Added new sting to be translated
This commit is contained in:
Boris du Reau
parent
9e6e7418c2
commit
97d1f19cd6
@ -2,7 +2,15 @@
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#
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# French base translation file
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# Translated by Tripoli France
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# Should you need to add new logical keys here is the proposed method
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#
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# className.ComponentType.componentName
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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_fr.properties
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@ -51,14 +59,14 @@ BasicFrame.SimpleFileFilter3 = Fichiers RockSim (*.rkt)
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BasicFrame.tab.Rocketdesign = Projet fusée
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BasicFrame.tab.Flightsim = Simulations de vol
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BasicFrame.title.Addnewcomp = Ajouter une nouvelle pièce
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BasicFrame.item.Openrocketdesign = Ouvrir un projet fusée
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BasicFrame.item.Openexamplerocketdesign = Ouvrir un exemple de projet fusée
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BasicFrame.item.SavecurRocketdesign = Sauvegarder le projet fusée courant
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BasicFrame.item.SavecurRocketdesnewfile = Sauvegarder le projet fusée courant dans un nouveau fichier
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BasicFrame.item.Printpart = Imprimer la liste des pièces et les modèles d'ailerons
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BasicFrame.item.Closedesign = Fermer le projet fusée courant
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BasicFrame.item.Quitprogram = Quitter le programme
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BasicFrame.menu.Rocketedt = Modification de la fusée
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!BasicFrame.item.Openrocketdesign = Ouvrir un projet fusée
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!BasicFrame.item.Openexamplerocketdesign = Ouvrir un exemple de projet fusée
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!BasicFrame.item.SavecurRocketdesign = Sauvegarder le projet fusée courant
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!BasicFrame.item.SavecurRocketdesnewfile = Sauvegarder le projet fusée courant dans un nouveau fichier
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!BasicFrame.item.Printpart = Imprimer la liste des pièces et les modèles d'ailerons
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!BasicFrame.item.Closedesign = Fermer le projet fusée courant
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!BasicFrame.item.Quitprogram = Quitter le programme
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!BasicFrame.menu.Rocketedt = Modification de la fusée
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BasicFrame.dlg.lbl1 = Le projet '
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BasicFrame.dlg.lbl2 = ' N'a pas été sauvegardé.
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BasicFrame.dlg.lbl3 = Voulez vous le sauvegarder?
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@ -68,6 +76,13 @@ BasicFrame.WarningDialog.txt1 = Les problemes suivant sont survenus lors de l'ou
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BasicFrame.WarningDialog.txt2 = Certains elements du projet n'ont peut etre pas été chargé correctement.
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BasicFrame.WarningDialog.title = Avertissement lors de l'ouverture du fichier
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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 = Annuler
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@ -78,9 +93,11 @@ dlg.but.ok = Accepter
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dlg.but.cancel = Annuler
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dlg.but.close = Fermer
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! General file type names
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filetypes.pdf = PDF files
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! About Dialog
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AboutDialog.lbl.version = Version
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! The texts below provide additional credits for the translation maintainer
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@ -105,6 +122,7 @@ PrintDialog.error.preview.title = Impossible d'ouvrir la pr
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PrintDialog.error.preview.desc1 = Impossible d'ouvrir la prévisualisation PDF.
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PrintDialog.error.preview.desc2 = S'il vous plait utilisez l'option "Sauvegarder en PDF" à la place.
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!PrintSettingsDialog
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PrintSettingsDialog.title = Configuration impression
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PrintSettingsDialog.lbl.Templatefillcolor = Couleur de remplissage du modele:
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@ -114,6 +132,7 @@ PrintSettingsDialog.lbl.Paperorientation = Orientation du papier:
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PrintSettingsDialog.but.Reset = Réinitialiser
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PrintSettingsDialog.but.Close = Fermer
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! Bug Report dialog
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bugreport.dlg.title = Rapport d'erreurs
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bugreport.dlg.but.Sendbugreport = Envoyer un rapport d'erreurs
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@ -129,6 +148,8 @@ bugreport.dlg.failedmsg2 = S'il vous plait envoyez le rapport manuellement
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bugreport.dlg.failedmsg3 = Erreur d'envoi du rapport
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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.
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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>
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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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@ -162,13 +183,12 @@ edtmotorconfdlg.lbl.Leavenamedefault = Laisser le champ vide par d
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! Example design dialog
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exdesigndlg.but.open = Ouvrir
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exdesigndlg.lbl.Selectexample = Chosir l'exemple de projet à ouvrir:
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exdesigndlg.lbl.Selectexample = Choisir l'exemple de projet à ouvrir:
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exdesigndlg.lbl.Openexampledesign = Ouvrir un exemple de projet
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exdesigndlg.lbl.Exampledesignsnotfound = Impossible de trouver les exemples de projets.
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exdesigndlg.lbl.Examplesnotfound = Exemples non trouvés
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! Material edit panel
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matedtpan.but.new = Nouveau
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matedtpan.but.edit = Editer
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@ -235,6 +255,7 @@ pref.dlg.lbl.Temperature = Temp
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pref.dlg.lbl.Momentofinertia = Moment d'inertie:
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pref.dlg.lbl.Pressure = Pression:
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pref.dlg.lbl.Stability = Stabilité:
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pref.dlg.lbl.FlightTime = Durée du vol:
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pref.dlg.lbl.effect1 = Les changements prendront effet la prochaine fois que vous ouvrirez une fenêtre.
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pref.dlg.lbl.Checkingupdates = Recherche des mises à jour...
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pref.dlg.lbl.msg1 = Une erreur est survenue durant la communication avec le serveur.
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@ -288,6 +309,10 @@ simedtdlg.lbl.ttip.Pressure = Pression atmosph
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simedtdlg.lbl.Launchsite = Site de lancement
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simedtdlg.lbl.Latitude = Latitude:
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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.
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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 = Altitude:
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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.
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simedtdlg.border.Launchrod = Rampe de lancement
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@ -306,6 +331,8 @@ simedtdlg.lbl.ExtBarrowman = Barrowman
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simedtdlg.lbl.Simmethod = Méthode de Simulation:
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simedtdlg.lbl.ttip.Simmethod1 = <html>Le simulateur de six degrés de liberté permet la liberté totale de fusée en vol.<br>
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simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.
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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 = Règlage du pas de temps:
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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>
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simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of
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@ -327,6 +354,12 @@ simedtdlg.IntensityDesc.High = Haute
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simedtdlg.IntensityDesc.Veryhigh = Très haute
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simedtdlg.IntensityDesc.Extreme = Extreme
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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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@ -370,6 +403,7 @@ SimuRunDlg.msg.unknownerror1 = Une erreur inconnue s'est produite lors de la sim
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SimuRunDlg.msg.unknownerror2 = Le programme peut être instable, vous devez enregistrer toutes vos créations et redémarrez OpenRocket maintenant!
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! SimulationExportPanel
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SimExpPan.desc = Fichiers dont les données sont séparées par une virgule (*.csv)
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SimExpPan.border.Vartoexport = Variables à exporter
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@ -398,6 +432,12 @@ SimExpPan.ExportingVar.desc3 = variable sur un total de
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SimExpPan.Col.Variable = Variable
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SimExpPan.Col.Unit = Unité
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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 = Courbe du moteur
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MotorPlot.but.Select = Selection
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@ -432,8 +472,6 @@ simplotpanel.LEFT_NAME = Gauche
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simplotpanel.RIGHT_NAME = Droite
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simplotpanel.CUSTOM = Personnalisé
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! Component add buttons
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compaddbuttons.Bodycompandfinsets = Pièces du corps et ailerons
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compaddbuttons.Nosecone = Cône
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@ -493,6 +531,7 @@ componentanalysisdlg.println.settingnam = SETTING NAN VALUES
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componentanalysisdlg.lbl.reflenght = Longueur de référence:
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componentanalysisdlg.lbl.refarea = Aire de référence:
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!componentanalysisdlg.but.close =Fermer
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componentanalysisdlg.TabStability.Col.Component = Pièce
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! Custom Material dialog
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custmatdlg.title.Custommaterial = Matériau personnalisé
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@ -521,7 +560,6 @@ ringcompcfg.EngineBlock.desc = <html>Un <b>bloc moteur </b> emp
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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.
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! Body Tube Config
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BodyTubecfg.lbl.Bodytubelength = Longueur du tube:
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BodyTubecfg.lbl.Outerdiameter = Diamètre externe:
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@ -604,9 +642,9 @@ RocketCompCfg.lbl.Length = Longueur:
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RocketCompCfg.lbl.Thickness = Epaisseur:
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RocketCompCfg.checkbox.Endcapped = Arrière clos
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RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped.
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RocketCompCfg.title.Noseconeshoulder = accotement du cône
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RocketCompCfg.title.Aftshoulder = accotement arrière
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RocketCompCfg.border.Foreshoulder = Fore shoulder
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RocketCompCfg.title.Noseconeshoulder = Accotement du cône
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RocketCompCfg.title.Aftshoulder = Accotement arrière
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RocketCompCfg.border.Foreshoulder = Accotement avant
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!RocketCompCfg.lbl.Length = Length:
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! BulkheadConfig
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@ -654,10 +692,12 @@ FreeformFinSetCfg.lbl.Posrelativeto = Position par rapport
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FreeformFinSetCfg.lbl.plus = plus
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FreeformFinSetCfg.lbl.FincrossSection = Coupe de l'aileron:
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FreeformFinSetCfg.lbl.Thickness = Epaisseur:
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FreeformFinSetCfg.lbl.Double-click = Double-click
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FreeformFinSetCfg.lbl.toedit = pour editer
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FreeformFinSetCfg.lbl.Clickdrag = Cliquer+déplacer: Ajouter et déplacer des points
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FreeformFinSetCfg.lbl.Ctrlclick = Ctrl+cliquer: Enlever un point
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! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
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FreeformFinSetCfg.lbl.doubleClick1 = Double-click
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FreeformFinSetCfg.lbl.doubleClick2 = pour editer
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FreeformFinSetCfg.lbl.clickDrag = Cliquer+déplacer: Ajouter et déplacer des points
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FreeformFinSetCfg.lbl.ctrlClick = Ctrl+cliquer: Enlever un point
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!InnerTubeConfig
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InnerTubeCfg.tab.Motor = Moteur
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@ -897,25 +937,39 @@ TCMotorSelPan.title.Thrustcurve = Courbe de pouss
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TCMotorSelPan.title.Thrust = Poussée
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TCMotorSelPan.delayBox.None = Aucun
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! PlotDialog
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PlotDialog.title.Flightdataplot = Tracé du vol
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PlotDialog.Chart.Simulatedflight = Simulation du vol
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PlotDialog.CheckBox.Showdatapoints = Afficher un point pour chaque valeur
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PlotDialog.lbl.Chart = Cliquer+déplacer en bas +droite pour agrandir, haut+gauche pour rétrécir
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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 = Fichier
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main.menu.file.desc = File-handling related tasks
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main.menu.file.new = Nouveau
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main.menu.file.new.desc = Create a new rocket design
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main.menu.file.open = Ouvrir...
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BasicFrame.item.Openrocketdesign = Open a rocket design
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main.menu.file.openExample = Ouvrir exemple...
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BasicFrame.item.Openexamplerocketdesign = Open an example rocket design
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main.menu.file.save = Sauvegarder
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BasicFrame.item.SavecurRocketdesign = Save the current rocket design
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main.menu.file.saveAs = Sauvegarder sous...
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main.menu.file.print = Imprimer...
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BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
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main.menu.file.print = Imprimer/Exporter en PDF...
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main.menu.file.print.desc = Print or save as PDF the parts list and fin templates
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main.menu.file.close = Fermer
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BasicFrame.item.Closedesign = Ferme le projet fusée en cour
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main.menu.file.quit = Quitter
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BasicFrame.item.Quitprogram = Quitte le programme
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main.menu.edit = Editer
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BasicFrame.menu.Rocketedt = Rocket editing
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main.menu.edit.undo = Annuler modification
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main.menu.edit.undo.desc = Annuler l'opération précédente
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main.menu.edit.redo = Refaire modification
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@ -925,16 +979,27 @@ main.menu.edit.copy = Copier
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main.menu.edit.paste = Coller
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main.menu.edit.delete = Effacer
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main.menu.edit.resize = Redimensionner...
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main.menu.edit.resize.desc = Scale parts of the rocket design
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main.menu.edit.preferences = Préférences
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main.menu.edit.preferences.desc = Setup the application preferences
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main.menu.analyze = Analyse
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main.menu.analyze.desc = Rocket analysis
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main.menu.analyze.componentAnalysis = Analyse des Pièces
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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 = Aide
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main.menu.help.desc = Information à propos d'OpenRocket
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main.menu.help.license = Licence
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main.menu.help.license.desc = OpenRocket license information
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main.menu.help.bugReport = Rapport d'erreurs
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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 = A propos
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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 = Quel est ce menu?
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@ -966,13 +1031,14 @@ Databases.materials.Spruce = Sapin
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Databases.materials.StyrofoamgenericEPS = Polystyrène (générique EPS)
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Databases.materials.StyrofoamBluefoamXPS = \"Mousse Bleue\" de polystyrène (XPS)
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Databases.materials.Quantumtubing = Tube Quantum
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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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Databases.materials.Polyethylenethin = Polyéthylène (fin)
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Databases.materials.Polyethyleneheavy = Polyéthylène (lourd)
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Databases.materials.Silk = Soie
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Databases.materials.Paperoffice1 = Papier (bureau)
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Databases.materials.Paperoffice = Papier (bureau)
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Databases.materials.Cellophane = Cellophane
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Databases.materials.Crepepaper = Cr\u00eape paper
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! LINE_MATERIAL
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@ -995,7 +1061,6 @@ ExternalComponent.Regularpaint = Peinture classique
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ExternalComponent.Smoothpaint = Fine couche
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ExternalComponent.Polished = Polie
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! LineStyle
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LineStyle.Solid = Ligne pleine
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LineStyle.Dashed = Tiret
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@ -1031,7 +1096,6 @@ RocketComponent.Position.BOTTOM = Bas de la pi
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RocketComponent.Position.AFTER = Après la pièce parent
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RocketComponent.Position.ABSOLUTE = Pointe de l'ogive
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! LaunchLug
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LaunchLug.Launchlug = Tube de guidage
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! NoseCone
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@ -1198,6 +1262,9 @@ FlightDataType.TYPE_AIR_PRESSURE = Pression atmosph
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FlightDataType.TYPE_SPEED_OF_SOUND = Vitesse du son
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FlightDataType.TYPE_TIME_STEP = Pas de simulation du temps
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FlightDataType.TYPE_COMPUTATION_TIME = Temps de calcul
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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 = Mouvement vertical par rapport au temps
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@ -1236,7 +1303,9 @@ ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and r
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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 = Redimensionner
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ScaleDialog.undo.scaleRocket = Redimensionner la fusée
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ScaleDialog.undo.scaleComponent = Redimensionner une pièce
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ScaleDialog.undo.scaleComponents = Redimensionner les pièces
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!icons
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Icons.Undo = Undo
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@ -1256,16 +1325,181 @@ EllipticalFinSet.Ellipticalfinset = Ailerons elyptique
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! Modifiers
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optimization.modifier.nosecone.length = Longuer du cone
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optimization.modifier.nosecone.length = Longueur du cone
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optimization.modifier.nosecone.length.desc = Optimise la longueur du cone.
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optimization.modifier.nosecone.diameter = Diamètre du Cone
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optimization.modifier.nosecone.diameter.desc = Optimise le diamètre du cone.
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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
|
||||
|
||||
Loading…
x
Reference in New Issue
Block a user