configs.add(config);
//// Stability vs. time
- config = new PlotConfiguration("Stability vs. time");
+ config = new PlotConfiguration(trans.get("PlotConfiguration.Stability"));
config.addPlotDataType(FlightDataType.TYPE_STABILITY, 0);
config.addPlotDataType(FlightDataType.TYPE_CP_LOCATION, 1);
config.addPlotDataType(FlightDataType.TYPE_CG_LOCATION, 1);
configs.add(config);
//// Drag coefficients vs. Mach number
- config = new PlotConfiguration("Drag coefficients vs. Mach number",
+ config = new PlotConfiguration(trans.get("PlotConfiguration.Dragcoef"),
FlightDataType.TYPE_MACH_NUMBER);
config.addPlotDataType(FlightDataType.TYPE_DRAG_COEFF, 0);
config.addPlotDataType(FlightDataType.TYPE_FRICTION_DRAG_COEFF, 0);
configs.add(config);
//// Roll characteristics
- config = new PlotConfiguration("Roll characteristics");
+ config = new PlotConfiguration(trans.get("PlotConfiguration.Rollcharacteristics"));
config.addPlotDataType(FlightDataType.TYPE_ROLL_RATE, 0);
config.addPlotDataType(FlightDataType.TYPE_ROLL_MOMENT_COEFF, 1);
config.addPlotDataType(FlightDataType.TYPE_ROLL_FORCING_COEFF, 1);
configs.add(config);
//// Angle of attack and orientation vs. time
- config = new PlotConfiguration("Angle of attack and orientation vs. time");
+ config = new PlotConfiguration(trans.get("PlotConfiguration.Angleofattack"));
config.addPlotDataType(FlightDataType.TYPE_AOA, 0);
config.addPlotDataType(FlightDataType.TYPE_ORIENTATION_PHI);
config.addPlotDataType(FlightDataType.TYPE_ORIENTATION_THETA);
configs.add(config);
//// Simulation time step and computation time
- config = new PlotConfiguration("Simulation time step and computation time");
+ config = new PlotConfiguration(trans.get("PlotConfiguration.Simulationtime"));
config.addPlotDataType(FlightDataType.TYPE_TIME_STEP);
config.addPlotDataType(FlightDataType.TYPE_COMPUTATION_TIME);
config.setEvent(FlightEvent.Type.IGNITION, true);