wsf::six_dof::utils Namespace Reference

Enumerations
enum	CanFlyAtReturnValue { CAN_NOT_FLY , CONTROL_FAIL , CAN_FLY }

Functions
WSF_SIX_DOF_EXPORT PointMassMover *	CastToPointMass (Mover *aVehicle)
WSF_SIX_DOF_EXPORT void	CreateAutopilotConfigFile (PointMassMover *aVehicle, const std::string &aFilename)
WSF_SIX_DOF_EXPORT CanFlyAtReturnValue	CanFlyAt (PointMassMover *aObject, double aAltitude_ft, double aVelocity_fps, double aThrottleForward, double aFlapsDown)
WSF_SIX_DOF_EXPORT void	CreateAutopilotSupportFile (PointMassMover *aObject, const std::string &aFilename)
WSF_SIX_DOF_EXPORT void	CreateAutopilotSupportFileWithMaxMach (PointMassMover *aObject, const std::string &aFilename, const double &aMaxMach)
WSF_SIX_DOF_EXPORT void	CommonCreateAutopilotSupportFile (PointMassTableTool &aTool, const std::string &aFilename)
WSF_SIX_DOF_EXPORT RigidBodyMover *	CastToRigidBody (Mover *aVehicle)
WSF_SIX_DOF_EXPORT void	Autotune (RigidBodyMover *aVehicle)
WSF_SIX_DOF_EXPORT void	CreateAutopilotConfigFile (const RigidBodyMover *aVehicle, const std::string &aFilename)
WSF_SIX_DOF_EXPORT std::vector< Pid::Type >	GetRelevantPids (const RigidBodyMover *aVehicle)
WSF_SIX_DOF_EXPORT CanFlyAtReturnValue	CanFlyAt (RigidBodyMover *aObject, double aAltitude_ft, double aVelocity_fps, double aThrottleForward, double aFlapsDown)
WSF_SIX_DOF_EXPORT void	CreateAutopilotSupportFile (RigidBodyMover *aObject, const std::string &aFilename)
WSF_SIX_DOF_EXPORT void	CreateAutopilotSupportFileWithMaxMach (RigidBodyMover *aObject, const std::string &aFilename, const double &aMaxMach)
WSF_SIX_DOF_EXPORT void	CommonCreateAutopilotSupportFile (RigidBodyTableTool &aTool, const std::string &aFilename)
WSF_SIX_DOF_EXPORT double	GetSphericalEarthRadius_m ()
WSF_SIX_DOF_EXPORT const SinglePidValueData &	GetSinglePidData (Pid::Type aPidType, const AutopilotPidGroupValueData &aPidValues)
std::string	OutputDoubleString (double aValue, int aWidth, int aPrecision)
WSF_SIX_DOF_EXPORT int64_t	TimeToTime (double aSimTime_sec)
WSF_SIX_DOF_EXPORT double	TimeToTime (int64_t aSimTime_nanosec)
WSF_SIX_DOF_EXPORT double	NextGuessFromFalsePosition (double aInputA, double aOutputA, double aInputB, double aOutputB)
WSF_SIX_DOF_EXPORT void	UpdateFalsePositionBounds (double &aInputA, double &aOutputA, double &aInputB, double &aOutputB, double aInputC, double aOutputC)
WSF_SIX_DOF_EXPORT void	CalcUnitVectors (const UtDCM &aDCM, UtVec3dX &aUnitVecX, UtVec3dX &aUnitVecY, UtVec3dX &aUnitVecZ)
WSF_SIX_DOF_EXPORT void	CalcLocalNEDVectors (const UtVec3dX &aPos, UtVec3dX &aLocalNorth, UtVec3dX &aLocalEast, UtVec3dX &aLocalDown)
WSF_SIX_DOF_EXPORT void	CalcLocalAngles (const UtVec3dX &aLocalNorth, const UtVec3dX &aLocalEast, const UtVec3dX &aLocalDown, const UtVec3dX &aUnitVecX, const UtVec3dX &aUnitVecZ, double &aLocalYaw_rad, double &aLocalPitch_rad, double &aLocalRoll_rad)
WSF_SIX_DOF_EXPORT void	InertialToBodyRel (const UtDCM &aMatrix, const UtVec3dX &aInertial, UtVec3dX &aBodyRel)
WSF_SIX_DOF_EXPORT void	DCM_InertialToBodyRel (const UtDCM &aMatrix, const UtVec3dX &aInertial, UtVec3dX &aBodyRel)
WSF_SIX_DOF_EXPORT void	AlphaBetaFromInertialVel (const UtDCM &aMatrix, const UtVec3dX &aInertialVel_mps, double &aSpeed_fps, double &aAlpha_deg, double &aBeta_deg)
WSF_SIX_DOF_EXPORT void	AlphaBetaFromBodyRelVel (const UtVec3dX &aVel_fps, double &aAlpha_deg, double &aBeta_deg, double &aSpeed_fps)
WSF_SIX_DOF_EXPORT void	AlphaBetaFromBodyRelVel (const UtVec3dX &aVel_fps, double &aAlpha_deg, double &aBeta_deg)
WSF_SIX_DOF_EXPORT void	LimitThrottleNormalized (double &aThrottle)
WSF_SIX_DOF_EXPORT void	LimitThrottleAfterburner (double &aThrottle)

Variables
static constexpr int64_t	cDT_RIGID_BODY_NANOSEC = 10000000
static constexpr int64_t	cDT_POINT_MASS_NANOSEC = 50000000
static constexpr double	cDT_RIGID_BODY_SEC = (0.000000001 * static_cast<double>(cDT_RIGID_BODY_NANOSEC))
static constexpr double	cDT_POINT_MASS_SEC = (0.000000001 * static_cast<double>(cDT_POINT_MASS_NANOSEC))
static constexpr int64_t	cEPSILON_SIMTIME_NANOSEC = 100
static constexpr double	cEPSILON_SIMTIME_SEC = (0.000000001 * static_cast<double>(cEPSILON_SIMTIME_NANOSEC))
static constexpr double	cREFERENCE_GRAV_ACCEL_MPS2 = 9.80665

Enumeration Type Documentation

CanFlyAtReturnValue

enum wsf::six_dof::utils::CanFlyAtReturnValue

Enumerator
CAN_NOT_FLY
CONTROL_FAIL
CAN_FLY

Function Documentation

AlphaBetaFromBodyRelVel() [1/2]

void wsf::six_dof::utils::AlphaBetaFromBodyRelVel	(	const UtVec3dX &	aVel_fps,
		double &	aAlpha_deg,
		double &	aBeta_deg )

AlphaBetaFromBodyRelVel() [2/2]

void wsf::six_dof::utils::AlphaBetaFromBodyRelVel	(	const UtVec3dX &	aVel_fps,
		double &	aAlpha_deg,
		double &	aBeta_deg,
		double &	aSpeed_fps )

References AlphaBetaFromBodyRelVel().

Referenced by AlphaBetaFromBodyRelVel(), and AlphaBetaFromInertialVel().

AlphaBetaFromInertialVel()

void wsf::six_dof::utils::AlphaBetaFromInertialVel	(	const UtDCM &	aMatrix,
		const UtVec3dX &	aInertialVel_mps,
		double &	aSpeed_fps,
		double &	aAlpha_deg,
		double &	aBeta_deg )

References AlphaBetaFromBodyRelVel(), and DCM_InertialToBodyRel().

Referenced by wsf::six_dof::KinematicState::CalculateSecondaryParameters(), and wsf::six_dof::KinematicState::UpdateAeroState().

Autotune()

void wsf::six_dof::utils::Autotune

(

RigidBodyMover *

aVehicle

)

References wsf::six_dof::TunerGAManager::Advance(), wsf::six_dof::Pid::Alpha, wsf::six_dof::Pid::Altitude, wsf::six_dof::Pid::BankAngle, wsf::six_dof::Pid::Beta, wsf::six_dof::Pid::DeltaPitch, wsf::six_dof::Pid::DeltaRoll, wsf::six_dof::Pid::FlightPathAngle, wsf::six_dof::RigidBodyMover::ForceLandingGearDownInstantly(), wsf::six_dof::Mover::GetActivePilotObject(), wsf::six_dof::CommonController::GetAutopilotPidValues(), wsf::six_dof::PilotObject::GetCommonController(), wsf::six_dof::TunerGAManager::GetCurrentSpecimen(), wsf::six_dof::Mover::GetEnvironment(), wsf::six_dof::TunerGASpecimen::GetKd(), wsf::six_dof::TunerGASpecimen::GetKi(), wsf::six_dof::TunerGASpecimen::GetKp(), wsf::six_dof::RigidBodyMover::GetLandingGear(), wsf::six_dof::RigidBodyLandingGear::GetNominalHeightAboveGroundOnGear(), wsf::six_dof::TunerGAManager::GetOptimum(), GetRelevantPids(), GetSinglePidData(), wsf::six_dof::Mover::GetStartingLatLon(), wsf::six_dof::Environment::GetTerrainElevation(), wsf::six_dof::TunerGAManager::InitializePopulation(), wsf::six_dof::TunerGAManager::IsComplete(), wsf::six_dof::TunerGASpecimen::PidLogElement::pidValues, wsf::six_dof::Pid::PitchAngle, wsf::six_dof::Pid::PitchRate, wsf::six_dof::Pid::RollHeading, wsf::six_dof::Pid::RollRate, wsf::six_dof::PilotObject::SetAutopilotAlpha(), wsf::six_dof::PilotObject::SetAutopilotAltitude(), wsf::six_dof::PilotObject::SetAutopilotBeta(), wsf::six_dof::PilotObject::SetAutopilotDeltaPitch(), wsf::six_dof::PilotObject::SetAutopilotDeltaRoll(), wsf::six_dof::PilotObject::SetAutopilotFlightPathAngle(), wsf::six_dof::PilotObject::SetAutopilotPitchAngle(), wsf::six_dof::PilotObject::SetAutopilotPitchRate(), wsf::six_dof::PilotObject::SetAutopilotRollAngle(), wsf::six_dof::PilotObject::SetAutopilotRollHeading(), wsf::six_dof::PilotObject::SetAutopilotRollRate(), wsf::six_dof::PilotObject::SetAutopilotSpeedKTAS(), wsf::six_dof::PilotObject::SetAutopilotVerticalSpeed(), wsf::six_dof::PilotObject::SetAutopilotYawHeading(), wsf::six_dof::PilotObject::SetAutopilotYawRate(), wsf::six_dof::CommonController::SetPidGainKD(), wsf::six_dof::CommonController::SetPidGainKI(), wsf::six_dof::CommonController::SetPidGainKP(), wsf::six_dof::PilotObject::SetPrePositionTAS(), wsf::six_dof::Pid::Speed, wsf::six_dof::Pid::TaxiHeading, wsf::six_dof::Pid::TaxiSpeed, wsf::six_dof::Pid::TaxiYawRate, wsf::six_dof::TunerGASpecimen::PidLogElement::timeStamp, wsf::six_dof::Mover::Update(), wsf::six_dof::Pid::VerticalSpeed, wsf::six_dof::Pid::YawHeading, and wsf::six_dof::Pid::YawRate.

Referenced by wsf::six_dof::RigidBodyMoverTestObject::Autotune().

CalcLocalAngles()

void wsf::six_dof::utils::CalcLocalAngles	(	const UtVec3dX &	aLocalNorth,
		const UtVec3dX &	aLocalEast,
		const UtVec3dX &	aLocalDown,
		const UtVec3dX &	aUnitVecX,
		const UtVec3dX &	aUnitVecZ,
		double &	aLocalYaw_rad,
		double &	aLocalPitch_rad,
		double &	aLocalRoll_rad )

CalcLocalNEDVectors()

void wsf::six_dof::utils::CalcLocalNEDVectors	(	const UtVec3dX &	aPos,
		UtVec3dX &	aLocalNorth,
		UtVec3dX &	aLocalEast,
		UtVec3dX &	aLocalDown )

CalcUnitVectors()

void wsf::six_dof::utils::CalcUnitVectors	(	const UtDCM &	aDCM,
		UtVec3dX &	aUnitVecX,
		UtVec3dX &	aUnitVecY,
		UtVec3dX &	aUnitVecZ )

CanFlyAt() [1/2]

wsf::six_dof::utils::CanFlyAtReturnValue wsf::six_dof::utils::CanFlyAt	(	PointMassMover *	aObject,
		double	aAltitude_ft,
		double	aVelocity_fps,
		double	aThrottleForward,
		double	aFlapsDown )

References CAN_FLY, CAN_NOT_FLY, CONTROL_FAIL, wsf::six_dof::Mover::GetAccelNED_mps2(), wsf::six_dof::Mover::GetKinematicState(), wsf::six_dof::KinematicState::GetOmegaBodyDot(), wsf::six_dof::Mover::GetVertSpeed_fpm(), and wsf::six_dof::Mover::TestingUpdate().

Referenced by wsf::six_dof::PointMassMoverTestObject::CanFlyAt(), and wsf::six_dof::RigidBodyMoverTestObject::CanFlyAt().

CanFlyAt() [2/2]

wsf::six_dof::utils::CanFlyAtReturnValue wsf::six_dof::utils::CanFlyAt	(	RigidBodyMover *	aObject,
		double	aAltitude_ft,
		double	aVelocity_fps,
		double	aThrottleForward,
		double	aFlapsDown )

References CAN_FLY, CAN_NOT_FLY, CONTROL_FAIL, wsf::six_dof::Mover::GetAccelNED_mps2(), wsf::six_dof::Mover::GetKinematicState(), wsf::six_dof::KinematicState::GetOmegaBodyDot(), wsf::six_dof::Mover::GetVertSpeed_fpm(), and wsf::six_dof::Mover::TestingUpdate().

CastToPointMass()

wsf::six_dof::PointMassMover * wsf::six_dof::utils::CastToPointMass

(

Mover *

aVehicle

)

Referenced by wsf::six_dof::PointMassCommonController::SetParentVehicle().

CastToRigidBody()

wsf::six_dof::RigidBodyMover * wsf::six_dof::utils::CastToRigidBody

(

Mover *

aVehicle

)

Referenced by wsf::six_dof::RigidBodyGroundReactionPoint::CalcGroundReactionForceMoment(), wsf::six_dof::RigidBodyGroundReactionPoint::CalcNormalForceMoment(), wsf::six_dof::RigidBodyGroundReactionPoint::GetSteeringData(), wsf::six_dof::RigidBodyGroundReactionPoint::Initialize(), wsf::six_dof::RigidBodyLandingGear::Initialize(), wsf::six_dof::RigidBodyCommonController::SetParentVehicle(), wsf::six_dof::RigidBodyLandingGear::Update(), and wsf::six_dof::RigidBodyLandingGear::VehicleIsAtRest().

CommonCreateAutopilotSupportFile() [1/2]

void wsf::six_dof::utils::CommonCreateAutopilotSupportFile	(	PointMassTableTool &	aTool,
		const std::string &	aFilename )

References wsf::six_dof::PointMassTableTool::CreateAutopilotTables(), wsf::six_dof::PointMassTableTool::OutputAlphaMachCLTableToInputString(), wsf::six_dof::PointMassTableTool::OutputAlphaMaxMachTableToInputString(), wsf::six_dof::PointMassTableTool::OutputAlphaMinMachTableToInputString(), wsf::six_dof::PointMassTableTool::OutputCLMachAlphaTableToInputString(), wsf::six_dof::PointMassTableTool::OutputCLMaxMachTableToInputString(), and wsf::six_dof::PointMassTableTool::OutputCLMinMachTableToInputString().

Referenced by CreateAutopilotSupportFile(), CreateAutopilotSupportFile(), CreateAutopilotSupportFileWithMaxMach(), and CreateAutopilotSupportFileWithMaxMach().

CommonCreateAutopilotSupportFile() [2/2]

void wsf::six_dof::utils::CommonCreateAutopilotSupportFile	(	RigidBodyTableTool &	aTool,
		const std::string &	aFilename )

References wsf::six_dof::RigidBodyTableTool::CreateAutopilotTables(), wsf::six_dof::RigidBodyTableTool::OutputAlphaMachCLTableToInputString(), wsf::six_dof::RigidBodyTableTool::OutputAlphaMaxMachTableToInputString(), wsf::six_dof::RigidBodyTableTool::OutputAlphaMinMachTableToInputString(), wsf::six_dof::RigidBodyTableTool::OutputCLMachAlphaTableToInputString(), wsf::six_dof::RigidBodyTableTool::OutputCLMaxMachTableToInputString(), wsf::six_dof::RigidBodyTableTool::OutputCLMinMachTableToInputString(), and wsf::six_dof::RigidBodyTableTool::OutputStickMachAlphaTablesToInputString().

CreateAutopilotConfigFile() [1/2]

void wsf::six_dof::utils::CreateAutopilotConfigFile	(	const RigidBodyMover *	aVehicle,
		const std::string &	aFilename )

References wsf::six_dof::AutopilotLimitsAndSettings::afterburnerThreshold, wsf::six_dof::Pid::Alpha, wsf::six_dof::AutopilotLimitsAndSettings::alpha_Max, wsf::six_dof::AutopilotLimitsAndSettings::alpha_Min, wsf::six_dof::Pid::Altitude, wsf::six_dof::Pid::BankAngle, wsf::six_dof::AutopilotLimitsAndSettings::bankAngle_Max, wsf::six_dof::Control::BankToTurnNoYaw, wsf::six_dof::Control::BankToTurnWithYaw, wsf::six_dof::Pid::Beta, wsf::six_dof::AutopilotLimitsAndSettings::beta_Max, wsf::six_dof::Pid::DeltaPitch, wsf::six_dof::Pid::DeltaRoll, wsf::six_dof::Pid::FlightPathAngle, wsf::six_dof::Pid::ForwardAccel, wsf::six_dof::AutopilotLimitsAndSettings::forwardAccel_Max, wsf::six_dof::AutopilotLimitsAndSettings::forwardAccel_Min, wsf::six_dof::Mover::GetActivePilotObject(), wsf::six_dof::PilotObject::GetCommonController(), wsf::six_dof::CommonController::GetControlMethod(), wsf::six_dof::CommonController::GetCurrentLimitsAndSettings(), wsf::six_dof::Pid::PitchAngle, wsf::six_dof::AutopilotLimitsAndSettings::pitchGLoad_Max, wsf::six_dof::AutopilotLimitsAndSettings::pitchGLoad_Min, wsf::six_dof::Pid::PitchRate, wsf::six_dof::AutopilotLimitsAndSettings::pitchRate_Max, wsf::six_dof::AutopilotLimitsAndSettings::pitchRate_Min, wsf::six_dof::Pid::RollHeading, wsf::six_dof::Pid::RollRate, wsf::six_dof::AutopilotLimitsAndSettings::rollRate_Max, wsf::six_dof::AutopilotLimitsAndSettings::routeAllowableAngleError_rad, wsf::six_dof::Pid::Speed, wsf::six_dof::AutopilotLimitsAndSettings::speedBrakeThreshold, wsf::six_dof::Pid::TaxiForwardAccel, wsf::six_dof::Pid::TaxiHeading, wsf::six_dof::Pid::TaxiSpeed, wsf::six_dof::AutopilotLimitsAndSettings::taxiSpeed_Max, wsf::six_dof::Pid::TaxiYawRate, wsf::six_dof::AutopilotLimitsAndSettings::taxiYawRate_Max, wsf::six_dof::AutopilotLimitsAndSettings::turnRollInMultiplier, wsf::six_dof::Pid::VerticalSpeed, wsf::six_dof::AutopilotLimitsAndSettings::vertSpd_Max, wsf::six_dof::AutopilotLimitsAndSettings::vertSpd_Min, WritePIDBlock(), wsf::six_dof::AutopilotLimitsAndSettings::yawGLoad_Max, wsf::six_dof::Pid::YawHeading, wsf::six_dof::Pid::YawRate, wsf::six_dof::AutopilotLimitsAndSettings::yawRate_Max, wsf::six_dof::Control::YawToTurnNoRoll, wsf::six_dof::Control::YawToTurnRollRate, and wsf::six_dof::Control::YawToTurnZeroBank.

CreateAutopilotConfigFile() [2/2]

void wsf::six_dof::utils::CreateAutopilotConfigFile	(	PointMassMover *	aVehicle,
		const std::string &	aFilename )

References wsf::six_dof::AutopilotLimitsAndSettings::afterburnerThreshold, wsf::six_dof::AutopilotLimitsAndSettings::alpha_Max, wsf::six_dof::AutopilotLimitsAndSettings::alpha_Min, wsf::six_dof::Pid::Altitude, wsf::six_dof::Pid::BankAngle, wsf::six_dof::AutopilotLimitsAndSettings::bankAngle_Max, wsf::six_dof::Control::BankToTurnNoYaw, wsf::six_dof::Control::BankToTurnWithYaw, wsf::six_dof::AutopilotLimitsAndSettings::beta_Max, wsf::six_dof::Pid::FlightPathAngle, wsf::six_dof::Pid::ForwardAccel, wsf::six_dof::AutopilotLimitsAndSettings::forwardAccel_Max, wsf::six_dof::AutopilotLimitsAndSettings::forwardAccel_Min, wsf::six_dof::Mover::GetActivePilotObject(), wsf::six_dof::PilotObject::GetCommonController(), wsf::six_dof::CommonController::GetControlMethod(), wsf::six_dof::CommonController::GetCurrentLimitsAndSettings(), wsf::six_dof::Pid::PitchAngle, wsf::six_dof::AutopilotLimitsAndSettings::pitchGLoad_Max, wsf::six_dof::AutopilotLimitsAndSettings::pitchGLoad_Min, wsf::six_dof::Pid::PitchRate, wsf::six_dof::AutopilotLimitsAndSettings::pitchRate_Max, wsf::six_dof::AutopilotLimitsAndSettings::pitchRate_Min, wsf::six_dof::Pid::RollHeading, wsf::six_dof::AutopilotLimitsAndSettings::rollRate_Max, wsf::six_dof::AutopilotLimitsAndSettings::routeAllowableAngleError_rad, wsf::six_dof::Pid::Speed, wsf::six_dof::AutopilotLimitsAndSettings::speedBrakeThreshold, wsf::six_dof::AutopilotLimitsAndSettings::turnRollInMultiplier, wsf::six_dof::Pid::VerticalSpeed, wsf::six_dof::AutopilotLimitsAndSettings::vertSpd_Max, wsf::six_dof::AutopilotLimitsAndSettings::vertSpd_Min, WritePIDBlock(), wsf::six_dof::AutopilotLimitsAndSettings::yawGLoad_Max, wsf::six_dof::Pid::YawHeading, wsf::six_dof::Pid::YawRate, wsf::six_dof::AutopilotLimitsAndSettings::yawRate_Max, wsf::six_dof::Control::YawToTurnNoRoll, wsf::six_dof::Control::YawToTurnRollRate, and wsf::six_dof::Control::YawToTurnZeroBank.

Referenced by wsf::six_dof::PointMassMoverTestObject::CreateAutopilotConfigFile(), and wsf::six_dof::RigidBodyMoverTestObject::CreateAutopilotConfigFile().

CreateAutopilotSupportFile() [1/2]

void wsf::six_dof::utils::CreateAutopilotSupportFile	(	PointMassMover *	aObject,
		const std::string &	aFilename )

References CommonCreateAutopilotSupportFile().

Referenced by wsf::six_dof::PointMassMoverTestObject::CreateAutopilotSupportFile(), and wsf::six_dof::RigidBodyMoverTestObject::CreateAutopilotSupportFile().

CreateAutopilotSupportFile() [2/2]

void wsf::six_dof::utils::CreateAutopilotSupportFile	(	RigidBodyMover *	aObject,
		const std::string &	aFilename )

References CommonCreateAutopilotSupportFile().

CreateAutopilotSupportFileWithMaxMach() [1/2]

void wsf::six_dof::utils::CreateAutopilotSupportFileWithMaxMach	(	PointMassMover *	aObject,
		const std::string &	aFilename,
		const double &	aMaxMach )

References CommonCreateAutopilotSupportFile(), and wsf::six_dof::PointMassTableTool::InitializeTableMachValues().

Referenced by wsf::six_dof::PointMassMoverTestObject::CreateAutopilotSupportFileWithMaxMach(), and wsf::six_dof::RigidBodyMoverTestObject::CreateAutopilotSupportFileWithMaxMach().

CreateAutopilotSupportFileWithMaxMach() [2/2]

void wsf::six_dof::utils::CreateAutopilotSupportFileWithMaxMach	(	RigidBodyMover *	aObject,
		const std::string &	aFilename,
		const double &	aMaxMach )

References CommonCreateAutopilotSupportFile(), and wsf::six_dof::RigidBodyTableTool::InitializeTableMachValues().

DCM_InertialToBodyRel()

void wsf::six_dof::utils::DCM_InertialToBodyRel	(	const UtDCM &	aMatrix,
		const UtVec3dX &	aInertial,
		UtVec3dX &	aBodyRel )

Referenced by AlphaBetaFromInertialVel().

GetRelevantPids()

std::vector< wsf::six_dof::Pid::Type > wsf::six_dof::utils::GetRelevantPids

(

const RigidBodyMover *

aVehicle

)

References wsf::six_dof::RigidBodyMover::HasLandingGear(), wsf::six_dof::Pid::TaxiHeading, wsf::six_dof::Pid::TaxiSpeed, and wsf::six_dof::Pid::TaxiYawRate.

Referenced by Autotune().

GetSinglePidData()

const wsf::six_dof::SinglePidValueData & wsf::six_dof::utils::GetSinglePidData	(	Pid::Type	aPidType,
		const AutopilotPidGroupValueData &	aPidValues )

References wsf::six_dof::Pid::Alpha, wsf::six_dof::AutopilotPidGroupValueData::alphaPID, wsf::six_dof::Pid::Altitude, wsf::six_dof::AutopilotPidGroupValueData::altitudePID, wsf::six_dof::Pid::BankAngle, wsf::six_dof::AutopilotPidGroupValueData::bankAnglePID, wsf::six_dof::Pid::Beta, wsf::six_dof::AutopilotPidGroupValueData::betaPID, wsf::six_dof::Pid::DeltaPitch, wsf::six_dof::AutopilotPidGroupValueData::deltaPitchPID, wsf::six_dof::Pid::DeltaRoll, wsf::six_dof::AutopilotPidGroupValueData::deltaRollPID, wsf::six_dof::Pid::FlightPathAngle, wsf::six_dof::AutopilotPidGroupValueData::flightPathAnglePID, wsf::six_dof::Pid::ForwardAccel, wsf::six_dof::AutopilotPidGroupValueData::forwardAccelPID, wsf::six_dof::Pid::PitchAngle, wsf::six_dof::AutopilotPidGroupValueData::pitchAnglePID, wsf::six_dof::Pid::PitchRate, wsf::six_dof::AutopilotPidGroupValueData::pitchRatePID, wsf::six_dof::Pid::RollHeading, wsf::six_dof::AutopilotPidGroupValueData::rollHeadingPID, wsf::six_dof::Pid::RollRate, wsf::six_dof::AutopilotPidGroupValueData::rollRatePID, wsf::six_dof::Pid::Speed, wsf::six_dof::AutopilotPidGroupValueData::speedPID, wsf::six_dof::Pid::TaxiHeading, wsf::six_dof::AutopilotPidGroupValueData::taxiHeadingPID, wsf::six_dof::Pid::TaxiSpeed, wsf::six_dof::AutopilotPidGroupValueData::taxiSpeedPID, wsf::six_dof::Pid::TaxiYawRate, wsf::six_dof::AutopilotPidGroupValueData::taxiYawRatePID, wsf::six_dof::Pid::VerticalSpeed, wsf::six_dof::AutopilotPidGroupValueData::verticalSpeedPID, wsf::six_dof::Pid::YawHeading, wsf::six_dof::AutopilotPidGroupValueData::yawheadingPID, wsf::six_dof::Pid::YawRate, and wsf::six_dof::AutopilotPidGroupValueData::yawRatePID.

Referenced by Autotune().

GetSphericalEarthRadius_m()

WSF_SIX_DOF_EXPORT double wsf::six_dof::utils::GetSphericalEarthRadius_m

(

)

InertialToBodyRel()

void wsf::six_dof::utils::InertialToBodyRel	(	const UtDCM &	aMatrix,
		const UtVec3dX &	aInertial,
		UtVec3dX &	aBodyRel )

LimitThrottleAfterburner()

void wsf::six_dof::utils::LimitThrottleAfterburner

(

double &

aThrottle

)

Referenced by wsf::six_dof::JetEngine::CalculateThrust(), wsf::six_dof::PointMassPropulsionSystem::SetThrottleLeverPosition(), wsf::six_dof::RigidBodyPropulsionSystem::SetThrottleLeverPosition(), and wsf::six_dof::JetEngine::SetThrottlePosition().

LimitThrottleNormalized()

void wsf::six_dof::utils::LimitThrottleNormalized

(

double &

aThrottle

)

Referenced by wsf::six_dof::RamjetEngine::CalcThrustMultiplier(), wsf::six_dof::JetEngine::CalculateThrust(), wsf::six_dof::RocketLiquidPropellantEngine::CalculateThrust(), wsf::six_dof::RocketSolidPropellantEngine::CalculateThrust(), wsf::six_dof::PointMassPropulsionSystem::SetThrottleLeverPosition(), wsf::six_dof::RigidBodyPropulsionSystem::SetThrottleLeverPosition(), wsf::six_dof::JetEngine::SetThrottlePosition(), wsf::six_dof::RamjetEngine::SetThrottlePosition(), wsf::six_dof::RocketLiquidPropellantEngine::SetThrottlePosition(), and wsf::six_dof::RocketSolidPropellantEngine::SetThrottlePosition().

NextGuessFromFalsePosition()

double wsf::six_dof::utils::NextGuessFromFalsePosition	(	double	aInputA,
		double	aOutputA,
		double	aInputB,
		double	aOutputB )

Referenced by wsf::six_dof::MoverTestObject::FuelBurnAtRequiredThrust(), and wsf::six_dof::MoverTestObject::ThrottleSettingToProduceThrust().

OutputDoubleString()

std::string wsf::six_dof::utils::OutputDoubleString	(	double	aValue,
		int	aWidth,
		int	aPrecision )

Referenced by wsf::six_dof::PointMassMachDataTable::OutputToString(), wsf::six_dof::PointMassMachParamDataTable::OutputToString(), wsf::six_dof::RigidBodyMachDataTable::OutputToString(), and wsf::six_dof::RigidBodyMachParamDataTable::OutputToString().

TimeToTime() [1/2]

int64_t wsf::six_dof::utils::TimeToTime

(

double

aSimTime_sec

)

Referenced by wsf::six_dof::RigidBodyMover::CalculateLandingGearFM(), wsf::six_dof::PointMassMover::CalculatePropulsionFM(), wsf::six_dof::RigidBodyMover::CalculatePropulsionFM(), wsf::six_dof::RocketLiquidPropellantEngine::CalculateThrust(), wsf::six_dof::RocketSolidPropellantEngine::CalculateThrust(), wsf::six_dof::Mover::CalculateWashIn(), wsf::six_dof::Mover::DirectJettisonOfSubobject(), wsf::six_dof::RigidBodyCommonController::GetAimHeadingAndTurnRateForTaxiWaypointNav_deg(), wsf::six_dof::CommonController::GetAimHeadingForWaypointNav_deg(), wsf::six_dof::Mover::GetLastUpdateTime_sec(), wsf::six_dof::Mover::GetLifeTime_sec(), wsf::six_dof::Mover::GetStepSize_sec(), wsf::six_dof::Mover::GetTimeOfFlight_sec(), wsf::six_dof::Mover::Initialize(), wsf::six_dof::PointMassMover::InitializeDetails(), wsf::six_dof::RigidBodyMover::InitializeDetails(), wsf::six_dof::Mover::InitializeSequencers(), wsf::six_dof::PointMassMover::ObjectPropulsionCalculations(), wsf::six_dof::RigidBodyMover::ObjectPropulsionCalculations(), wsf::six_dof::Mover::PerformCrash(), wsf::six_dof::Sequencer::ProcessInput(), wsf::six_dof::PointMassCommonController::ProcessStandardLateralNavMode_Beta(), wsf::six_dof::PointMassCommonController::ProcessStandardVerticalNavMode_Alpha(), wsf::six_dof::PointMassMover::SetLastSimTime(), wsf::six_dof::RigidBodyMover::SetLastSimTime(), wsf::six_dof::GuidanceComputer::StopEngines(), wsf::six_dof::Mover::Update(), wsf::six_dof::PointMassCommonController::Update(), wsf::six_dof::PointMassControlActuator::Update(), wsf::six_dof::PointMassIntegrator::Update(), wsf::six_dof::PropulsionSystem::Update(), wsf::six_dof::RigidBodyCommonController::Update(), wsf::six_dof::RigidBodyControlActuator::Update(), wsf::six_dof::RigidBodyIntegrator::Update(), wsf::six_dof::RigidBodyLandingGear::Update(), wsf::six_dof::KinematicState::UpdateAeroState(), wsf::six_dof::Mover::UpdateFuelBurn(), and wsf::six_dof::Mover::UpdateObject().

TimeToTime() [2/2]

double wsf::six_dof::utils::TimeToTime

(

int64_t

aSimTime_nanosec

)

UpdateFalsePositionBounds()

void wsf::six_dof::utils::UpdateFalsePositionBounds	(	double &	aInputA,
		double &	aOutputA,
		double &	aInputB,
		double &	aOutputB,
		double	aInputC,
		double	aOutputC )

Referenced by wsf::six_dof::MoverTestObject::FuelBurnAtRequiredThrust(), and wsf::six_dof::MoverTestObject::ThrottleSettingToProduceThrust().

Variable Documentation

cDT_POINT_MASS_NANOSEC

int64_t wsf::six_dof::utils::cDT_POINT_MASS_NANOSEC = 50000000

staticconstexpr

cDT_POINT_MASS_SEC

double wsf::six_dof::utils::cDT_POINT_MASS_SEC = (0.000000001 * static_cast<double>(cDT_POINT_MASS_NANOSEC))

staticconstexpr

cDT_RIGID_BODY_NANOSEC

int64_t wsf::six_dof::utils::cDT_RIGID_BODY_NANOSEC = 10000000

staticconstexpr

cDT_RIGID_BODY_SEC

double wsf::six_dof::utils::cDT_RIGID_BODY_SEC = (0.000000001 * static_cast<double>(cDT_RIGID_BODY_NANOSEC))

staticconstexpr

Referenced by wsf::six_dof::CommonController::NestedFeedbackLoop::GetMiddleLoopInterval_sec(), and wsf::six_dof::CommonController::NestedFeedbackLoop::GetOuterLoopInterval_sec().

cEPSILON_SIMTIME_NANOSEC

int64_t wsf::six_dof::utils::cEPSILON_SIMTIME_NANOSEC = 100

staticconstexpr

Referenced by wsf::six_dof::Mover::Update(), and wsf::six_dof::KinematicState::UpdateAeroState().

cEPSILON_SIMTIME_SEC

double wsf::six_dof::utils::cEPSILON_SIMTIME_SEC = (0.000000001 * static_cast<double>(cEPSILON_SIMTIME_NANOSEC))

staticconstexpr

Referenced by wsf::six_dof::RigidBodyGroundReactionPoint::CalcGroundReactionForceMoment(), wsf::six_dof::RigidBodyGroundReactionPoint::CalcNormalForceMoment(), wsf::six_dof::FuelTank::CalculateFuelBurn(), wsf::six_dof::FuelTank::CalculateFuelFill(), wsf::six_dof::FuelTank::CalculateFuelTransfer(), wsf::six_dof::JetEngine::CalculateThrust(), wsf::six_dof::RamjetEngine::CalculateThrust(), wsf::six_dof::RocketLiquidPropellantEngine::CalculateThrust(), wsf::six_dof::RocketSolidPropellantEngine::CalculateThrust(), wsf::six_dof::PointMassMover::InitializeDetails(), wsf::six_dof::RigidBodyMover::InitializeDetails(), wsf::six_dof::RigidBodyIntegrator::PropagateRotation(), wsf::six_dof::FuelTank::UpdateFuelBurn(), wsf::six_dof::FuelTank::UpdateFuelFill(), and wsf::six_dof::FuelTank::UpdateFuelTransfer().

cREFERENCE_GRAV_ACCEL_MPS2

double wsf::six_dof::utils::cREFERENCE_GRAV_ACCEL_MPS2 = 9.80665

staticconstexpr

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration(), wsf::six_dof::PilotObject::FlyRates(), and wsf::six_dof::PointMassIntegrator::PropagateUsingAcceleration().