X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=core%2Fresources%2Fl10n%2Fmessages.properties;h=f982f0d14a29cad3fab2320edb56b6a343421de5;hb=4d97d149b0ef11eac895be021600613d3f152ad9;hp=0715bc7968fb823d3634ce75834294c6973fb87b;hpb=091345cb872e40e9e263c9b7accf2fee67c19aa5;p=debian%2Fopenrocket
diff --git a/core/resources/l10n/messages.properties b/core/resources/l10n/messages.properties
index 0715bc79..f982f0d1 100644
--- a/core/resources/l10n/messages.properties
+++ b/core/resources/l10n/messages.properties
@@ -169,6 +169,9 @@ debuglogdlg.lbl.Logmessage = Log message:
debuglogdlg.lbl.Stacktrace = Stack trace:
+! MotorChooserDialog
+MotorChooserDialog.title = Select a rocket motor
+
! Edit Motor configuration dialog
edtmotorconfdlg.but.removemotor = Remove motor
edtmotorconfdlg.but.Selectmotor = Select motor
@@ -454,14 +457,18 @@ customExpression.Description = Description
! Custom expression panel
customExpressionPanel.but.NewExpression = New expression
+customExpressionPanel.but.ttip.NewExpression = Add a new custom expression
+customExpressionPanel.but.Import = Import
+customExpressionPanel.but.ttip.Import = Import custom expressions from another .ork file
customExpressionPanel.lbl.UpdateNote = You must run the simulation before data will be available for plotting.
customExpressionPanel.lbl.CalcNote = Expressions will be calculated in the order shown.
-customExpressionPanel.lbl.CustomExpressions = Custom Expressions :
+customExpressionPanel.lbl.CustomExpressions = Custom Expressions
customExpression.Units.but.ttip.Remove = Remove this expression
customExpression.Units.but.ttip.Edit = Edit this expression
customExpression.Units.but.ttip.MoveUp = Move expression up in calculation order
customExpression.Units.but.ttip.MoveDown = Move expression down in calculation order
+
! Custom expression builder window
ExpressionBuilderDialog.title = Expression Builder
ExpressionBuilderDialog.InsertVariable = Insert Variable
@@ -482,12 +489,12 @@ CustomOperatorSelector.title = Operator Selector
Operator.plus = Addition
Operator.minus = Subtraction
Operator.star = Multiplication
-Operator.div = Divison
+Operator.div = Division
Operator.mod = Modulo
Operator.pow = Exponentiation
Operator.abs = Absolute value
-Operator.ceil = Ceiling (next integer value
-Operator.floor = Floor (previous integer value
+Operator.ceil = Ceiling (next integer value)
+Operator.floor = Floor (previous integer value)
Operator.sqrt = Square root
Operator.cbrt = Cubic root
Operator.exp = Euler\'s number raised to the value (e^x)
@@ -498,9 +505,24 @@ Operator.tan = Tangent
Operator.asin = Arc sine
Operator.acos = Arc cosine
Operator.atan = Arc tangent
-Operator.hsin = Hyerbolic sine
+Operator.hsin = Hyperbolic sine
Operator.hcos = Hyperbolic cosine
Operator.htan = Hyperbolic tangent
+Operator.log10 = Base 10 logarithm
+Operator.round = Round to nearest integer value
+Operator.random = Random number between zero and given value
+Operator.expm1 = The same as exp(x)-1, but more accurate for small x
+Operator.mean = The arithmetic mean of a given range
+Operator.min = The minimum value in a given range
+Operator.max = The maximum value in a given range
+Operator.var = The variance of a given range
+Operator.stdev = The standard deviation of a given range
+Operator.rms = The root-mean-squared value of a given range
+Operator.lclip = Clips a value (1st parameter) to be no less than a given value (2nd parameter)
+Operator.uclip = Clips a value (1st parameter) to be no greater than a given value (2nd parameter)
+Operator.binf = Gives the fraction of values in a given range (1st parameter) inside a bin with given lower (2nd parameter) and upper (3rd parameter) bounds
+Operator.trapz = Integrates the given range using trapezoidal integration
+Operator.tnear = Find the time corresponding to the point in a range (1st parameter) nearest to a given value (2nd parameter)
! MotorPlot
MotorPlot.title.Motorplot = Motor plot
@@ -1068,6 +1090,8 @@ main.menu.analyze.componentAnalysis = Component analysis
main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately
main.menu.analyze.optimization = Rocket optimization
main.menu.analyze.optimization.desc = General rocket design optimization
+main.menu.analyze.customExpressions = Custom expressions
+main.menu.analyze.customExpressions.desc = Define new flight data types by writing custom mathematical expressions
main.menu.help = Help
main.menu.help.desc = Information about OpenRocket
@@ -1090,7 +1114,13 @@ main.menu.debug.createtestrocket = Create test rocket
! Translate here all material database
!
+Material.CUSTOM = Custom
+
! Material database
+Databases.materials.types.Bulk = Bulk
+Databases.materials.types.Line = Line
+Databases.materials.types.Surface = Surface
+
! BULK_MATERIAL
Databases.materials.Acrylic = Acrylic
Databases.materials.Aluminum = Aluminum
@@ -1165,8 +1195,8 @@ Shape.Ellipsoid = Ellipsoid
Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter.
Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
Shape.Powerseries = Power series
-Shape.Powerseries.desc1 = A power series nose cone has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 this is a \u00BD-power or parabolic nose cone, for k=0.75 a \u00BE-power, and for k=1 a conical nose cone.
-Shape.Powerseries.desc2 = A power series transition has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 the transition is \u00BD-power or parabolic, for k=0.75 a \u00BE-power, and for k=1 conical.
+Shape.Powerseries.desc1 = A power series nose cone has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 this is a \u00bd-power or parabolic nose cone, for k=0.75 a \u00be-power, and for k=1 a conical nose cone.
+Shape.Powerseries.desc2 = A power series transition has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 the transition is \u00bd-power or parabolic, for k=0.75 a \u00be-power, and for k=1 conical.
Shape.Parabolicseries = Parabolic series
Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a full parabola which is tangent to the body tube, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical nose cone.
Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a full parabola which is tangent to the body tube at the aft end, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical transition.
@@ -1216,6 +1246,14 @@ Parachute.Parachute = Parachute
ShockCord.ShockCord = Shock cord
! Bulkhead
Bulkhead.Bulkhead = Bulkhead
+! CenteringRing
+CenteringRing.CenteringRing = Centering ring
+! EngineBlock
+EngineBlock.EngineBlock = Engine block
+! Streamer
+Streamer.Streamer = Streamer
+! Sleeve
+Sleeve.Sleeve = Sleeve
!Rocket
Rocket.motorCount.Nomotor = [No motors]