componentanalysisdlg.lbl.refarea = Reference area:
!componentanalysisdlg.But.close =Close
componentanalysisdlg.TabStability.Col.Component = Component
+componentanalysisdlg.TOTAL = Total
+componentanalysisdlg.noWarnings = <html><i><font color=\"gray\">No warnings.</font></i>
! Custom Material dialog
custmatdlg.title.Custommaterial = Custom material
TCMotorSelPan.title.Thrustcurve = Thrust curve:
TCMotorSelPan.title.Thrust = Thrust
TCMotorSelPan.delayBox.None = None
+TCMotorSelPan.noDescription = No description available.
! PlotDialog
TCurveMotorCol.DIAMETER = Diameter
TCurveMotorCol.LENGTH = Length
+TCurveMotor.ttip.diameter = Diameter:
+TCurveMotor.ttip.length = Length:
+TCurveMotor.ttip.maxThrust = Maximum thrust:
+TCurveMotor.ttip.avgThrust = Average thrust:
+TCurveMotor.ttip.burnTime = Burn time:
+TCurveMotor.ttip.totalImpulse = Total impulse:
+TCurveMotor.ttip.launchMass = Launch mass:
+TCurveMotor.ttip.emptyMass = Empty mass:
+
! RocketInfo
RocketInfo.lengthLine.Length = Length
RocketInfo.lengthLine.maxdiameter = , max. diameter
componentanalysisdlg.TabStability.Col.CG = \u0426\u0422
componentanalysisdlg.TabStability.Col.Mass = \u041c\u0430\u0441\u0441\u0430
componentanalysisdlg.TabStability.Col.CP = \u0426\u0414
+componentanalysisdlg.TOTAL = \u0412\u0441\u0435\u0433\u043e
+componentanalysisdlg.noWarnings = <html><i><font color=\"gray\">\u041f\u0440\u0435\u0434\u0443\u043f\u0440\u0435\u0436\u0434\u0435\u043d\u0438\u0439 \u043d\u0435\u0442.</font></i>
+
! Custom Material dialog
custmatdlg.title.Custommaterial = \u041f\u043e\u043b\u044c\u0437\u043e\u0432\u0430\u0442\u0435\u043b\u044c\u0441\u043a\u0438\u0439 \u043c\u0430\u0442\u0435\u0440\u0438\u0430\u043b
TCMotorSelPan.title.Thrustcurve = \u041f\u0440\u043e\u0444\u0438\u043b\u044c \u0442\u044f\u0433\u0438:
TCMotorSelPan.title.Thrust = \u0422\u044f\u0433\u0430
TCMotorSelPan.delayBox.None = \u041d\u0435\u0442
+TCMotorSelPan.noDescription = \u041e\u043f\u0438\u0441\u0430\u043d\u0438\u0435 \u043e\u0442\u0441\u0443\u0442\u0441\u0442\u0432\u0443\u0435\u0442.
! PlotDialog
TCurveMotorCol.DIAMETER = \u0414\u0438\u0430\u043c\u0435\u0442\u0440
TCurveMotorCol.LENGTH = \u0414\u043b\u0438\u043d\u0430
+TCurveMotor.ttip.diameter = \u0414\u0438\u0430\u043c\u0435\u0442\u0440:
+TCurveMotor.ttip.length = \u0414\u043b\u0438\u043d\u0430:
+TCurveMotor.ttip.maxThrust = \u041c\u0430\u043a\u0441\u0438\u043c\u0430\u043b\u044c\u043d\u0430\u044f \u0442\u044f\u0433\u0430:
+TCurveMotor.ttip.avgThrust = \u0421\u0440\u0435\u0434\u043d\u044f\u044f \u0442\u044f\u0433\u0430:
+TCurveMotor.ttip.burnTime = \u0412\u0440\u0435\u043c\u044f \u0433\u043e\u0440\u0435\u043d\u0438\u044f:
+TCurveMotor.ttip.totalImpulse = \u041e\u0431\u0449\u0438\u0439 \u0438\u043c\u043f\u0443\u043b\u044c\u0441:
+TCurveMotor.ttip.launchMass = \u0421\u0442\u0430\u0440\u0442\u043e\u0432\u0430\u044f \u043c\u0430\u0441\u0441\u0430:
+TCurveMotor.ttip.emptyMass = \u041c\u0430\u0441\u0441\u0430 \u0431\u0435\u0437 \u0442\u043e\u043f\u043b\u0438\u0432\u0430:
+
! RocketInfo
RocketInfo.lengthLine.Length = \u0414\u043b\u0438\u043d\u0430
RocketInfo.lengthLine.maxdiameter = , \u043c\u0430\u043a\u0441. \u0434\u0438\u0430\u043c\u0435\u0442\u0440
roll = new DoubleModel(rocketPanel, "CPRoll", UnitGroup.UNITS_ROLL);
//// Wind direction:
- panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.winddir")), "width 100lp!");
+ panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.winddir")), "width 120lp!");
panel.add(new UnitSelector(theta, true), "width 50lp!");
BasicSlider slider = new BasicSlider(theta.getSliderModel(0, 2 * Math.PI));
panel.add(slider, "growx, split 2");
panel.add(scrollPane, "gap paragraph, spany 4, width 300lp!, growy 1, height :100lp:, wrap");
////Angle of attack:
- panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.angleofattack")), "width 100lp!");
+ panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.angleofattack")), "width 120lp!");
panel.add(new UnitSelector(aoa, true), "width 50lp!");
panel.add(new BasicSlider(aoa.getSliderModel(0, Math.PI)), "growx, wrap");
//// Mach number:
- panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.machnumber")), "width 100lp!");
+ panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.machnumber")), "width 120lp!");
panel.add(new UnitSelector(mach, true), "width 50lp!");
panel.add(new BasicSlider(mach.getSliderModel(0, 3)), "growx, wrap");
//// Roll rate:
- panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.rollrate")), "width 100lp!");
+ panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.rollrate")), "width 120lp!");
panel.add(new UnitSelector(roll, true), "width 50lp!");
panel.add(new BasicSlider(roll.getSliderModel(-20 * 2 * Math.PI, 20 * 2 * Math.PI)),
"growx, wrap paragraph");
public Object getValueAt(int row) {
RocketComponent c = cpData.get(row).getComponent();
if (c instanceof Rocket) {
- return "Total";
+ return trans.get("componentanalysisdlg.TOTAL");
}
return c.toString();
}
public Object getValueAt(int row) {
RocketComponent c = dragData.get(row).getComponent();
if (c instanceof Rocket) {
- return "Total";
+ return trans.get("componentanalysisdlg.TOTAL");
}
return c.toString();
}
public Object getValueAt(int row) {
RocketComponent c = rollData.get(row).getComponent();
if (c instanceof Rocket) {
- return "Total";
+ return trans.get("componentanalysisdlg.TOTAL");
}
return c.toString();
}
// Set warnings
if (set.isEmpty()) {
warningList.setListData(new String[] {
- "<html><i><font color=\"gray\">No warnings.</font></i>"
+ trans.get("componentanalysisdlg.noWarnings")
});
} else {
warningList.setListData(new Vector<Warning>(set));
tip += "<i>" + desc.replace("\n", "<br>") + "</i><br><hr>";
}
- tip += ("Diameter: " +
+ tip += (trans.get("TCurveMotor.ttip.diameter") + " " +
UnitGroup.UNITS_MOTOR_DIMENSIONS.getDefaultUnit().toStringUnit(m.getDiameter()) +
"<br>");
- tip += ("Length: " +
+ tip += (trans.get("TCurveMotor.ttip.length") + " " +
UnitGroup.UNITS_MOTOR_DIMENSIONS.getDefaultUnit().toStringUnit(m.getLength()) +
"<br>");
- tip += ("Maximum thrust: " +
+ tip += (trans.get("TCurveMotor.ttip.maxThrust") + " " +
UnitGroup.UNITS_FORCE.getDefaultUnit().toStringUnit(m.getMaxThrustEstimate()) +
"<br>");
- tip += ("Average thrust: " +
+ tip += (trans.get("TCurveMotor.ttip.avgThrust") + " " +
UnitGroup.UNITS_FORCE.getDefaultUnit().toStringUnit(m.getAverageThrustEstimate()) +
"<br>");
- tip += ("Burn time: " +
+ tip += (trans.get("TCurveMotor.ttip.burnTime") + " " +
UnitGroup.UNITS_SHORT_TIME.getDefaultUnit()
.toStringUnit(m.getBurnTimeEstimate()) + "<br>");
- tip += ("Total impulse: " +
+ tip += (trans.get("TCurveMotor.ttip.totalImpulse") + " " +
UnitGroup.UNITS_IMPULSE.getDefaultUnit()
.toStringUnit(m.getTotalImpulseEstimate()) + "<br>");
- tip += ("Launch mass: " +
+ tip += (trans.get("TCurveMotor.ttip.launchMass") + " " +
UnitGroup.UNITS_MASS.getDefaultUnit().toStringUnit(m.getLaunchCG().weight) +
"<br>");
- tip += ("Empty mass: " +
+ tip += (trans.get("TCurveMotor.ttip.emptyMass") + " " +
UnitGroup.UNITS_MASS.getDefaultUnit()
.toStringUnit(m.getEmptyCG().weight));
return tip;
s = s.trim();
if (s.length() == 0) {
//// No description available.
- comment.setText("No description available.");
+ comment.setText(trans.get("TCMotorSelPan.noDescription"));
comment.setFont(noCommentFont);
comment.setForeground(NO_COMMENT_COLOR);
} else {