6 +309,10 @@ simedtdlg.lbl.ttip.Pressure = Pression atmosph simedtdlg.lbl.Launchsite = Site de lancement simedtdlg.lbl.Latitude = Latitude: simedtdlg.lbl.ttip.Latitude = La latitude du site de lancement affecte l'attraction gravitationnelle de la Terre.
> Les valeurs positives sont dans l'hémisphère Nord, les valeurs négatives sur l'hémisphère Sud. + +simedtdlg.lbl.Longitude = Longitude: +simedtdlg.lbl.ttip.Longitude = Required for weather prediction and elevation models. + simedtdlg.lbl.Altitude = Altitude: simedtdlg.lbl.ttip.Altitude = Altitude du site de lancement par rapport au niveau de la mer.
Cela affecte la position de la fusée dans le modèle atmosphérique. simedtdlg.border.Launchrod = Rampe de lancement @@ -306,6 +331,8 @@ simedtdlg.lbl.ExtBarrowman = Barrowman simedtdlg.lbl.Simmethod = Méthode de Simulation: simedtdlg.lbl.ttip.Simmethod1 = Le simulateur de six degrés de liberté permet la liberté totale de fusée en vol.
simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4th order Runge-Kutta 4 numerical integration. +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 = Règlage du pas de temps: simedtdlg.lbl.ttip.Timestep1 = Le temps entre les étapes de la simulation.
Avec un pas de temps plus petit la simulation est plus lente mais également plus précise.
simedtdlg.lbl.ttip.Timestep2 = The 4th order simulation method is quite accurate with a time step of @@ -327,6 +354,12 @@ simedtdlg.IntensityDesc.High = Haute simedtdlg.IntensityDesc.Veryhigh = Très haute simedtdlg.IntensityDesc.Extreme = Extreme +GeodeticComputationStrategy.none.name = None +GeodeticComputationStrategy.none.desc = Perform no geodetic computations. +GeodeticComputationStrategy.spherical.name = Spherical approximation +GeodeticComputationStrategy.spherical.desc = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. +GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid +GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
Slower and unnecessary in most cases. @@ -370,6 +403,7 @@ SimuRunDlg.msg.unknownerror1 = Une erreur inconnue s'est produite lors de la sim SimuRunDlg.msg.unknownerror2 = Le programme peut être instable, vous devez enregistrer toutes vos créations et redémarrez OpenRocket maintenant! + ! SimulationExportPanel SimExpPan.desc = Fichiers dont les données sont séparées par une virgule (*.csv) SimExpPan.border.Vartoexport = Variables à exporter @@ -398,6 +432,12 @@ SimExpPan.ExportingVar.desc3 = variable sur un total de SimExpPan.Col.Variable = Variable SimExpPan.Col.Unit = Unité + +CsvOptionPanel.separator.space = SPACE +CsvOptionPanel.separator.tab = TAB + + + ! MotorPlot MotorPlot.title.Motorplot = Courbe du moteur MotorPlot.but.Select = Selection @@ -432,8 +472,6 @@ simplotpanel.LEFT_NAME = Gauche simplotpanel.RIGHT_NAME = Droite simplotpanel.CUSTOM = Personnalisé - - ! Component add buttons compaddbuttons.Bodycompandfinsets = Pièces du corps et ailerons compaddbuttons.Nosecone = Cône @@ -493,6 +531,7 @@ componentanalysisdlg.println.settingnam = SETTING NAN VALUES componentanalysisdlg.lbl.reflenght = Longueur de référence: componentanalysisdlg.lbl.refarea = Aire de référence: !componentanalysisdlg.but.close =Fermer +componentanalysisdlg.TabStability.Col.Component = Pièce ! Custom Material dialog custmatdlg.title.Custommaterial = Matériau personnalisé @@ -521,7 +560,6 @@ ringcompcfg.EngineBlock.desc = Un bloc moteur emp 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. - ! Body Tube Config BodyTubecfg.lbl.Bodytubelength = Longueur du tube: BodyTubecfg.lbl.Outerdiameter = Diamètre externe: @@ -604,9 +642,9 @@ RocketCompCfg.lbl.Length = Longueur: RocketCompCfg.lbl.Thickness = Epaisseur: RocketCompCfg.checkbox.Endcapped = Arrière clos RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped. -RocketCompCfg.title.Noseconeshoulder = accotement du cône -RocketCompCfg.title.Aftshoulder = accotement arrière -RocketCompCfg.border.Foreshoulder = Fore shoulder +RocketCompCfg.title.Noseconeshoulder = Accotement du cône +RocketCompCfg.title.Aftshoulder = Accotement arrière +RocketCompCfg.border.Foreshoulder = Accotement avant !RocketCompCfg.lbl.Length = Length: ! BulkheadConfig @@ -654,10 +692,12 @@ FreeformFinSetCfg.lbl.Posrelativeto = Position par rapport FreeformFinSetCfg.lbl.plus = plus FreeformFinSetCfg.lbl.FincrossSection = Coupe de l'aileron: FreeformFinSetCfg.lbl.Thickness = Epaisseur: -FreeformFinSetCfg.lbl.Double-click = Double-click -FreeformFinSetCfg.lbl.toedit = pour editer -FreeformFinSetCfg.lbl.Clickdrag = Cliquer+déplacer: Ajouter et déplacer des points -FreeformFinSetCfg.lbl.Ctrlclick = Ctrl+cliquer: Enlever un point +! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle +FreeformFinSetCfg.lbl.doubleClick1 = Double-click +FreeformFinSetCfg.lbl.doubleClick2 = pour editer +FreeformFinSetCfg.lbl.clickDrag = Cliquer+déplacer: Ajouter et déplacer des points +FreeformFinSetCfg.lbl.ctrlClick = Ctrl+cliquer: Enlever un point + !InnerTubeConfig InnerTubeCfg.tab.Motor = Moteur @@ -897,25 +937,39 @@ TCMotorSelPan.title.Thrustcurve = Courbe de pouss TCMotorSelPan.title.Thrust = Poussée TCMotorSelPan.delayBox.None = Aucun + ! PlotDialog PlotDialog.title.Flightdataplot = Tracé du vol PlotDialog.Chart.Simulatedflight = Simulation du vol PlotDialog.CheckBox.Showdatapoints = Afficher un point pour chaque valeur PlotDialog.lbl.Chart = Cliquer+déplacer en bas +droite pour agrandir, haut+gauche pour rétrécir + ! "main" prefix is used for the main application dialog +# FIXME: Rename the description keys + main.menu.file = Fichier +main.menu.file.desc = File-handling related tasks main.menu.file.new = Nouveau +main.menu.file.new.desc = Create a new rocket design main.menu.file.open = Ouvrir... +BasicFrame.item.Openrocketdesign = Open a rocket design main.menu.file.openExample = Ouvrir exemple... +BasicFrame.item.Openexamplerocketdesign = Open an example rocket design main.menu.file.save = Sauvegarder +BasicFrame.item.SavecurRocketdesign = Save the current rocket design main.menu.file.saveAs = Sauvegarder sous... -main.menu.file.print = Imprimer... +BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file +main.menu.file.print = Imprimer/Exporter en PDF... +main.menu.file.print.desc = Print or save as PDF the parts list and fin templates main.menu.file.close = Fermer +BasicFrame.item.Closedesign = Ferme le projet fusée en cour main.menu.file.quit = Quitter +BasicFrame.item.Quitprogram = Quitte le programme main.menu.edit = Editer +BasicFrame.menu.Rocketedt = Rocket editing main.menu.edit.undo = Annuler modification main.menu.edit.undo.desc = Annuler l'opération précédente main.menu.edit.redo = Refaire modification @@ -925,16 +979,27 @@ main.menu.edit.copy = Copier main.menu.edit.paste = Coller main.menu.edit.delete = Effacer main.menu.edit.resize = Redimensionner... +main.menu.edit.resize.desc = Scale parts of the rocket design main.menu.edit.preferences = Préférences +main.menu.edit.preferences.desc = Setup the application preferences main.menu.analyze = Analyse +main.menu.analyze.desc = Rocket analysis main.menu.analyze.componentAnalysis = Analyse des Pièces +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 = Aide +main.menu.help.desc = Information à propos d'OpenRocket main.menu.help.license = Licence +main.menu.help.license.desc = OpenRocket license information main.menu.help.bugReport = Rapport d'erreurs +main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket main.menu.help.debugLog = Debug log +main.menu.help.debugLog.desc = View the OpenRocket debug log main.menu.help.about = A propos +main.menu.help.about.desc = Copyright details about OpenRocket main.menu.debug = Debug main.menu.debug.whatisthismenu = Quel est ce menu? @@ -966,13 +1031,14 @@ Databases.materials.Spruce = Sapin Databases.materials.StyrofoamgenericEPS = Polystyrène (générique EPS) Databases.materials.StyrofoamBluefoamXPS = \"Mousse Bleue\" de polystyrène (XPS) Databases.materials.Quantumtubing = Tube Quantum +Databases.materials.BlueTube = Blue tube !SURFACE_MATERIAL Databases.materials.Ripstopnylon = Ripstop nylon Databases.materials.Mylar = Mylar Databases.materials.Polyethylenethin = Polyéthylène (fin) Databases.materials.Polyethyleneheavy = Polyéthylène (lourd) Databases.materials.Silk = Soie -Databases.materials.Paperoffice1 = Papier (bureau) +Databases.materials.Paperoffice = Papier (bureau) Databases.materials.Cellophane = Cellophane Databases.materials.Crepepaper = Cr\u00eape paper ! LINE_MATERIAL @@ -995,7 +1061,6 @@ ExternalComponent.Regularpaint = Peinture classique ExternalComponent.Smoothpaint = Fine couche ExternalComponent.Polished = Polie - ! LineStyle LineStyle.Solid = Ligne pleine LineStyle.Dashed = Tiret @@ -1031,7 +1096,6 @@ RocketComponent.Position.BOTTOM = Bas de la pi RocketComponent.Position.AFTER = Après la pièce parent RocketComponent.Position.ABSOLUTE = Pointe de l'ogive - ! LaunchLug LaunchLug.Launchlug = Tube de guidage ! NoseCone @@ -1198,6 +1262,9 @@ FlightDataType.TYPE_AIR_PRESSURE = Pression atmosph FlightDataType.TYPE_SPEED_OF_SOUND = Vitesse du son FlightDataType.TYPE_TIME_STEP = Pas de simulation du temps FlightDataType.TYPE_COMPUTATION_TIME = Temps de calcul +FlightDataType.TYPE_LATITUDE = Latitude +FlightDataType.TYPE_LONGITUDE = Longitude +FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration ! PlotConfiguration PlotConfiguration.Verticalmotion = Mouvement vertical par rapport au temps @@ -1236,7 +1303,9 @@ ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and r 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 = Redimensionner - +ScaleDialog.undo.scaleRocket = Redimensionner la fusée +ScaleDialog.undo.scaleComponent = Redimensionner une pièce +ScaleDialog.undo.scaleComponents = Redimensionner les pièces !icons Icons.Undo = Undo @@ -1256,16 +1325,181 @@ EllipticalFinSet.Ellipticalfinset = Ailerons elyptique ! Modifiers -optimization.modifier.nosecone.length = Longuer du cone +optimization.modifier.nosecone.length = Longueur du cone +optimization.modifier.nosecone.length.desc = Optimise la longueur du cone. optimization.modifier.nosecone.diameter = Diamètre du Cone +optimization.modifier.nosecone.diameter.desc = Optimise le diamètre du cone. optimization.modifier.nosecone.thickness = Epaisseur du Cone +optimization.modifier.nosecone.thickness.desc = Optimize l'epasseur des paroies du cone. +optimization.modifier.nosecone.shapeparameter = Parametre de la forme +optimization.modifier.nosecone.shapeparameter.desc = Optimise les parametres de forme du cone. optimization.modifier.transition.length = Longueur de la Transition +optimization.modifier.transition.length.desc = Optimise la longueur de la transition. optimization.modifier.transition.forediameter = Transition fore diameter +optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter. optimization.modifier.transition.aftdiameter = Transition aft diameter +optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter. optimization.modifier.transition.thickness = Epaisseur de la transition +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 = Longueur du tube du corps +optimization.modifier.bodytube.length.desc = Optimise la longueur du tube. optimization.modifier.bodytube.outerDiameter = Diamètre externe du tube du corps +optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness. optimization.modifier.bodytube.innerDiameter = Body tube inner diameter optimization.modifier.bodytube.thickness = Epaisseur du tube du corps +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 = Longueur +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 = Longueur +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 = Démarrer l'optimization +GeneralOptimizationDialog.btn.stop = Terminer l'optimization +GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize: +GeneralOptimizationDialog.btn.add = Ajouter +GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization +GeneralOptimizationDialog.btn.remove = Enlever +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 = Parametres disponible: +GeneralOptimizationDialog.lbl.optimizationOpts = Options pour l'optimization +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 = Fermer +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 = Simulation simple +GeneralOptimizationDialog.noSimulationName = Pas de 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 = Stabilité + + +! Dialog for plotting optimization results +OptimizationPlotDialog.title = Résultats de l'optimisation +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 = Stabilité: +OptimizationPlotDialog.plot.label.optimum = Optimum + +! Optimization parameters +MaximumAltitudeParameter.name = Altitude de l'apogée +MaximumVelocityParameter.name = Maximum velocity +MaximumAccelerationParameter.name = Accelération maximum +StabilityParameter.name = Stabilité +GroundHitVelocityParameter.name = Vitesse à l'atterrissage +LandingDistanceParameter.name = Distance à l'attérrissage +TotalFlightTimeParameter.name = Durée totale du vol +DeploymentVelocityParameter.name = Velocity at parachute deployment