+optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.\r
+\r
+optimization.modifier.trapezoidfinset.rootChord = Root chord\r
+optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).\r
+optimization.modifier.trapezoidfinset.tipChord = Tip chord\r
+optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).\r
+optimization.modifier.trapezoidfinset.sweep = Sweep\r
+optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).\r
+optimization.modifier.trapezoidfinset.height = Height\r
+optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
+\r
+optimization.modifier.ellipticalfinset.length = Root chord\r
+optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.\r
+optimization.modifier.ellipticalfinset.height = Height\r
+optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
+\r
+optimization.modifier.finset.cant = Cant angle\r
+optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.\r
+optimization.modifier.finset.position = Position\r
+optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.\r
+\r
+optimization.modifier.launchlug.length = Longueur\r
+optimization.modifier.launchlug.length.desc = Optimize the launch lug length.\r
+optimization.modifier.launchlug.outerDiameter = Outer diameter\r
+optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.\r
+optimization.modifier.launchlug.thickness = Thickness\r
+optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.\r
+optimization.modifier.launchlug.position = Position\r
+optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.\r
+\r
+\r
+optimization.modifier.internalcomponent.position = Position\r
+optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.\r
+\r
+optimization.modifier.masscomponent.mass = Mass\r
+optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.\r
+\r
+optimization.modifier.parachute.diameter = Diameter\r
+optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.\r
+optimization.modifier.parachute.coefficient = Drag coefficient\r
+optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.\r
+\r
+optimization.modifier.streamer.length = Longueur\r
+optimization.modifier.streamer.length.desc = Optimize the length of the streamer.\r
+optimization.modifier.streamer.width = Width\r
+optimization.modifier.streamer.width.desc = Optimize the width of the streamer.\r
+optimization.modifier.streamer.aspectRatio = Aspect ratio\r
+optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.\r
+optimization.modifier.streamer.coefficient = Drag coefficient\r
+optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.\r
+\r
+optimization.modifier.recoverydevice.deployDelay = Deployment delay\r
+optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.\r
+optimization.modifier.recoverydevice.deployAltitude = Deployment altitude\r
+optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.\r
+\r
+optimization.modifier.rocketcomponent.overrideMass = Override mass\r
+optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.\r
+optimization.modifier.rocketcomponent.overrideCG = Override CG\r
+optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.\r
+\r
+optimization.modifier.motormount.overhang = Motor overhang\r
+optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.\r
+optimization.modifier.motormount.delay = Motor ignition delay\r
+optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.\r
+\r
+\r
+\r
+\r
+! General rocket design optimization dialog\r
+\r
+GeneralOptimizationDialog.title = Rocket optimization\r
+GeneralOptimizationDialog.goal.maximize = Maximize value\r
+GeneralOptimizationDialog.goal.minimize = Minimize value\r
+GeneralOptimizationDialog.goal.seek = Seek value of\r
+GeneralOptimizationDialog.btn.start = Démarrer l'optimization\r
+GeneralOptimizationDialog.btn.stop = Terminer l'optimization\r
+GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:\r
+GeneralOptimizationDialog.btn.add = Ajouter\r
+GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization\r
+GeneralOptimizationDialog.btn.remove = Enlever\r
+GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization\r
+GeneralOptimizationDialog.btn.removeAll = Remove all\r
+GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization\r
+GeneralOptimizationDialog.lbl.availableParams = Parametres disponible:\r
+GeneralOptimizationDialog.lbl.optimizationOpts = Options pour l'optimization\r
+GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:\r
+GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize\r
+GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:\r
+GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized\r
+GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:\r
+GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization\r
+GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek\r
+GeneralOptimizationDialog.lbl.requireStability = Required stability\r
+GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:\r
+GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design\r
+GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:\r
+GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design\r
+GeneralOptimizationDialog.status.bestValue = Best value:\r
+GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.\r
+GeneralOptimizationDialog.status.stepCount = Step count:\r
+GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.\r
+GeneralOptimizationDialog.status.evalCount = Evaluations:\r
+GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.\r
+GeneralOptimizationDialog.status.stepSize = Step size:\r
+GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)\r
+GeneralOptimizationDialog.btn.plotPath = Plot path\r
+GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)\r
+GeneralOptimizationDialog.btn.save = Save path\r
+GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.\r
+GeneralOptimizationDialog.btn.apply = Apply optimization\r
+GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design\r
+GeneralOptimizationDialog.btn.reset = Reset\r
+GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design\r
+GeneralOptimizationDialog.btn.close = Fermer\r
+GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design\r
+GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.\r
+GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters\r
+GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:\r
+GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed\r
+GeneralOptimizationDialog.undoText = Apply optimization\r
+GeneralOptimizationDialog.basicSimulationName = Simulation simple\r
+GeneralOptimizationDialog.noSimulationName = Pas de simulation\r
+GeneralOptimizationDialog.table.col.parameter = Parameter\r
+GeneralOptimizationDialog.table.col.current = Current\r
+GeneralOptimizationDialog.table.col.min = Minimum\r
+GeneralOptimizationDialog.table.col.max = Maximum\r
+GeneralOptimizationDialog.export.header = Include header line\r
+GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.\r
+GeneralOptimizationDialog.export.stability = Stabilité\r
+\r
+\r
+! Dialog for plotting optimization results\r
+OptimizationPlotDialog.title = Résultats de l'optimisation\r
+OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out\r
+OptimizationPlotDialog.plot1d.title = Optimization result\r
+OptimizationPlotDialog.plot1d.series = Optimization result\r
+OptimizationPlotDialog.plot2d.title = Optimization path\r
+OptimizationPlotDialog.plot2d.path = Optimization path\r
+OptimizationPlotDialog.plot2d.evals = Evaluations\r
+OptimizationPlotDialog.plot.ttip.stability = Stabilité:\r
+OptimizationPlotDialog.plot.label.optimum = Optimum\r
+\r
+! Optimization parameters\r
+MaximumAltitudeParameter.name = Altitude de l'apogée\r
+MaximumVelocityParameter.name = Maximum velocity\r
+MaximumAccelerationParameter.name = Accelération maximum\r
+StabilityParameter.name = Stabilité\r
+GroundHitVelocityParameter.name = Vitesse à l'atterrissage\r
+LandingDistanceParameter.name = Distance à l'attérrissage\r
+TotalFlightTimeParameter.name = Durée totale du vol\r
+DeploymentVelocityParameter.name = Velocity at parachute deployment\r