Added latest French and Spanish translations
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@ -59,14 +59,6 @@ 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.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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@ -77,11 +69,11 @@ BasicFrame.WarningDialog.txt2 = Certains elements du projet n'ont peut etre pas
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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.fileExists.title = Le fichier existe déjà
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error.fileExists.desc = Le fichier '{filename}' existe déjà. Voulez vous l'ecraser?
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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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error.writing.title = Erreur d'ecriture du fichier
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error.writing.desc = Une erreur est survenue lors de l'ecriture dans le fichier:
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! Labels used in buttons of dialog windows
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button.ok = OK
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@ -95,7 +87,7 @@ dlg.but.close = Fermer
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! General file type names
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filetypes.pdf = PDF files
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filetypes.pdf = fichier PDF
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! About Dialog
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@ -112,7 +104,7 @@ AboutDialog.lbl.translatorIcon = logoTripoliFrance.png
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! Print dialog
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PrintDialog.title = Imprimer ou exporter
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PrintDialog.but.previewAndPrint = Previsualiser et imprimer
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PrintDialog.but.previewAndPrint = Prévisualiser et imprimer
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PrintDialog.checkbox.showByStage = Montrer par étage
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PrintDialog.lbl.selectElements = Choisir les elements à inclure:
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printdlg.but.saveaspdf = Sauvegarder en PDF
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@ -125,9 +117,9 @@ PrintDialog.error.preview.desc2 = S'il vous plait utilisez l'option "Sauvegarder
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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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PrintSettingsDialog.lbl.Templatefillcolor = Couleur de remplissage du modéle:
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PrintSettingsDialog.lbl.Templatebordercolor = Couleur des bords du modéle:
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PrintSettingsDialog.lbl.Papersize = Dimessions du papier:
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PrintSettingsDialog.lbl.Papersize = Dimenssions du papier:
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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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@ -148,8 +140,8 @@ 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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bugreport.dlg.provideDescription = S'il vous plait veuillez fournir d'abord une description du bug.
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bugreport.dlg.provideDescription.title = La description du bug est absente
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! Debug log dialog
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@ -193,7 +185,7 @@ exdesigndlg.lbl.Examplesnotfound = Exemples non trouv
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matedtpan.but.new = Nouveau
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matedtpan.but.edit = Editer
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matedtpan.but.delete = Effacer
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matedtpan.but.revertall = Revenir aux valeurs précédente
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matedtpan.but.revertall = Revenir aux valeurs précédentes
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matedtpan.col.Material = Matériaux
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matedtpan.col.Type = Type
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matedtpan.col.Density = Densité
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@ -311,7 +303,7 @@ 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.ttip.Longitude = <html>Neccessaire pour les prédictions du temps 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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@ -331,7 +323,7 @@ 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.GeodeticMethod = Calculs Geodetic:
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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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@ -354,9 +346,9 @@ 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.none.name = Aucune
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GeodeticComputationStrategy.none.desc = Ne pas faire de calculs geodeti.
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GeodeticComputationStrategy.spherical.name = Aproximation sphérique
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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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@ -381,7 +373,7 @@ simpanel.dlg.lbl.DeleteSim3 = Effacer les simulations
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simpanel.col.Name = Nom
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simpanel.col.Motors = Moteurs
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simpanel.col.Apogee = Apogée
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simpanel.col.Maxvelocity = Vélocité Max.
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simpanel.col.Maxvelocity = Vitesse Max.
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simpanel.col.Maxacceleration = Accélération Max.
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simpanel.col.Timetoapogee = Temps pour atteindre l'apogée
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simpanel.col.Flighttime = Temps de vol
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@ -392,7 +384,7 @@ SimuRunDlg.title.RunSim = Simulations en cour...
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SimuRunDlg.lbl.Running = En cour ...
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SimuRunDlg.lbl.Simutime = Temps de simulation:
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SimuRunDlg.lbl.Altitude = Altitude:
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SimuRunDlg.lbl.Velocity = Vélocité:
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SimuRunDlg.lbl.Velocity = Vitesse:
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SimuRunDlg.msg.Unabletosim = Simulation impossible:
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SimuRunDlg.msg.errorOccurred = Une erreur s'est produite durant la simulation:
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SimuRunDlg.msg.AnException1 = Une exception s'est produite lors de la simulation:
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@ -568,7 +560,7 @@ BodyTubecfg.lbl.Wallthickness = Epaisseur des parois:
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BodyTubecfg.tab.General = Général
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BodyTubecfg.tab.Generalproperties = Propriétés générales
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BodyTubecfg.tab.Motor = Moteur
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BodyTubecfg.tab.Motormountconf = Configuration porte moteur
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BodyTubecfg.tab.Motormountconf = Configuration du porte moteur
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BodyTubecfg.checkbox.Automatic = Automatique
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BodyTubecfg.checkbox.Filled = Aspérités bouchées
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@ -641,7 +633,7 @@ RocketCompCfg.lbl.Diameter = Diam
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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.ttip.Endcapped = Precise si l'arriere du cone est clos.
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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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@ -761,9 +753,9 @@ MotorCfg.but.Removemotor = Enlever le moteur
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MotorCfg.lbl.motorLabel = Aucun
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! NoseConeConfig
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NoseConeCfg.lbl.Noseconeshape = Forme du nez de la fusée:
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NoseConeCfg.lbl.Noseconeshape = Forme du cone de la fusée:
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NoseConeCfg.lbl.Shapeparam = Paramètre de la forme:
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NoseConeCfg.lbl.Noseconelength = Longueur du nez de la fusée:
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NoseConeCfg.lbl.Noseconelength = Longueur du cone de la fusée:
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NoseConeCfg.lbl.Basediam = Diamètre de la base:
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NoseConeCfg.checkbox.Automatic = Automatique
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NoseConeCfg.lbl.Wallthickness = Epaisseur de la paroi:
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@ -825,7 +817,7 @@ SleeveCfg.tab.Generalproperties = Propri
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StreamerCfg.lbl.Striplength = Longueur de la bande:
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StreamerCfg.lbl.Stripwidth = Largeur de la bande:
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StreamerCfg.lbl.Striparea = Surface de la bande:
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StreamerCfg.lbl.Aspectratio = Aspect ratio:
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StreamerCfg.lbl.Aspectratio = Proportions:
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StreamerCfg.lbl.Material = Matériau:
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StreamerCfg.combo.ttip.MaterialModel = La nature du matériau affecte le poids de la pièce.
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StreamerCfg.lbl.longA1 = <html>Coefficient de traînée C<sub>D</sub>:
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@ -952,54 +944,54 @@ PlotDialog.lbl.Chart = Cliquer+d
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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.new.desc = Crée un nouveau projet fusée
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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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BasicFrame.item.Openrocketdesign = Ouvre un projet fusée
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main.menu.file.openExample = Ouvrir un exemple...
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BasicFrame.item.Openexamplerocketdesign = Ouvre un exemple de projet fusée
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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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BasicFrame.item.SavecurRocketdesign = Sauvegarde le projet fusée en cours
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main.menu.file.saveAs = Sauvegarder sous...
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BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
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BasicFrame.item.SavecurRocketdesnewfile = Sauvegarde le projet fusée en cour dans un nouveau fichier
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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.print.desc = Imprimer ou sauvegarde en PDF la liste des pieces et les gabaries des ailerons
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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 = Modifier
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BasicFrame.menu.Rocketedt = Modification de la fusée
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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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main.menu.edit.redo.desc = Redo the previously undone operation
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main.menu.edit.redo.desc = Refaire l'opération precedente qui avait été défaite
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main.menu.edit.cut = Couper
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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.resize.desc = Redimensionner certaines parties de la fusée
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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.edit.preferences.desc = Configure les préférences de l'application
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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.desc = Analyses de la fusée
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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.analyze.componentAnalysis.desc = Analyse séparé des pices de la fusée
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main.menu.analyze.optimization = Optimisation de la fusée
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main.menu.analyze.optimization.desc = Optimisation generale de la fusée
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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.license.desc = Information sur la license d'OpenRocket
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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.bugReport.desc = Information pour pouvoir sgnaler les bugs dans 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.debugLog.desc = Visualiser le fichier log d'OpenRocket
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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.help.about.desc = Détails du Copyright d'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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@ -1040,7 +1032,7 @@ Databases.materials.Polyethyleneheavy = Poly
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Databases.materials.Silk = Soie
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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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Databases.materials.Crepepaper = Papier crepon
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! LINE_MATERIAL
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Databases.materials.Threadheavy-duty = Fil(résistant)
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Databases.materials.Elasticcordround2mm = Corde Elastique (ronde 2mm, 1/16 in)
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@ -1131,7 +1123,7 @@ Rocket.compname.Rocket = Fus
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MotorMount.IgnitionEvent.AUTOMATIC = Automatique (lancement ou charge d'éjection)
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MotorMount.IgnitionEvent.LAUNCH = Lancement
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MotorMount.IgnitionEvent.EJECTION_CHARGE = Premiere charge d'ejection ou étage precedent
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MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
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MotorMount.IgnitionEvent.BURNOUT = Premiere combustion total de létage precedente
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MotorMount.IgnitionEvent.NEVER = Jamais
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!ComponentIcons
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@ -1150,7 +1142,7 @@ ComponentIcons.Engineblock = Bague de retension moteur
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ComponentIcons.Parachute = Parachute
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ComponentIcons.Streamer = Banderolle
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ComponentIcons.Shockcord = Cordon amortisseur
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ComponentIcons.Masscomponent = Mass component
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ComponentIcons.Masscomponent = Piéce Masse
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ComponentIcons.disabled = (désactivé)
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! StageAction
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@ -1270,7 +1262,7 @@ FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration
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PlotConfiguration.Verticalmotion = Mouvement vertical par rapport au temps
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PlotConfiguration.Totalmotion = Mouvement total par rapport au temps
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PlotConfiguration.Flightside = Flight side profile
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PlotConfiguration.Stability = Stabilité par rapport temps
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PlotConfiguration.Stability = Stabilité par rapport au temps
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PlotConfiguration.Dragcoef = Coefficients de traînée par rapport au Mach number
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PlotConfiguration.Rollcharacteristics = Caractéristiques de roulis
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PlotConfiguration.Angleofattack = Angle d'attaque et orientation par rapport au temps
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@ -1330,28 +1322,28 @@ 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
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optimization.modifier.nosecone.thickness.desc = Optimize l'epasseur des paroies du cone.
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optimization.modifier.nosecone.thickness.desc = Optimise l'epasseur des paroies du cone.
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optimization.modifier.nosecone.shapeparameter = Parametre de la forme
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optimization.modifier.nosecone.shapeparameter.desc = Optimise les parametres de forme du cone.
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optimization.modifier.transition.length = Longueur de la Transition
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optimization.modifier.transition.length.desc = Optimise la longueur de la transition.
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optimization.modifier.transition.forediameter = Transition fore diameter
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optimization.modifier.transition.forediameter = Diametre avant de la Transition
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optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.
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optimization.modifier.transition.aftdiameter = Transition aft diameter
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optimization.modifier.transition.aftdiameter = Diametre arriere de la transition
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optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.
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optimization.modifier.transition.thickness = Epaisseur de la transition
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optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.
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optimization.modifier.transition.shapeparameter = Shape parameter
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optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.
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optimization.modifier.transition.thickness.desc = Optimise l'epaisseurs des paroies de la transition.
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optimization.modifier.transition.shapeparameter = Parametre de la forme
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optimization.modifier.transition.shapeparameter.desc = Optimise le parametre de la forme.
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optimization.modifier.bodytube.length = Longueur du tube du corps
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optimization.modifier.bodytube.length.desc = Optimise la longueur du tube.
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optimization.modifier.bodytube.length.desc = Optimise la longueur du tube du corps.
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optimization.modifier.bodytube.outerDiameter = Diamètre externe du tube du corps
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optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.
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optimization.modifier.bodytube.innerDiameter = Body tube inner diameter
|
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optimization.modifier.bodytube.outerDiameter.desc = Optimise le diametre externe du tube du corps tout en maintenant l'epaisseur des paroies.
|
||||
optimization.modifier.bodytube.innerDiameter = Diametre interne du tube du corps
|
||||
optimization.modifier.bodytube.thickness = Epaisseur du tube du corps
|
||||
optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.
|
||||
optimization.modifier.bodytube.thickness.desc = Optimise l'epaisseur des paroies du tube du corps.
|
||||
|
||||
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).
|
||||
@ -1359,24 +1351,24 @@ 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 = Hauteur
|
||||
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 = Hauteur
|
||||
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.finset.position.desc = Optimisation de la position du jeux d'ailerons sur le corps de la fusée.
|
||||
|
||||
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.length.desc = Optimisation de la longueur du tube de guidage.
|
||||
optimization.modifier.launchlug.outerDiameter = Diametre externe
|
||||
optimization.modifier.launchlug.outerDiameter.desc = Optimisation du diametre externe du tube de guidage.
|
||||
optimization.modifier.launchlug.thickness = Epaisseur
|
||||
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.
|
||||
@ -1385,72 +1377,72 @@ optimization.modifier.launchlug.position.desc = Optimize the launch lug position
|
||||
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 = Masse
|
||||
optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.
|
||||
|
||||
optimization.modifier.parachute.diameter = Diameter
|
||||
optimization.modifier.parachute.diameter = Diametre
|
||||
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.parachute.coefficient.desc = Optimisation du coéfficient de trainée du 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.length.desc = Optimisation de la longueur de la banderolle (streamer).
|
||||
optimization.modifier.streamer.width = Largeur
|
||||
optimization.modifier.streamer.width.desc = Optimisation de la largeur de la banderolle (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.streamer.coefficient = Coefficient de trainée
|
||||
optimization.modifier.streamer.coefficient.desc = Optimisation du coéfficient de trainée de la banderolle (streamer).
|
||||
|
||||
optimization.modifier.recoverydevice.deployDelay = Deployment delay
|
||||
optimization.modifier.recoverydevice.deployDelay = Retard du deploiement
|
||||
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.recoverydevice.deployAltitude = Altitude du deploiement
|
||||
optimization.modifier.recoverydevice.deployAltitude.desc = Optimise l'altitude de déploiement du dispositif de récupération.
|
||||
|
||||
optimization.modifier.rocketcomponent.overrideMass = Override mass
|
||||
optimization.modifier.rocketcomponent.overrideMass = Forcer la masse
|
||||
optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.
|
||||
optimization.modifier.rocketcomponent.overrideCG = Override CG
|
||||
optimization.modifier.rocketcomponent.overrideCG = forcer le 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.
|
||||
optimization.modifier.motormount.delay = Retard de l'alumage moteur
|
||||
optimization.modifier.motormount.delay.desc = Optimisation du retard d'alumage du moteur.
|
||||
|
||||
|
||||
|
||||
|
||||
! General rocket design optimization dialog
|
||||
|
||||
GeneralOptimizationDialog.title = Rocket optimization
|
||||
GeneralOptimizationDialog.title = Optimisation de la fusée
|
||||
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.lbl.paramsToOptimize = Parametres à optimiser:
|
||||
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.btn.removeAll = Tout enlever
|
||||
GeneralOptimizationDialog.btn.removeAll.ttip = Enlever tous les parametres de l'optimisation
|
||||
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.optimizeSim = Optimiser la simulation:
|
||||
GeneralOptimizationDialog.lbl.optimizeSim.ttip = Choisir la simulation à optimiser
|
||||
GeneralOptimizationDialog.lbl.optimizeValue = Valeur optimum
|
||||
GeneralOptimizationDialog.lbl.optimizeValue.ttip = Choisir quelle valeur à optimiser
|
||||
GeneralOptimizationDialog.lbl.optimizeGoal = But de l'optimisation:
|
||||
GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Choisir le but de l'optimisation
|
||||
GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek
|
||||
GeneralOptimizationDialog.lbl.requireStability = Required stability
|
||||
GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:
|
||||
GeneralOptimizationDialog.lbl.requireStability = Stabilité désirée
|
||||
GeneralOptimizationDialog.lbl.requireMinStability = Stabilité minimum:
|
||||
GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design
|
||||
GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:
|
||||
GeneralOptimizationDialog.lbl.requireMaxStability = Stabilité maximum:
|
||||
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.bestValue = Meilleure valeur:
|
||||
GeneralOptimizationDialog.status.bestValue.ttip = Meilleure valeur optimum trouvé jusqu'à present.
|
||||
GeneralOptimizationDialog.status.stepCount = Step count:
|
||||
GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.
|
||||
GeneralOptimizationDialog.status.evalCount = Evaluations:
|
||||
@ -1463,22 +1455,22 @@ 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 = Re-initialiser
|
||||
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.btn.close.ttip = Fermer la fenetre de dialogue sans modifier la fusée
|
||||
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.error.selectParams.title = Choisir les parametres de l'optimisation
|
||||
GeneralOptimizationDialog.error.optimizationFailure.text = L'optimisation n'a pas fonctionnée:
|
||||
GeneralOptimizationDialog.error.optimizationFailure.title = L'optimisation n'a pas réussie
|
||||
GeneralOptimizationDialog.undoText = Appliquer l'optimisation
|
||||
GeneralOptimizationDialog.basicSimulationName = Simulation simple
|
||||
GeneralOptimizationDialog.noSimulationName = Pas de simulation
|
||||
GeneralOptimizationDialog.table.col.parameter = Parameter
|
||||
GeneralOptimizationDialog.table.col.current = Current
|
||||
GeneralOptimizationDialog.table.col.parameter = Parametre
|
||||
GeneralOptimizationDialog.table.col.current = Courrant
|
||||
GeneralOptimizationDialog.table.col.min = Minimum
|
||||
GeneralOptimizationDialog.table.col.max = Maximum
|
||||
GeneralOptimizationDialog.export.header = Include header line
|
||||
GeneralOptimizationDialog.export.header = Inclure la ligne d'en tete
|
||||
GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.
|
||||
GeneralOptimizationDialog.export.stability = Stabilité
|
||||
|
||||
@ -1486,20 +1478,20 @@ GeneralOptimizationDialog.export.stability = Stabilit
|
||||
! 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.plot1d.title = Resultat de l'optimisation
|
||||
OptimizationPlotDialog.plot1d.series = Resultat de l'optimisation
|
||||
OptimizationPlotDialog.plot2d.title = Optimization path
|
||||
OptimizationPlotDialog.plot2d.path = Optimization path
|
||||
OptimizationPlotDialog.plot2d.path = Chemin pour l'optimisation
|
||||
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
|
||||
MaximumVelocityParameter.name = Vitesse maximum
|
||||
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
|
||||
DeploymentVelocityParameter.name = Vitesse lors de l'ouverture du parachute
|
||||
|
Loading…
x
Reference in New Issue
Block a user