WsfScriptP6DOF_Mover.hpp

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// ****************************************************************************
// CUI
//
// The Advanced Framework for Simulation, Integration, and Modeling (AFSIM)
//
// Copyright 2003-2015 The Boeing Company. All rights reserved.
//
// The use, dissemination or disclosure of data in this file is subject to
// limitation or restriction. See accompanying README and LICENSE for details.
// ****************************************************************************
// ****************************************************************************
// Updated by Infoscitex, a DCS Company.
// ****************************************************************************
 
#ifndef WSFSCRIPTP6DOF_MOVER_HPP
#define WSFSCRIPTP6DOF_MOVER_HPP
 
#include "wsf_p6dof_export.h"
 
#include "script/WsfScriptMoverClass.hpp"

class WSF_P6DOF_EXPORT WsfScriptP6DOF_MoverClass : public WsfScriptMoverClass
{
public:
   WsfScriptP6DOF_MoverClass(const std::string& aClassName, UtScriptTypes* aTypesPtr);
 
   // -----------------------------------------------------------------------
 
   // VEHICLE KINEMATIC STATE SUPPORT
 
   // Altitude
   UT_DECLARE_SCRIPT_METHOD(GetAltitude); // Altitude in meters
 
   // Attitude
   UT_DECLARE_SCRIPT_METHOD(GetHeading); // Heading in degrees
   UT_DECLARE_SCRIPT_METHOD(GetPitch);   // Pitch in degrees
   UT_DECLARE_SCRIPT_METHOD(GetRoll);    // Roll in degrees
 
   // Vertical Speed/Angle
   UT_DECLARE_SCRIPT_METHOD(GetVerticalSpeed);   // Vertical speed in meters/sec
   UT_DECLARE_SCRIPT_METHOD(GetFlightPathAngle); // Gamma in degrees
 
   // Angular Rates
   UT_DECLARE_SCRIPT_METHOD(GetYawRate);   // Yaw rate in rad/sec
   UT_DECLARE_SCRIPT_METHOD(GetPitchRate); // Pitch rate in rad/sec
   UT_DECLARE_SCRIPT_METHOD(GetRollRate);  // Roll rate in rad/sec
 
   // Accelerations
   UT_DECLARE_SCRIPT_METHOD(GetGLoad); // G-Load in Gees
   UT_DECLARE_SCRIPT_METHOD(GetNx);    // Nx in Gees
   UT_DECLARE_SCRIPT_METHOD(GetNy);    // Ny in Gees
   UT_DECLARE_SCRIPT_METHOD(GetNz);    // Nz in Gees
 
   // Airspeed and Mach
   UT_DECLARE_SCRIPT_METHOD(GetKCAS); // Speed in knots calibrated air speed
   UT_DECLARE_SCRIPT_METHOD(GetKIAS); // Speed in knots indicated air speed
   UT_DECLARE_SCRIPT_METHOD(GetKTAS); // Speed in knots true air speed
   UT_DECLARE_SCRIPT_METHOD(GetMach); // Speed in Mach
 
   // Dynamic Pressure
   UT_DECLARE_SCRIPT_METHOD(GetDynamicPressure); // Q in lbs/ft^2
 
   // -----------------------------------------------------------------------
 
   // MASS PROPERTIES SUPPORT
 
   // Weights
   UT_DECLARE_SCRIPT_METHOD(GetTotalWeight);   // Weight/mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetCurrentWeight); // Weight/mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetEmptyWeight);   // Weight/mass in kg
 
   // Center of gravity/mass (CG/CM) relative to reference point
   UT_DECLARE_SCRIPT_METHOD(GetCgX); // CG location in meters
   UT_DECLARE_SCRIPT_METHOD(GetCgY); // CG location in meters
   UT_DECLARE_SCRIPT_METHOD(GetCgZ); // CG location in meters
 
   // -----------------------------------------------------------------------
 
   // ENGINE SUPPORT
 
   UT_DECLARE_SCRIPT_METHOD(StartupEngines);
   UT_DECLARE_SCRIPT_METHOD(ShutdownEngines);
   UT_DECLARE_SCRIPT_METHOD(IsProducingThrust);
   UT_DECLARE_SCRIPT_METHOD(GetTotalThrust);
   UT_DECLARE_SCRIPT_METHOD(GetEngineThrust);
   UT_DECLARE_SCRIPT_METHOD(GetAfterburnerOn);
   UT_DECLARE_SCRIPT_METHOD(GetEngineFuelFlowRate);
   UT_DECLARE_SCRIPT_METHOD(GetEngineAfterburnerOn);
   UT_DECLARE_SCRIPT_METHOD(SetFuelFeed);
   UT_DECLARE_SCRIPT_METHOD(SetFuelFeedAllEngines);
 
   // -----------------------------------------------------------------------
 
   // FUEL SYSTEM SUPPORT
 
   // Fuel System
   UT_DECLARE_SCRIPT_METHOD(AddFuel);                  // Fuel mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetTotalFuelCapacity);     // Fuel mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetInternalFuelCapacity);  // Fuel mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetExternalFuelCapacity);  // Fuel mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetTotalFuelRemaining);    // Fuel mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetInternalFuelRemaining); // Fuel mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetExternalFuelRemaining); // Fuel mass in kg
 
   // Fuel Tanks
   UT_DECLARE_SCRIPT_METHOD(GetFuelTankCapacity); // Fuel mass in kg
   UT_DECLARE_SCRIPT_METHOD(GetFuelInTank);       // Fuel mass in kg
   UT_DECLARE_SCRIPT_METHOD(SetFuelInTank);       // Fuel mass in kg
 
   // Fuel Flow
   UT_DECLARE_SCRIPT_METHOD(GetTotalFuelFlowRate); // Fuel flow in kg/sec
 
   // Fuel Transfers
   UT_DECLARE_SCRIPT_METHOD(AddFuelTransfer);
   UT_DECLARE_SCRIPT_METHOD(RemoveFuelTransfer);
 
   // Joker fuel state
   UT_DECLARE_SCRIPT_METHOD(SetJokerFuelState);   // Sets Joker fuel (kg)
   UT_DECLARE_SCRIPT_METHOD(GetJokerFuelState);   // Returns Joker fuel (kg)
   UT_DECLARE_SCRIPT_METHOD(GetJokerFuelReached); // Returns true if Joker
 
   // Bingo fuel state
   UT_DECLARE_SCRIPT_METHOD(SetBingoFuelState);   // Sets Bingo fuel (kg)
   UT_DECLARE_SCRIPT_METHOD(GetBingoFuelState);   // Returns Bingo fuel (kg)
   UT_DECLARE_SCRIPT_METHOD(GetBingoFuelReached); // Returns true if Bingo
 
   // -----------------------------------------------------------------------
 
   // LANDING GEAR AND BRAKING SUPPORT
 
   // Landing Gear
   UT_DECLARE_SCRIPT_METHOD(RetractLandingGear);
   UT_DECLARE_SCRIPT_METHOD(LowerLandingGear);
   UT_DECLARE_SCRIPT_METHOD(GetLandingGearPosition); // Angle in degrees
 
   // Weight on Wheels
   UT_DECLARE_SCRIPT_METHOD(WeightOnWheels);
   UT_DECLARE_SCRIPT_METHOD(WeightOnNoseWheel);
 
   // Nose Wheel Steering (NWS)
   UT_DECLARE_SCRIPT_METHOD(SetEnableNWS);
   UT_DECLARE_SCRIPT_METHOD(GetNoseWheelAngle); // Angle in degrees
 
   // Brake Controls
   UT_DECLARE_SCRIPT_METHOD(EnableDirectBraking);
   UT_DECLARE_SCRIPT_METHOD(SetParkingBrake);
   UT_DECLARE_SCRIPT_METHOD(ApplyLeftGearBrake);
   UT_DECLARE_SCRIPT_METHOD(ApplyRightGearBrake);
   UT_DECLARE_SCRIPT_METHOD(ReleaseWheelBrakes);
   UT_DECLARE_SCRIPT_METHOD(ReleaseDirectBraking);
 
   // -----------------------------------------------------------------------
 
   // EXTERNAL FORCES SUPPORT
 
   // This allows an external force (such as a ground tug or aircraft carrier
   // catapult) to apply a force to the nose gear. The angle is measured as
   // zero being forward and positive angles being to the right.
   UT_DECLARE_SCRIPT_METHOD(ApplyExternalForce); // Force in lbs
 
   // This removes any and all external forces on the nose gear
   UT_DECLARE_SCRIPT_METHOD(RemoveExternalForce);
 
   // -----------------------------------------------------------------------
 
   // SEQUENCER SUPPORT
 
   // Sequencer Activation
   UT_DECLARE_SCRIPT_METHOD(ActivateSequencer);
 
   // -----------------------------------------------------------------------
 
   // MANEUVER SUPPORT
 
   UT_DECLARE_SCRIPT_METHOD(GetCurrentManeuver);
   UT_DECLARE_SCRIPT_METHOD(GetManeuverSequence);
   UT_DECLARE_SCRIPT_METHOD(ExecuteManeuver);
   UT_DECLARE_SCRIPT_METHOD(ExecuteManeuverSequence);
   UT_DECLARE_SCRIPT_METHOD(CancelManeuvers);
 
   // -----------------------------------------------------------------------
 
   // AUTOPILOT SUPPORT
 
   // Autopilot commands
   UT_DECLARE_SCRIPT_METHOD(EnableAutopilot);
 
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotAltitude);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotVerticalSpeed);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotPitchAngle);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotFlightPathAngle);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotPitchRate);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotDeltaPitch);
   UT_DECLARE_SCRIPT_METHOD(SetPitchGLoad);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotRollAngle);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotRollRate);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotDeltaRoll);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotSpeedKTAS);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotSpeedKCAS);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotSpeedKIAS);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotSpeedMach);
   UT_DECLARE_SCRIPT_METHOD(SetTaxiMode);
   UT_DECLARE_SCRIPT_METHOD(SetTaxiRadius);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotLateralWaypointMode);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotVerticalWaypointMode);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotSpeedWaypointMode);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotWaypointMode);
   UT_DECLARE_SCRIPT_METHOD(SetAutopilotNoControl);
 
   // Returns the active pilot/controller
   UT_DECLARE_SCRIPT_METHOD(GetActivePilot);
 
   // Sets the active pilot/controller
   UT_DECLARE_SCRIPT_METHOD(ActivateManualPilot);
   UT_DECLARE_SCRIPT_METHOD(ActivateSyntheticPilot);
   UT_DECLARE_SCRIPT_METHOD(ActivateHardwareAutopilot);
   UT_DECLARE_SCRIPT_METHOD(ActivateGuidanceAutopilot);
 
   // These provide modes/values for the three autopilot channels
   UT_DECLARE_SCRIPT_METHOD(GetAutopilotLateralMode);
   UT_DECLARE_SCRIPT_METHOD(GetAutopilotLateralModeValue);
   UT_DECLARE_SCRIPT_METHOD(GetAutopilotVerticalMode);
   UT_DECLARE_SCRIPT_METHOD(GetAutopilotVerticalModeValue);
   UT_DECLARE_SCRIPT_METHOD(GetAutopilotSpeedMode);
   UT_DECLARE_SCRIPT_METHOD(GetAutopilotSpeedModeValue);
 
   // Current autopilot limits
   UT_DECLARE_SCRIPT_METHOD(GetPitchGLoadMin);
   UT_DECLARE_SCRIPT_METHOD(GetPitchGLoadMax);
   UT_DECLARE_SCRIPT_METHOD(GetAlphaMin);
   UT_DECLARE_SCRIPT_METHOD(GetAlphaMax);
   UT_DECLARE_SCRIPT_METHOD(GetPitchRateMin);
   UT_DECLARE_SCRIPT_METHOD(GetPitchRateMax);
   UT_DECLARE_SCRIPT_METHOD(GetVerticalSpeedMin);
   UT_DECLARE_SCRIPT_METHOD(GetVerticalSpeedMax);
   UT_DECLARE_SCRIPT_METHOD(GetYawGLoadMax);
   UT_DECLARE_SCRIPT_METHOD(GetBetaMax);
   UT_DECLARE_SCRIPT_METHOD(GetYawRateMax);
   UT_DECLARE_SCRIPT_METHOD(GetRollRateMax);
   UT_DECLARE_SCRIPT_METHOD(GetBankAngleMax);
   UT_DECLARE_SCRIPT_METHOD(GetForwardAccelMin);
   UT_DECLARE_SCRIPT_METHOD(GetForwardAccelMax);
   UT_DECLARE_SCRIPT_METHOD(GetTaxiSpeedMax);
   UT_DECLARE_SCRIPT_METHOD(GetTaxiYawRateMax);
 
   // Set autopilot limits
   UT_DECLARE_SCRIPT_METHOD(SetPitchGLoadMin);
   UT_DECLARE_SCRIPT_METHOD(SetPitchGLoadMax);
   UT_DECLARE_SCRIPT_METHOD(SetAlphaMin);
   UT_DECLARE_SCRIPT_METHOD(SetAlphaMax);
   UT_DECLARE_SCRIPT_METHOD(SetPitchRateMin);
   UT_DECLARE_SCRIPT_METHOD(SetPitchRateMax);
   UT_DECLARE_SCRIPT_METHOD(SetVerticalSpeedMin);
   UT_DECLARE_SCRIPT_METHOD(SetVerticalSpeedMax);
   UT_DECLARE_SCRIPT_METHOD(SetYawGLoadMax);
   UT_DECLARE_SCRIPT_METHOD(SetBetaMax);
   UT_DECLARE_SCRIPT_METHOD(SetYawRateMax);
   UT_DECLARE_SCRIPT_METHOD(SetRollRateMax);
   UT_DECLARE_SCRIPT_METHOD(SetBankAngleMax);
   UT_DECLARE_SCRIPT_METHOD(SetForwardAccelMin);
   UT_DECLARE_SCRIPT_METHOD(SetForwardAccelMax);
   UT_DECLARE_SCRIPT_METHOD(SetTaxiSpeedMax);
   UT_DECLARE_SCRIPT_METHOD(SetTaxiYawRateMax);
 
   // Turn roll-in controls
   UT_DECLARE_SCRIPT_METHOD(SetTurnRollInMultiplier);
   UT_DECLARE_SCRIPT_METHOD(GetCurrentTurnRollInMultiplier);
   UT_DECLARE_SCRIPT_METHOD(GetDefaultTurnRollInMultiplier);
 
   // Allowable angle error values
   UT_DECLARE_SCRIPT_METHOD(SetRouteAllowableAngleError);
   UT_DECLARE_SCRIPT_METHOD(GetCurrentRouteAllowableAngleError);
   UT_DECLARE_SCRIPT_METHOD(GetDefaultRouteAllowableAngleError);
 
   // Revert autopilot limits to default values
   UT_DECLARE_SCRIPT_METHOD(RevertLimitsToDefaults);
 
   // -----------------------------------------------------------------------
 
   // APPEARANCE SUPPORT
 
   // Engine Operation Effects
   UT_DECLARE_SCRIPT_METHOD(GetEngineIsOperating);
   UT_DECLARE_SCRIPT_METHOD(GetEngineIsSmoking);
   UT_DECLARE_SCRIPT_METHOD(GetEngineAfterburnerIsOn);
 
   // Trailing Effects
   UT_DECLARE_SCRIPT_METHOD(GetContrailTrailingEffect);
   UT_DECLARE_SCRIPT_METHOD(GetRocketSmokeTrailingEffect);
   UT_DECLARE_SCRIPT_METHOD(GetDamageSmokeTrailingEffect);
 
   // Launch Effects
   UT_DECLARE_SCRIPT_METHOD(GetLaunchFlashSmokeIsPresent);
 
   // Damage Appearance
   UT_DECLARE_SCRIPT_METHOD(GetRisingSmokePlumeIsPresent);
   UT_DECLARE_SCRIPT_METHOD(GetFlamesArePresent);
   UT_DECLARE_SCRIPT_METHOD(GetIsLightlyDamaged);
   UT_DECLARE_SCRIPT_METHOD(GetIsHeavilyDamaged);
 
   // -----------------------------------------------------------------------
 
   // DAMAGE AND DESTRUCTION SUPPORT
 
   // Damaged
   UT_DECLARE_SCRIPT_METHOD(SetLightDamage);
   UT_DECLARE_SCRIPT_METHOD(SetHeavyDamage);
 
   // Destroyed
   UT_DECLARE_SCRIPT_METHOD(SetDestroyed);
 
   // -----------------------------------------------------------------------
 
   // CONTROL INPUTS SUPPORT
 
   // Thrust Vector Control
   UT_DECLARE_SCRIPT_METHOD(EnableThrustVectoring);
 
   // Thrust Reverser Control
   UT_DECLARE_SCRIPT_METHOD(SetThrustReverserPosition);
 
   // Enable/disable Overall Control
   UT_DECLARE_SCRIPT_METHOD(EnableControls);
 
   // Direct Control Functions
   UT_DECLARE_SCRIPT_METHOD(TakeDirectControlInput);
   UT_DECLARE_SCRIPT_METHOD(ReleaseDirectControlInput);
   UT_DECLARE_SCRIPT_METHOD(SetDirectControlInputs);
 
   // Direct throttle controls
   UT_DECLARE_SCRIPT_METHOD(EnableDirectThrottleInput);
   UT_DECLARE_SCRIPT_METHOD(MoveThrottleToIdle);
   UT_DECLARE_SCRIPT_METHOD(MoveThrottleToFull);
   UT_DECLARE_SCRIPT_METHOD(MoveThrottleToMilitary);
   UT_DECLARE_SCRIPT_METHOD(MoveThrottleToAfterburner);
   UT_DECLARE_SCRIPT_METHOD(ReleaseDirectThrottleInput);
 
   // Direct speed brake controls
   UT_DECLARE_SCRIPT_METHOD(EnableDirectSpeedBrakeInput);
   UT_DECLARE_SCRIPT_METHOD(OpenSpeedBrake);
   UT_DECLARE_SCRIPT_METHOD(CloseSpeedBrake);
   UT_DECLARE_SCRIPT_METHOD(ReleaseDirectSpeedBrakeInput);
   UT_DECLARE_SCRIPT_METHOD(GetSpeedBrakePosition); // Returns the position/angle (deg)
 
   // Flaps controls
   UT_DECLARE_SCRIPT_METHOD(SetFlapsPosition);
   UT_DECLARE_SCRIPT_METHOD(GetFlapsPosition); // Returns the position/angle (deg)
 
   // Spoilers controls
   UT_DECLARE_SCRIPT_METHOD(SetSpoilersPosition);
   UT_DECLARE_SCRIPT_METHOD(GetSpoilersPosition); // Returns the position/angle (deg)
 
   // Flight control inputs
   UT_DECLARE_SCRIPT_METHOD(GetStickRightPosition);          // Range of -1 to +1
   UT_DECLARE_SCRIPT_METHOD(GetStickBackPosition);           // Range of -1 to +1
   UT_DECLARE_SCRIPT_METHOD(GetRudderRightPosition);         // Range of -1 to +1
   UT_DECLARE_SCRIPT_METHOD(GetThrottleMilitaryPosition);    // Range of 0 to 1
   UT_DECLARE_SCRIPT_METHOD(GetThrottleAfterburnerPosition); // Range of 0 to 1
   UT_DECLARE_SCRIPT_METHOD(GetThrustReverserPosition);      // Range of 0 to 1
   UT_DECLARE_SCRIPT_METHOD(GetSpeedBrakeControlPosition);   // Range of 0 to 1
   UT_DECLARE_SCRIPT_METHOD(GetFlapsLeverPosition);          // Range of 0 to 1
   UT_DECLARE_SCRIPT_METHOD(GetSpoilersLeverPosition);       // Range of 0 to 1
   UT_DECLARE_SCRIPT_METHOD(GetLandingGearLeverPosition);    // Range of 0 to 1
 
   // -----------------------------------------------------------------------
 
   // CONTROL SURFACE POSITIONS SUPPORT
 
   // This provides the angle (deg) of the specified control surface (string)
   UT_DECLARE_SCRIPT_METHOD(GetAngleOfControlSurface);
 
   // This returns an array of control surface names (strings)
   UT_DECLARE_SCRIPT_METHOD(GetListOfControlSurfaceNames);
 
   // These provide the angle (deg) of common control surfaces
   UT_DECLARE_SCRIPT_METHOD(GetAileronsBothPosition);
   UT_DECLARE_SCRIPT_METHOD(GetStabilatorLeftPosition);
   UT_DECLARE_SCRIPT_METHOD(GetStabilatorRightPosition);
   UT_DECLARE_SCRIPT_METHOD(GetRudderPosition);
 
   // -----------------------------------------------------------------------
 
   // FORCES AND MOMENTS (F&M) SUPPORT
 
   // Forces and Moments (F&M)
   UT_DECLARE_SCRIPT_METHOD(GetLift);            // Lift in Newtons
   UT_DECLARE_SCRIPT_METHOD(GetDrag);            // Drag in Newtons
   UT_DECLARE_SCRIPT_METHOD(GetSideForce);       // Side force in Newtons
   UT_DECLARE_SCRIPT_METHOD(GetThrustMagnitude); // Thrust magnitude in Newtons
   UT_DECLARE_SCRIPT_METHOD(GetYawMoment);       // Yaw moment in Newton*meters
   UT_DECLARE_SCRIPT_METHOD(GetPitchMoment);     // Pitch moment in Newton*meters
   UT_DECLARE_SCRIPT_METHOD(GetRollMoment);      // Roll moment in Newton*meters
 
   // -----------------------------------------------------------------------
 
   // AERODYNAMICS SUPPORT
 
   // Alpha (angle of attack)
   UT_DECLARE_SCRIPT_METHOD(GetAlpha);    // Alpha in degrees
   UT_DECLARE_SCRIPT_METHOD(GetAlphaDot); // Alpha-Dot in degrees/second
 
   // Beta (angle of sideslip)
   UT_DECLARE_SCRIPT_METHOD(GetBeta);    // Beta in degrees
   UT_DECLARE_SCRIPT_METHOD(GetBetaDot); // Beta-Dot in degrees/second
 
   // Provides CLmax at the specified Mach
   UT_DECLARE_SCRIPT_METHOD(GetCLMaxAtMach);
 
   // Provides alpha (degrees) at CLmax for the specified Mach
   UT_DECLARE_SCRIPT_METHOD(GetAlphaAtCLMaxAtMach);
 
   // Provides maximum g-load possible (in the primary lift direction)
   UT_DECLARE_SCRIPT_METHOD(MaxPotentialManeuverGLoad);
 
   // -----------------------------------------------------------------------
 
   // AIRSPEED CALCULATIONS SUPPORT
 
   // Airspeed/Mach calculation support
   UT_DECLARE_SCRIPT_METHOD(CalcKtasFromKcas);
   UT_DECLARE_SCRIPT_METHOD(CalcKtasFromMach);
   UT_DECLARE_SCRIPT_METHOD(CalcKtasFromFps);
   UT_DECLARE_SCRIPT_METHOD(CalcKcasFromKtas);
   UT_DECLARE_SCRIPT_METHOD(CalcKcasFromMach);
   UT_DECLARE_SCRIPT_METHOD(CalcKcasFromFps);
   UT_DECLARE_SCRIPT_METHOD(CalcMachFromKcas);
   UT_DECLARE_SCRIPT_METHOD(CalcMachFromKtas);
   UT_DECLARE_SCRIPT_METHOD(CalcMachFromFps);
   UT_DECLARE_SCRIPT_METHOD(CalcFpsFromKcas);
   UT_DECLARE_SCRIPT_METHOD(CalcFpsFromKtas);
   UT_DECLARE_SCRIPT_METHOD(CalcFpsFromMach);
   UT_DECLARE_SCRIPT_METHOD(CalcDynamicPressure_lbft2);
   UT_DECLARE_SCRIPT_METHOD(CalcFpsFromAltitudeDynamicPressure);
 
   // -----------------------------------------------------------------------
 
   // TESTING SUPPORT
 
   // The following functions are for Testing and should not be documented,
   //  to hide them from normal users
   UT_DECLARE_SCRIPT_METHOD(GetTestSupportObject);
   UT_DECLARE_SCRIPT_METHOD(SetTestingIgnoreAllCrashes);
   UT_DECLARE_SCRIPT_METHOD(GetTestingIgnoreAllCrashes);
   UT_DECLARE_SCRIPT_METHOD(SetTestingClampToSealLevelMinAlt);
   UT_DECLARE_SCRIPT_METHOD(GetTestingClampToSealLevelMinAlt);
};
 
#endif