X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=src%2Fnet%2Fsf%2Fopenrocket%2Fsimulation%2FFlightDataType.java;h=eea84dde568097948457201cb71bf6dfdd4d83da;hb=493c32a7f337bef1f19e1629c99a70a55af8a61a;hp=a089d4c1ddae1cb4bf483ad8f95ed6718da158fc;hpb=23b96c50e7906f26dd5f6108ac5de673b950563a;p=debian%2Fopenrocket diff --git a/src/net/sf/openrocket/simulation/FlightDataType.java b/src/net/sf/openrocket/simulation/FlightDataType.java index a089d4c1..eea84dde 100644 --- a/src/net/sf/openrocket/simulation/FlightDataType.java +++ b/src/net/sf/openrocket/simulation/FlightDataType.java @@ -3,6 +3,8 @@ package net.sf.openrocket.simulation; import java.util.HashMap; import java.util.Map; +import net.sf.openrocket.l10n.Translator; +import net.sf.openrocket.startup.Application; import net.sf.openrocket.unit.UnitGroup; /** @@ -19,7 +21,8 @@ import net.sf.openrocket.unit.UnitGroup; * @author Sampo Niskanen */ public class FlightDataType implements Comparable { - + private static final Translator trans = Application.getTranslator(); + /** Priority of custom-created variables */ private static final int DEFAULT_PRIORITY = 999; @@ -29,98 +32,145 @@ public class FlightDataType implements Comparable { //// Time - public static final FlightDataType TYPE_TIME = newType("Time", UnitGroup.UNITS_FLIGHT_TIME, 1); + public static final FlightDataType TYPE_TIME = newType(trans.get("FlightDataType.TYPE_TIME"), UnitGroup.UNITS_FLIGHT_TIME, 1); //// Vertical position and motion - public static final FlightDataType TYPE_ALTITUDE = newType("Altitude", UnitGroup.UNITS_DISTANCE, 10); - public static final FlightDataType TYPE_VELOCITY_Z = newType("Vertical velocity", UnitGroup.UNITS_VELOCITY, 11); - public static final FlightDataType TYPE_ACCELERATION_Z = newType("Vertical acceleration", UnitGroup.UNITS_ACCELERATION, 12); + //// Altitude + public static final FlightDataType TYPE_ALTITUDE = newType(trans.get("FlightDataType.TYPE_ALTITUDE"), UnitGroup.UNITS_DISTANCE, 10); + //// Vertical velocity + public static final FlightDataType TYPE_VELOCITY_Z = newType(trans.get("FlightDataType.TYPE_VELOCITY_Z"), UnitGroup.UNITS_VELOCITY, 11); + //// Vertical acceleration + public static final FlightDataType TYPE_ACCELERATION_Z = newType(trans.get("FlightDataType.TYPE_ACCELERATION_Z"), UnitGroup.UNITS_ACCELERATION, 12); //// Total motion - public static final FlightDataType TYPE_VELOCITY_TOTAL = newType("Total velocity", UnitGroup.UNITS_VELOCITY, 20); - public static final FlightDataType TYPE_ACCELERATION_TOTAL = newType("Total acceleration", UnitGroup.UNITS_ACCELERATION, 21); + //// Total velocity + public static final FlightDataType TYPE_VELOCITY_TOTAL = newType(trans.get("FlightDataType.TYPE_VELOCITY_TOTAL"), UnitGroup.UNITS_VELOCITY, 20); + //// Total acceleration + public static final FlightDataType TYPE_ACCELERATION_TOTAL = newType(trans.get("FlightDataType.TYPE_ACCELERATION_TOTAL"), UnitGroup.UNITS_ACCELERATION, 21); //// Lateral position and motion - - public static final FlightDataType TYPE_POSITION_X = newType("Position upwind", UnitGroup.UNITS_DISTANCE, 30); - public static final FlightDataType TYPE_POSITION_Y = newType("Position parallel to wind", UnitGroup.UNITS_DISTANCE, 31); - public static final FlightDataType TYPE_POSITION_XY = newType("Lateral distance", UnitGroup.UNITS_DISTANCE, 32); - public static final FlightDataType TYPE_POSITION_DIRECTION = newType("Lateral direction", UnitGroup.UNITS_ANGLE, 33); - - public static final FlightDataType TYPE_VELOCITY_XY = newType("Lateral velocity", UnitGroup.UNITS_VELOCITY, 34); - public static final FlightDataType TYPE_ACCELERATION_XY = newType("Lateral acceleration", UnitGroup.UNITS_ACCELERATION, 35); + //// Position upwind + public static final FlightDataType TYPE_POSITION_X = newType(trans.get("FlightDataType.TYPE_POSITION_X"), UnitGroup.UNITS_DISTANCE, 30); + //// Position parallel to wind + public static final FlightDataType TYPE_POSITION_Y = newType(trans.get("FlightDataType.TYPE_POSITION_Y"), UnitGroup.UNITS_DISTANCE, 31); + //// Lateral distance + public static final FlightDataType TYPE_POSITION_XY = newType(trans.get("FlightDataType.TYPE_POSITION_XY"), UnitGroup.UNITS_DISTANCE, 32); + //// Lateral direction + public static final FlightDataType TYPE_POSITION_DIRECTION = newType(trans.get("FlightDataType.TYPE_POSITION_DIRECTION"), UnitGroup.UNITS_ANGLE, 33); + //// Lateral velocity + public static final FlightDataType TYPE_VELOCITY_XY = newType(trans.get("FlightDataType.TYPE_VELOCITY_XY"), UnitGroup.UNITS_VELOCITY, 34); + //// Lateral acceleration + public static final FlightDataType TYPE_ACCELERATION_XY = newType(trans.get("FlightDataType.TYPE_ACCELERATION_XY"), UnitGroup.UNITS_ACCELERATION, 35); //// Angular motion - public static final FlightDataType TYPE_AOA = newType("Angle of attack", UnitGroup.UNITS_ANGLE, 40); - public static final FlightDataType TYPE_ROLL_RATE = newType("Roll rate", UnitGroup.UNITS_ROLL, 41); - public static final FlightDataType TYPE_PITCH_RATE = newType("Pitch rate", UnitGroup.UNITS_ROLL, 42); - public static final FlightDataType TYPE_YAW_RATE = newType("Yaw rate", UnitGroup.UNITS_ROLL, 43); + //// Angle of attack + public static final FlightDataType TYPE_AOA = newType(trans.get("FlightDataType.TYPE_AOA"), UnitGroup.UNITS_ANGLE, 40); + //// Roll rate + public static final FlightDataType TYPE_ROLL_RATE = newType(trans.get("FlightDataType.TYPE_ROLL_RATE"), UnitGroup.UNITS_ROLL, 41); + //// Pitch rate + public static final FlightDataType TYPE_PITCH_RATE = newType(trans.get("FlightDataType.TYPE_PITCH_RATE"), UnitGroup.UNITS_ROLL, 42); + //// Yaw rate + public static final FlightDataType TYPE_YAW_RATE = newType(trans.get("FlightDataType.TYPE_YAW_RATE"), UnitGroup.UNITS_ROLL, 43); //// Stability information - public static final FlightDataType TYPE_MASS = newType("Mass", UnitGroup.UNITS_MASS, 50); - public static final FlightDataType TYPE_LONGITUDINAL_INERTIA = newType("Longitudinal moment of inertia", UnitGroup.UNITS_INERTIA, 51); - public static final FlightDataType TYPE_ROTATIONAL_INERTIA = newType("Rotational moment of inertia", UnitGroup.UNITS_INERTIA, 52); - public static final FlightDataType TYPE_CP_LOCATION = newType("CP location", UnitGroup.UNITS_LENGTH, 53); - public static final FlightDataType TYPE_CG_LOCATION = newType("CG location", UnitGroup.UNITS_LENGTH, 54); - public static final FlightDataType TYPE_STABILITY = newType("Stability margin calibers", UnitGroup.UNITS_COEFFICIENT, 55); + //// Mass + public static final FlightDataType TYPE_MASS = newType(trans.get("FlightDataType.TYPE_MASS"), UnitGroup.UNITS_MASS, 50); + //// Longitudinal moment of inertia + public static final FlightDataType TYPE_LONGITUDINAL_INERTIA = newType(trans.get("FlightDataType.TYPE_LONGITUDINAL_INERTIA"), UnitGroup.UNITS_INERTIA, 51); + //// Rotational moment of inertia + public static final FlightDataType TYPE_ROTATIONAL_INERTIA = newType(trans.get("FlightDataType.TYPE_ROTATIONAL_INERTIA"), UnitGroup.UNITS_INERTIA, 52); + //// CP location + public static final FlightDataType TYPE_CP_LOCATION = newType(trans.get("FlightDataType.TYPE_CP_LOCATION"), UnitGroup.UNITS_LENGTH, 53); + //// CG location + public static final FlightDataType TYPE_CG_LOCATION = newType(trans.get("FlightDataType.TYPE_CG_LOCATION"), UnitGroup.UNITS_LENGTH, 54); + //// Stability margin calibers + public static final FlightDataType TYPE_STABILITY = newType(trans.get("FlightDataType.TYPE_STABILITY"), UnitGroup.UNITS_COEFFICIENT, 55); //// Characteristic numbers - public static final FlightDataType TYPE_MACH_NUMBER = newType("Mach number", UnitGroup.UNITS_COEFFICIENT, 60); - public static final FlightDataType TYPE_REYNOLDS_NUMBER = newType("Reynolds number", UnitGroup.UNITS_COEFFICIENT, 61); + //// Mach number + public static final FlightDataType TYPE_MACH_NUMBER = newType(trans.get("FlightDataType.TYPE_MACH_NUMBER"), UnitGroup.UNITS_COEFFICIENT, 60); + //// Reynolds number + public static final FlightDataType TYPE_REYNOLDS_NUMBER = newType(trans.get("FlightDataType.TYPE_REYNOLDS_NUMBER"), UnitGroup.UNITS_COEFFICIENT, 61); //// Thrust and drag - public static final FlightDataType TYPE_THRUST_FORCE = newType("Thrust", UnitGroup.UNITS_FORCE, 70); - public static final FlightDataType TYPE_DRAG_FORCE = newType("Drag force", UnitGroup.UNITS_FORCE, 71); - public static final FlightDataType TYPE_DRAG_COEFF = newType("Drag coefficient", UnitGroup.UNITS_COEFFICIENT, 72); - public static final FlightDataType TYPE_AXIAL_DRAG_COEFF = newType("Axial drag coefficient", UnitGroup.UNITS_COEFFICIENT, 73); + //// Thrust + public static final FlightDataType TYPE_THRUST_FORCE = newType(trans.get("FlightDataType.TYPE_THRUST_FORCE"), UnitGroup.UNITS_FORCE, 70); + //// Drag force + public static final FlightDataType TYPE_DRAG_FORCE = newType(trans.get("FlightDataType.TYPE_DRAG_FORCE"), UnitGroup.UNITS_FORCE, 71); + //// Drag coefficient + public static final FlightDataType TYPE_DRAG_COEFF = newType(trans.get("FlightDataType.TYPE_DRAG_COEFF"), UnitGroup.UNITS_COEFFICIENT, 72); + //// Axial drag coefficient + public static final FlightDataType TYPE_AXIAL_DRAG_COEFF = newType(trans.get("FlightDataType.TYPE_AXIAL_DRAG_COEFF"), UnitGroup.UNITS_COEFFICIENT, 73); //// Component drag coefficients - public static final FlightDataType TYPE_FRICTION_DRAG_COEFF = newType("Friction drag coefficient", UnitGroup.UNITS_COEFFICIENT, 80); - public static final FlightDataType TYPE_PRESSURE_DRAG_COEFF = newType("Pressure drag coefficient", UnitGroup.UNITS_COEFFICIENT, 81); - public static final FlightDataType TYPE_BASE_DRAG_COEFF = newType("Base drag coefficient", UnitGroup.UNITS_COEFFICIENT, 82); + //// Friction drag coefficient + public static final FlightDataType TYPE_FRICTION_DRAG_COEFF = newType(trans.get("FlightDataType.TYPE_FRICTION_DRAG_COEFF"), UnitGroup.UNITS_COEFFICIENT, 80); + //// Pressure drag coefficient + public static final FlightDataType TYPE_PRESSURE_DRAG_COEFF = newType(trans.get("FlightDataType.TYPE_PRESSURE_DRAG_COEFF"), UnitGroup.UNITS_COEFFICIENT, 81); + //// Base drag coefficient + public static final FlightDataType TYPE_BASE_DRAG_COEFF = newType(trans.get("FlightDataType.TYPE_BASE_DRAG_COEFF"), UnitGroup.UNITS_COEFFICIENT, 82); //// Other coefficients - public static final FlightDataType TYPE_NORMAL_FORCE_COEFF = newType("Normal force coefficient", UnitGroup.UNITS_COEFFICIENT, 90); - public static final FlightDataType TYPE_PITCH_MOMENT_COEFF = newType("Pitch moment coefficient", UnitGroup.UNITS_COEFFICIENT, 91); - public static final FlightDataType TYPE_YAW_MOMENT_COEFF = newType("Yaw moment coefficient", UnitGroup.UNITS_COEFFICIENT, 92); - public static final FlightDataType TYPE_SIDE_FORCE_COEFF = newType("Side force coefficient", UnitGroup.UNITS_COEFFICIENT, 93); - public static final FlightDataType TYPE_ROLL_MOMENT_COEFF = newType("Roll moment coefficient", UnitGroup.UNITS_COEFFICIENT, 94); - public static final FlightDataType TYPE_ROLL_FORCING_COEFF = newType("Roll forcing coefficient", UnitGroup.UNITS_COEFFICIENT, 95); - public static final FlightDataType TYPE_ROLL_DAMPING_COEFF = newType("Roll damping coefficient", UnitGroup.UNITS_COEFFICIENT, 96); - - public static final FlightDataType TYPE_PITCH_DAMPING_MOMENT_COEFF = newType("Pitch damping coefficient", UnitGroup.UNITS_COEFFICIENT, 97); - public static final FlightDataType TYPE_YAW_DAMPING_MOMENT_COEFF = newType("Yaw damping coefficient", UnitGroup.UNITS_COEFFICIENT, 98); + //// Normal force coefficient + public static final FlightDataType TYPE_NORMAL_FORCE_COEFF = newType(trans.get("FlightDataType.TYPE_NORMAL_FORCE_COEFF"), UnitGroup.UNITS_COEFFICIENT, 90); + //// Pitch moment coefficient + public static final FlightDataType TYPE_PITCH_MOMENT_COEFF = newType(trans.get("FlightDataType.TYPE_PITCH_MOMENT_COEFF"), UnitGroup.UNITS_COEFFICIENT, 91); + //// Yaw moment coefficient + public static final FlightDataType TYPE_YAW_MOMENT_COEFF = newType(trans.get("FlightDataType.TYPE_YAW_MOMENT_COEFF"), UnitGroup.UNITS_COEFFICIENT, 92); + //// Side force coefficient + public static final FlightDataType TYPE_SIDE_FORCE_COEFF = newType(trans.get("FlightDataType.TYPE_SIDE_FORCE_COEFF"), UnitGroup.UNITS_COEFFICIENT, 93); + //// Roll moment coefficient + public static final FlightDataType TYPE_ROLL_MOMENT_COEFF = newType(trans.get("FlightDataType.TYPE_ROLL_MOMENT_COEFF"), UnitGroup.UNITS_COEFFICIENT, 94); + //// Roll forcing coefficient + public static final FlightDataType TYPE_ROLL_FORCING_COEFF = newType(trans.get("FlightDataType.TYPE_ROLL_FORCING_COEFF"), UnitGroup.UNITS_COEFFICIENT, 95); + //// Roll damping coefficient + public static final FlightDataType TYPE_ROLL_DAMPING_COEFF = newType(trans.get("FlightDataType.TYPE_ROLL_DAMPING_COEFF"), UnitGroup.UNITS_COEFFICIENT, 96); + + //// Pitch damping coefficient + public static final FlightDataType TYPE_PITCH_DAMPING_MOMENT_COEFF = newType(trans.get("FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF"), UnitGroup.UNITS_COEFFICIENT, 97); + //// Yaw damping coefficient + public static final FlightDataType TYPE_YAW_DAMPING_MOMENT_COEFF = newType(trans.get("FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF"), UnitGroup.UNITS_COEFFICIENT, 98); //// Reference length + area - public static final FlightDataType TYPE_REFERENCE_LENGTH = newType("Reference length", UnitGroup.UNITS_LENGTH, 100); - public static final FlightDataType TYPE_REFERENCE_AREA = newType("Reference area", UnitGroup.UNITS_AREA, 101); + //// Reference length + public static final FlightDataType TYPE_REFERENCE_LENGTH = newType(trans.get("FlightDataType.TYPE_REFERENCE_LENGTH"), UnitGroup.UNITS_LENGTH, 100); + //// Reference area + public static final FlightDataType TYPE_REFERENCE_AREA = newType(trans.get("FlightDataType.TYPE_REFERENCE_AREA"), UnitGroup.UNITS_AREA, 101); //// Orientation - public static final FlightDataType TYPE_ORIENTATION_THETA = newType("Vertical orientation (zenith)", UnitGroup.UNITS_ANGLE, 106); - public static final FlightDataType TYPE_ORIENTATION_PHI = newType("Lateral orientation (azimuth)", UnitGroup.UNITS_ANGLE, 107); + //// Vertical orientation (zenith) + public static final FlightDataType TYPE_ORIENTATION_THETA = newType(trans.get("FlightDataType.TYPE_ORIENTATION_THETA"), UnitGroup.UNITS_ANGLE, 106); + //// Lateral orientation (azimuth) + public static final FlightDataType TYPE_ORIENTATION_PHI = newType(trans.get("FlightDataType.TYPE_ORIENTATION_PHI"), UnitGroup.UNITS_ANGLE, 107); //// Atmospheric conditions - public static final FlightDataType TYPE_WIND_VELOCITY = newType("Wind velocity", UnitGroup.UNITS_VELOCITY, 110); - public static final FlightDataType TYPE_AIR_TEMPERATURE = newType("Air temperature", UnitGroup.UNITS_TEMPERATURE, 111); - public static final FlightDataType TYPE_AIR_PRESSURE = newType("Air pressure", UnitGroup.UNITS_PRESSURE, 112); - public static final FlightDataType TYPE_SPEED_OF_SOUND = newType("Speed of sound", UnitGroup.UNITS_VELOCITY, 113); + //// Wind velocity + public static final FlightDataType TYPE_WIND_VELOCITY = newType(trans.get("FlightDataType.TYPE_WIND_VELOCITY"), UnitGroup.UNITS_VELOCITY, 110); + //// Air temperature + public static final FlightDataType TYPE_AIR_TEMPERATURE = newType(trans.get("FlightDataType.TYPE_AIR_TEMPERATURE"), UnitGroup.UNITS_TEMPERATURE, 111); + //// Air pressure + public static final FlightDataType TYPE_AIR_PRESSURE = newType(trans.get("FlightDataType.TYPE_AIR_PRESSURE"), UnitGroup.UNITS_PRESSURE, 112); + //// Speed of sound + public static final FlightDataType TYPE_SPEED_OF_SOUND = newType(trans.get("FlightDataType.TYPE_SPEED_OF_SOUND"), UnitGroup.UNITS_VELOCITY, 113); //// Simulation information - public static final FlightDataType TYPE_TIME_STEP = newType("Simulation time step", UnitGroup.UNITS_TIME_STEP, 200); - public static final FlightDataType TYPE_COMPUTATION_TIME = newType("Computation time", UnitGroup.UNITS_SHORT_TIME, 201); + //// Simulation time step + public static final FlightDataType TYPE_TIME_STEP = newType(trans.get("FlightDataType.TYPE_TIME_STEP"), UnitGroup.UNITS_TIME_STEP, 200); + //// Computation time + public static final FlightDataType TYPE_COMPUTATION_TIME = newType(trans.get("FlightDataType.TYPE_COMPUTATION_TIME"), UnitGroup.UNITS_SHORT_TIME, 201);