simedtdlg.lbl.Launchsite = Launch site
simedtdlg.lbl.Latitude = Latitude:
simedtdlg.lbl.ttip.Latitude = <html>The launch site latitude affects the gravitational pull of Earth.<br>Positive values are on the Northern hemisphere, negative values on the Southern hemisphere.
+
+simedtdlg.lbl.Longitude = Longitude:
+simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.
+
simedtdlg.lbl.Altitude = Altitude:
simedtdlg.lbl.ttip.Altitude = <html>The launch altitude above mean sea level.<br>This affects the position of the rocket in the atmospheric model.
simedtdlg.border.Launchrod = Launch rod
simedtdlg.lbl.Simmethod = Simulation method:
simedtdlg.lbl.ttip.Simmethod1 = <html>The six degree-of-freedom simulator allows the rocket total freedom during flight.<br>
simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.
+simedtdlg.lbl.GeodeticMethod = Geodetic calculations:
+simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.
simedtdlg.lbl.Timestep = Time step:
simedtdlg.lbl.ttip.Timestep1 = <html>The time between simulation steps.<br>A smaller time step results in a more accurate but slower simulation.<br>
simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of
simedtdlg.IntensityDesc.Veryhigh = Very high
simedtdlg.IntensityDesc.Extreme = Extreme
+GeodeticComputationStrategy.flat.name = Flat Earth
+GeodeticComputationStrategy.flat.desc = Perform computations with a flat Earth approximation. Sufficient for low-altitude flights.
+GeodeticComputationStrategy.spherical.name = Spherical approximation
+GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.
+GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid
+GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.
+
+
! Simulation Panel
!RocketCompCfg.lbl.Length = Length:
! BulkheadConfig
-BulkheadCfg.tab.Radius = Radius:
+BulkheadCfg.tab.Diameter = Diameter:
BulkheadCfg.tab.Thickness = Thickness:
BulkheadCfg.tab.General = General
BulkheadCfg.tab.Generalproperties = General properties
ParachuteCfg.lbl.plusdelay = plus
! ShockCordConfig
-ShockCordCfg.lbl.Shockcordlength = Shock cord length
+ShockCordCfg.lbl.Shockcordlength = Shock cord length:
ShockCordCfg.lbl.Shockcordmaterial = Shock cord material:
ShockCordCfg.lbl.Posrelativeto = Position relative to:
ShockCordCfg.lbl.plus = plus
Databases.materials.StyrofoamgenericEPS = Styrofoam (generic EPS)
Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"Blue foam\" (XPS)
Databases.materials.Quantumtubing = Quantum tubing
+Databases.materials.BlueTube = Blue tube
!SURFACE_MATERIAL
Databases.materials.Ripstopnylon = Ripstop nylon
Databases.materials.Mylar = Mylar
FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
FlightDataType.TYPE_TIME_STEP = Simulation time step
FlightDataType.TYPE_COMPUTATION_TIME = Computation time
+FlightDataType.TYPE_LATITUDE = Latitude
+FlightDataType.TYPE_LONGITUDE = Longitude
+FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration
! PlotConfiguration
PlotConfiguration.Verticalmotion = Vertical motion vs. time
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 = Optimize the height (semi-span) of the fin set.
+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.
OptimizationPlotDialog.plot2d.path = Optimization path
OptimizationPlotDialog.plot2d.evals = Evaluations
OptimizationPlotDialog.plot.ttip.stability = Stability:
+OptimizationPlotDialog.plot.label.optimum = Optimum
! Optimization parameters
MaximumAltitudeParameter.name = Apogee altitude
StabilityParameter.name = Stability
GroundHitVelocityParameter.name = Ground hit speed
LandingDistanceParameter.name = Landing distance
+TotalFlightTimeParameter.name = Total flight time
+DeploymentVelocityParameter.name = Velocity at parachute deployment
+
+
+! Compass directions drawn on a compass rose.
+CompassRose.lbl.north = N
+CompassRose.lbl.east = E
+CompassRose.lbl.south = S
+CompassRose.lbl.west = W
+
+! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
+CompassSelectionButton.lbl.N = N
+CompassSelectionButton.lbl.NE = NE
+CompassSelectionButton.lbl.E = E
+CompassSelectionButton.lbl.SE = SE
+CompassSelectionButton.lbl.S = S
+CompassSelectionButton.lbl.SW = SW
+CompassSelectionButton.lbl.W = W
+CompassSelectionButton.lbl.NW = NW
+