#include <WsfP6DOF_MoverTestObject.hpp>

Collaboration diagram for WsfP6DOF_MoverTestObject:

[legend]

Public Member Functions
	WsfP6DOF_MoverTestObject (WsfP6DOF_Mover *aParentMover)
	Constructor.
void	Update (double aSimTime)
double	GetRangeSinceStart_km () const
void	SetMasterNoLagTesting (bool aEnable)
void	SetMasterFreezeLocation (bool aEnable)
void	SetMasterFreezeAltitude (bool aEnable)
void	SetMasterFreezeVerticalSpeed (bool aEnable)
void	SetMasterFreezePitch (bool aEnable)
void	SetMasterFreezeRoll (bool aEnable)
void	SetMasterFreezeYaw (bool aEnable)
void	SetMasterFreezeFuelBurn (bool aEnable)
void	SetMasterNoAlphaTesting (bool aEnable)
void	Autotune ()
void	CreateAutopilotConfigFile (const std::string &aFilename)
P6DofUtils::CanFlyAtReturnValue	CanFlyAt (double aAltitude_ft, double aVelocity_fps, double aThrottle, double aFlaps=0.0)
double	TurnRateAt (double aSpecificExcessPower_fps, double aTrueSpeed_fps, double aThrottleSetting)
double	TurnRateWithConditions (double aSpecificExcessPower_fps, double aCurrentMass_lbs, double aMaxGLoad, double aAltitude_ft, double aAirspeed_fps, double aThrottleSetting)
double	GetLevelFlightHorizontalThrust (double aAltitude_ft, double aMach, double aThrottle, double aGrossWeight_lbs)
double	GetLevelFlightDrag (double aAltitude_ft, double aMach, double aGrossWeight_lbs)
double	GetPitchingMoment (double aAltitude_ft, double aMach, double aAlpha_deg, double aStickBack)
double	GetLevelFlightFuelBurnRate (double aAltitude_ft, double aMach, double aGrossWeight_lbs)
void	FlyStraightLevelFullThrottle ()
void	CreateAutopilotSupportFile (const std::string &aFilename)
void	CreateAutopilotSupportFileWithMaxMach (const std::string &aFilename, const double &aMaxMach)
void	LimitAlphaByMaxGLoad (P6DofVehicle *aVehicle, double aMach, double aMaxGLoad, double aDynPressure_ppsqft, double &aAlpha_rad)
void	LimitAlphaByMaxGLoad (P6DofVehicle *aVehicle, double aMach, double aMaxGLoad, double aDynPressure_ppsqft, double aCurrentMass_lbs, double &aAlpha_rad)
void	SetVehicleMass (double aMass_lbs)
double	GetMaxGLoad ()
double	MaxInstantaneousGLoad (double aAltitude_ft, double aMach, double aCurrentMass_lbs)

Protected Member Functions
double	AlphaAtDesiredDrag (double aAlt_ft, double aSpeed_fps, double aDrag_lbs, bool &aOk)
bool	AlphaAtDesiredDrag (double aAlt_ft, double aMach, double aDrag_lbs, double aCurrentMass_lbs, double aMaxGLoad, double &aAlpha_rad)
void	SetupForTestingMode (bool aFreezeFuelBurn)
void	RestoreFromTestingMode ()
bool	CalcLevelFlightDragAndAlpha (double aAltitude_ft, double aMach, double aGrossWeight_lbs, double &aDrag_lbs, double &aAlpha_deg)
double	ThrottleSettingToProduceThrust (P6DofThrustProducerObject aEngine, P6DofAtmosphere aAtm, double aAltitude_ft, double aMach, double aRequiredThrust_lbs)
double	FuelBurnAtRequiredThrust (P6DofThrustProducerObject aEngine, P6DofAtmosphere aAtm, double aAltitude_ft, double aMach, double aRequiredThrust_lbs)
double	FuelBurnAtThrottleSetting (P6DofThrustProducerObject aEngine, P6DofAtmosphere aAtm, double aAltitude_ft, double aMach, double aThrottle)
double	ThrustAtThrottleSetting (P6DofThrustProducerObject aEngine, P6DofAtmosphere aAtm, double aAltitude_ft, double aMach, double aThrottle)
P6DofAtmosphere *	GetAtmosphere ()

Protected Attributes
WsfP6DOF_Mover *	mParentMover = nullptr
bool	mTestingNolag = false
bool	mTestingFreezeFuelBurn = false

Constructor & Destructor Documentation

◆ WsfP6DOF_MoverTestObject()

WsfP6DOF_MoverTestObject::WsfP6DOF_MoverTestObject ( WsfP6DOF_Mover * aParentMover )

explicit

Constructor.

References mParentMover.

Member Function Documentation

◆ AlphaAtDesiredDrag() [1/2]

bool WsfP6DOF_MoverTestObject::AlphaAtDesiredDrag	(	double	aAlt_ft,
		double	aMach,
		double	aDrag_lbs,
		double	aCurrentMass_lbs,
		double	aMaxGLoad,
		double &	aAlpha_rad )

protected

References P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcFpsFromMach(), P6DofVehicle::CalculateCmAreaForCoreAndControls(), P6DofAeroCoreObject::Cd_AlphaBetaMach(), P6DofAeroCoreObject::Cd_AlphaMach(), P6DofVehicle::GetActiveAeroObject(), P6DofCommonController::GetAlphaMaxMach(), GetAtmosphere(), P6DofVehicle::GetPilotManager(), P6DofPilotManager::GetSpecialCommonController(), P6DofVehicle::GetWingArea_sqft(), LimitAlphaByMaxGLoad(), mParentMover, and P6DofAeroCoreObject::UseLegacyAero().

◆ AlphaAtDesiredDrag() [2/2]

double WsfP6DOF_MoverTestObject::AlphaAtDesiredDrag	(	double	aAlt_ft,
		double	aSpeed_fps,
		double	aDrag_lbs,
		bool &	aOk )

protected

References P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcMachFromFps(), P6DofVehicle::CalculateCmAreaForCoreAndControls(), P6DofAeroCoreObject::Cd_AlphaBetaMach(), P6DofAeroCoreObject::Cd_AlphaMach(), P6DofVehicle::GetActiveAeroObject(), P6DofCommonController::GetAlphaMaxMach(), GetAtmosphere(), P6DofCommonController::GetCurrentLimitsAndSettings(), P6DofVehicle::GetPilotManager(), P6DofPilotManager::GetSpecialCommonController(), P6DofVehicle::GetWingArea_sqft(), LimitAlphaByMaxGLoad(), mParentMover, P6DOF::AutopilotLimitsAndSettings::pitchGLoad_Max, and P6DofAeroCoreObject::UseLegacyAero().

Referenced by TurnRateAt(), and TurnRateWithConditions().

◆ Autotune()

void WsfP6DOF_MoverTestObject::Autotune ( )

References P6DofUtils::Autotune(), and mParentMover.

◆ CalcLevelFlightDragAndAlpha()

bool WsfP6DOF_MoverTestObject::CalcLevelFlightDragAndAlpha	(	double	aAltitude_ft,
		double	aMach,
		double	aGrossWeight_lbs,
		double &	aDrag_lbs,
		double &	aAlpha_deg )

protected

References P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcFpsFromMach(), P6DofVehicle::CalculateCdAreaForCoreAndControls(), P6DofVehicle::GetActiveAeroObject(), P6DofCommonController::GetAlphaVsMachCL(), GetAtmosphere(), P6DofCommonController::GetCLMaxMach(), P6DofVehicle::GetPilotManager(), P6DofVehicle::GetRefArea_sqft(), P6DofPilotManager::GetSpecialCommonController(), P6DofCommonController::GetStickForZeroMomentVsMachAlpha(), P6DofVehicle::GetWingArea_sqft(), mParentMover, and P6DofAeroCoreObject::UsesRefArea().

Referenced by GetLevelFlightDrag(), GetLevelFlightFuelBurnRate(), and GetLevelFlightHorizontalThrust().

◆ CanFlyAt()

P6DofUtils::CanFlyAtReturnValue WsfP6DOF_MoverTestObject::CanFlyAt	(	double	aAltitude_ft,
		double	aVelocity_fps,
		double	aThrottle,
		double	aFlaps = 0.0 )

References P6DofUtils::CAN_NOT_FLY, P6DofUtils::CanFlyAt(), and mParentMover.

◆ CreateAutopilotConfigFile()

void WsfP6DOF_MoverTestObject::CreateAutopilotConfigFile ( const std::string & aFilename )

References P6DofUtils::CreateAutopilotConfigFile(), and mParentMover.

◆ CreateAutopilotSupportFile()

void WsfP6DOF_MoverTestObject::CreateAutopilotSupportFile ( const std::string & aFilename )

References P6DofUtils::CreateAutopilotSupportFile(), and mParentMover.

◆ CreateAutopilotSupportFileWithMaxMach()

void WsfP6DOF_MoverTestObject::CreateAutopilotSupportFileWithMaxMach	(	const std::string &	aFilename,
		const double &	aMaxMach )

References P6DofUtils::CreateAutopilotSupportFileWithMaxMach(), and mParentMover.

◆ FlyStraightLevelFullThrottle()

void WsfP6DOF_MoverTestObject::FlyStraightLevelFullThrottle ( )

References mParentMover, P6DofPilotObject::SetTestFlapsControllerPosition(), P6DofPilotObject::SetTestStickBackControllerPosition(), P6DofPilotObject::SetTestThrottleControllerPosition(), and P6DofPilotObject::TakeTestControl().

◆ FuelBurnAtRequiredThrust()

double WsfP6DOF_MoverTestObject::FuelBurnAtRequiredThrust	(	P6DofThrustProducerObject *	aEngine,
		P6DofAtmosphere *	aAtm,
		double	aAltitude_ft,
		double	aMach,
		double	aRequiredThrust_lbs )

protected

References P6DofThrustProducerObject::AfterburnerIsPresent(), P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcFpsFromMach(), P6DofThrustProducerObject::CalculateThrust(), P6DofForceAndMomentsObject::GetForceMagnitude_lbs(), P6DofThrustProducerObject::SetThrottlePosition(), and P6DofAtmosphere::StaticPressureAtAltitude().

Referenced by GetLevelFlightFuelBurnRate().

◆ FuelBurnAtThrottleSetting()

double WsfP6DOF_MoverTestObject::FuelBurnAtThrottleSetting	(	P6DofThrustProducerObject *	aEngine,
		P6DofAtmosphere *	aAtm,
		double	aAltitude_ft,
		double	aMach,
		double	aThrottle )

protected

References P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcFpsFromMach(), P6DofThrustProducerObject::CalculateThrust(), P6DofThrustProducerObject::SetThrottlePosition(), and P6DofAtmosphere::StaticPressureAtAltitude().

◆ GetAtmosphere()

P6DofAtmosphere * WsfP6DOF_MoverTestObject::GetAtmosphere ( )

protected

References P6DofScenario::GetAtmosphere(), P6DofObject::GetScenario(), and mParentMover.

Referenced by AlphaAtDesiredDrag(), AlphaAtDesiredDrag(), CalcLevelFlightDragAndAlpha(), GetLevelFlightFuelBurnRate(), GetLevelFlightHorizontalThrust(), GetPitchingMoment(), MaxInstantaneousGLoad(), TurnRateAt(), and TurnRateWithConditions().

◆ GetLevelFlightDrag()

double WsfP6DOF_MoverTestObject::GetLevelFlightDrag	(	double	aAltitude_ft,
		double	aMach,
		double	aGrossWeight_lbs )

References CalcLevelFlightDragAndAlpha(), RestoreFromTestingMode(), and SetupForTestingMode().

◆ GetLevelFlightFuelBurnRate()

double WsfP6DOF_MoverTestObject::GetLevelFlightFuelBurnRate	(	double	aAltitude_ft,
		double	aMach,
		double	aGrossWeight_lbs )

References CalcLevelFlightDragAndAlpha(), FuelBurnAtRequiredThrust(), GetAtmosphere(), P6DofPropulsionSystem::GetNumThrustProducers(), P6DofVehicle::GetPropulsionSystem(), P6DofPropulsionSystem::GetThrustProducerByIndex(), mParentMover, RestoreFromTestingMode(), and SetupForTestingMode().

◆ GetLevelFlightHorizontalThrust()

double WsfP6DOF_MoverTestObject::GetLevelFlightHorizontalThrust	(	double	aAltitude_ft,
		double	aMach,
		double	aThrottle,
		double	aGrossWeight_lbs )

References CalcLevelFlightDragAndAlpha(), GetAtmosphere(), P6DofPropulsionSystem::GetNumThrustProducers(), P6DofVehicle::GetPropulsionSystem(), P6DofPropulsionSystem::GetThrustProducerByIndex(), mParentMover, RestoreFromTestingMode(), SetupForTestingMode(), and ThrustAtThrottleSetting().

◆ GetMaxGLoad()

double WsfP6DOF_MoverTestObject::GetMaxGLoad ( )

References P6DofPilotManager::GetActiveGuidanceAutopilot(), P6DofPilotManager::GetActiveHardwareAutopilot(), P6DofPilotManager::GetActiveManualPilot(), P6DofPilotManager::GetActiveSyntheticPilot(), P6DofPilotObject::GetCommonController(), P6DofCommonController::GetCurrentLimitsAndSettings(), P6DofVehicle::GetPilotManager(), mParentMover, and P6DOF::AutopilotLimitsAndSettings::pitchGLoad_Max.

Referenced by MaxInstantaneousGLoad().

◆ GetPitchingMoment()

double WsfP6DOF_MoverTestObject::GetPitchingMoment	(	double	aAltitude_ft,
		double	aMach,
		double	aAlpha_deg,
		double	aStickBack )

References P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcFpsFromMach(), P6DofVehicle::CalculateCmAreaForCoreAndControls(), GetAtmosphere(), mParentMover, RestoreFromTestingMode(), and SetupForTestingMode().

◆ GetRangeSinceStart_km()

double WsfP6DOF_MoverTestObject::GetRangeSinceStart_km ( ) const

References mParentMover.

◆ LimitAlphaByMaxGLoad() [1/2]

void WsfP6DOF_MoverTestObject::LimitAlphaByMaxGLoad	(	P6DofVehicle *	aVehicle,
		double	aMach,
		double	aMaxGLoad,
		double	aDynPressure_ppsqft,
		double &	aAlpha_rad )

References P6DofAeroCoreObject::CL_AlphaBetaMach(), P6DofAeroCoreObject::CL_AlphaMach(), P6DofVehicle::GetActiveAeroObject(), P6DofVehicle::GetCurrentWeight_lbs(), P6DofVehicle::GetWingArea_sqft(), and P6DofAeroCoreObject::UseLegacyAero().

Referenced by AlphaAtDesiredDrag(), and AlphaAtDesiredDrag().

◆ LimitAlphaByMaxGLoad() [2/2]

void WsfP6DOF_MoverTestObject::LimitAlphaByMaxGLoad	(	P6DofVehicle *	aVehicle,
		double	aMach,
		double	aMaxGLoad,
		double	aDynPressure_ppsqft,
		double	aCurrentMass_lbs,
		double &	aAlpha_rad )

References P6DofAeroCoreObject::CL_AlphaBetaMach(), P6DofAeroCoreObject::CL_AlphaMach(), P6DofVehicle::GetActiveAeroObject(), P6DofVehicle::GetWingArea_sqft(), and P6DofAeroCoreObject::UseLegacyAero().

◆ MaxInstantaneousGLoad()

double WsfP6DOF_MoverTestObject::MaxInstantaneousGLoad	(	double	aAltitude_ft,
		double	aMach,
		double	aCurrentMass_lbs )

References P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcFpsFromMach(), P6DofVehicle::GetActiveAeroObject(), P6DofCommonController::GetAlphaVsMachCL(), GetAtmosphere(), P6DofCommonController::GetCLMaxMach(), GetMaxGLoad(), P6DofVehicle::GetPilotManager(), P6DofVehicle::GetRefArea_sqft(), P6DofPilotManager::GetSpecialCommonController(), P6DofCommonController::GetStickForZeroMomentVsMachAlpha(), P6DofVehicle::GetWingArea_sqft(), mParentMover, and P6DofAeroCoreObject::UsesRefArea().

◆ RestoreFromTestingMode()

void WsfP6DOF_MoverTestObject::RestoreFromTestingMode ( )

protected

References P6DofScenario::GetFreezeFlags(), P6DofObject::GetScenario(), mParentMover, mTestingFreezeFuelBurn, mTestingNolag, P6DofFreezeFlags::SetMasterFreezeFuelBurn(), and P6DofFreezeFlags::SetMasterNoLagTesting().

Referenced by GetLevelFlightDrag(), GetLevelFlightFuelBurnRate(), GetLevelFlightHorizontalThrust(), GetPitchingMoment(), TurnRateAt(), and TurnRateWithConditions().

◆ SetMasterFreezeAltitude()

void WsfP6DOF_MoverTestObject::SetMasterFreezeAltitude ( bool aEnable )

References mParentMover.

◆ SetMasterFreezeFuelBurn()

void WsfP6DOF_MoverTestObject::SetMasterFreezeFuelBurn ( bool aEnable )

References mParentMover.

◆ SetMasterFreezeLocation()

void WsfP6DOF_MoverTestObject::SetMasterFreezeLocation ( bool aEnable )

References mParentMover.

◆ SetMasterFreezePitch()

void WsfP6DOF_MoverTestObject::SetMasterFreezePitch ( bool aEnable )

References mParentMover.

◆ SetMasterFreezeRoll()

void WsfP6DOF_MoverTestObject::SetMasterFreezeRoll ( bool aEnable )

References mParentMover.

◆ SetMasterFreezeVerticalSpeed()

void WsfP6DOF_MoverTestObject::SetMasterFreezeVerticalSpeed ( bool aEnable )

References mParentMover.

◆ SetMasterFreezeYaw()

void WsfP6DOF_MoverTestObject::SetMasterFreezeYaw ( bool aEnable )

References mParentMover.

◆ SetMasterNoAlphaTesting()

void WsfP6DOF_MoverTestObject::SetMasterNoAlphaTesting ( bool aEnable )

References mParentMover.

◆ SetMasterNoLagTesting()

void WsfP6DOF_MoverTestObject::SetMasterNoLagTesting ( bool aEnable )

References mParentMover.

◆ SetupForTestingMode()

void WsfP6DOF_MoverTestObject::SetupForTestingMode ( bool aFreezeFuelBurn )

protected

References P6DofScenario::GetFreezeFlags(), P6DofFreezeFlags::GetMasterFreezeFuelBurn(), P6DofFreezeFlags::GetMasterNoLagTesting(), P6DofObject::GetScenario(), mParentMover, mTestingFreezeFuelBurn, mTestingNolag, P6DofFreezeFlags::SetMasterFreezeFuelBurn(), and P6DofFreezeFlags::SetMasterNoLagTesting().

Referenced by GetLevelFlightDrag(), GetLevelFlightFuelBurnRate(), GetLevelFlightHorizontalThrust(), GetPitchingMoment(), TurnRateAt(), and TurnRateWithConditions().

◆ SetVehicleMass()

void WsfP6DOF_MoverTestObject::SetVehicleMass ( double aMass_lbs )

References mParentMover.

◆ ThrottleSettingToProduceThrust()

double WsfP6DOF_MoverTestObject::ThrottleSettingToProduceThrust	(	P6DofThrustProducerObject *	aEngine,
		P6DofAtmosphere *	aAtm,
		double	aAltitude_ft,
		double	aMach,
		double	aRequiredThrust_lbs )

protected

References P6DofThrustProducerObject::AfterburnerIsPresent(), P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcFpsFromMach(), P6DofThrustProducerObject::CalculateThrust(), P6DofForceAndMomentsObject::GetForceMagnitude_lbs(), P6DofThrustProducerObject::SetThrottlePosition(), and P6DofAtmosphere::StaticPressureAtAltitude().

◆ ThrustAtThrottleSetting()

double WsfP6DOF_MoverTestObject::ThrustAtThrottleSetting	(	P6DofThrustProducerObject *	aEngine,
		P6DofAtmosphere *	aAtm,
		double	aAltitude_ft,
		double	aMach,
		double	aThrottle )

protected

References P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcFpsFromMach(), P6DofThrustProducerObject::CalculateThrust(), P6DofForceAndMomentsObject::GetForceMagnitude_lbs(), P6DofThrustProducerObject::SetThrottlePosition(), and P6DofAtmosphere::StaticPressureAtAltitude().

Referenced by GetLevelFlightHorizontalThrust(), TurnRateAt(), and TurnRateWithConditions().

◆ TurnRateAt()

double WsfP6DOF_MoverTestObject::TurnRateAt	(	double	aSpecificExcessPower_fps,
		double	aTrueSpeed_fps,
		double	aThrottleSetting )

References AlphaAtDesiredDrag(), P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcMachFromFps(), P6DofAeroCoreObject::CL_AlphaBetaMach(), P6DofAeroCoreObject::CL_AlphaMach(), P6DofVehicle::GetActiveAeroObject(), P6DofVehicle::GetAlt_m(), GetAtmosphere(), P6DofVehicle::GetCurrentWeight_lbs(), P6DofPropulsionSystem::GetNumThrustProducers(), P6DofVehicle::GetPropulsionSystem(), P6DofPropulsionSystem::GetThrustProducerByIndex(), P6DofVehicle::GetWingArea_sqft(), mParentMover, ok, RestoreFromTestingMode(), SetupForTestingMode(), ThrustAtThrottleSetting(), and P6DofAeroCoreObject::UseLegacyAero().

◆ TurnRateWithConditions()

double WsfP6DOF_MoverTestObject::TurnRateWithConditions	(	double	aSpecificExcessPower_fps,
		double	aCurrentMass_lbs,
		double	aMaxGLoad,
		double	aAltitude_ft,
		double	aAirspeed_fps,
		double	aThrottleSetting )

References AlphaAtDesiredDrag(), P6DofAtmosphere::CalcDynamicPressure_lbft2(), P6DofAtmosphere::CalcMachFromFps(), P6DofAeroCoreObject::CL_AlphaBetaMach(), P6DofAeroCoreObject::CL_AlphaMach(), P6DofVehicle::GetActiveAeroObject(), GetAtmosphere(), P6DofPropulsionSystem::GetNumThrustProducers(), P6DofVehicle::GetPropulsionSystem(), P6DofPropulsionSystem::GetThrustProducerByIndex(), P6DofVehicle::GetWingArea_sqft(), mParentMover, ok, RestoreFromTestingMode(), SetupForTestingMode(), ThrustAtThrottleSetting(), and P6DofAeroCoreObject::UseLegacyAero().

◆ Update()

void WsfP6DOF_MoverTestObject::Update ( double aSimTime )

References mParentMover.

Member Data Documentation

◆ mParentMover

WsfP6DOF_Mover* WsfP6DOF_MoverTestObject::mParentMover = nullptr

protected

◆ mTestingFreezeFuelBurn

bool WsfP6DOF_MoverTestObject::mTestingFreezeFuelBurn = false

protected

Referenced by RestoreFromTestingMode(), and SetupForTestingMode().

◆ mTestingNolag

bool WsfP6DOF_MoverTestObject::mTestingNolag = false

protected

Referenced by RestoreFromTestingMode(), and SetupForTestingMode().

The documentation for this class was generated from the following files:

Public Member Functions

Protected Member Functions

Protected Attributes

Constructor & Destructor Documentation

◆ WsfP6DOF_MoverTestObject()

Member Function Documentation

◆ AlphaAtDesiredDrag() [1/2]

◆ AlphaAtDesiredDrag() [2/2]

◆ Autotune()

◆ CalcLevelFlightDragAndAlpha()

◆ CanFlyAt()

◆ CreateAutopilotConfigFile()

◆ CreateAutopilotSupportFile()

◆ CreateAutopilotSupportFileWithMaxMach()

◆ FlyStraightLevelFullThrottle()

◆ FuelBurnAtRequiredThrust()

◆ FuelBurnAtThrottleSetting()

◆ GetAtmosphere()

◆ GetLevelFlightDrag()

◆ GetLevelFlightFuelBurnRate()

◆ GetLevelFlightHorizontalThrust()

◆ GetMaxGLoad()

◆ GetPitchingMoment()

◆ GetRangeSinceStart_km()

◆ LimitAlphaByMaxGLoad() [1/2]

◆ LimitAlphaByMaxGLoad() [2/2]

◆ MaxInstantaneousGLoad()

◆ RestoreFromTestingMode()

◆ SetMasterFreezeAltitude()

◆ SetMasterFreezeFuelBurn()

◆ SetMasterFreezeLocation()

◆ SetMasterFreezePitch()

◆ SetMasterFreezeRoll()

◆ SetMasterFreezeVerticalSpeed()

◆ SetMasterFreezeYaw()

◆ SetMasterNoAlphaTesting()

◆ SetMasterNoLagTesting()

◆ SetupForTestingMode()

◆ SetVehicleMass()

◆ ThrottleSettingToProduceThrust()

◆ ThrustAtThrottleSetting()

◆ TurnRateAt()

◆ TurnRateWithConditions()

◆ Update()

Member Data Documentation

◆ mParentMover

◆ mTestingFreezeFuelBurn

◆ mTestingNolag