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P6DofAtmosphere Class Reference

P6DofAtmosphere provides atmospheric data for Pseudo 6DOF objects. More...

#include <P6DofAtmosphere.hpp>

Public Member Functions

 P6DofAtmosphere ()
 P6DofAtmosphere (const std::string &aFilename)
P6DofAtmosphere & operator= (const P6DofAtmosphere &other)=delete
P6DofAtmosphere * Clone () const
 ~P6DofAtmosphere ()=default
double SpeedOfSoundAtAltitude_fps (double aAltitude_ft) const
double AirDensityAtAltitude (double aAltitude_ft) const
double StaticPressureAtAltitude (double aAltitude_ft) const
double TemperatureAtAltitude_F (double aAltitude_ft) const
double TemperatureAtAltitude_R (double aAltitude_ft) const
double CalcMachAtAltitude (double aAltitude_ft, double aSpeed_fps) const
double DensityRatioAtAltitude (double aAltitude_ft) const
double StaticPressureRatioAtAltitude (double aAltitude_ft) const
double TemperatureRatioAtAltitude (double aAltitude_ft) const
void GetAeroParametersAtAltitude (double aAltitude_ft, double aSpeed_fps, double &aAirDensity, double &aDynamicPressure_psf, double &aStaticPressure_psf, double &aMach) const
double CalcKtasFromKcas (double aAltitude_ft, double aSpeed_kcas) const
double CalcKtasFromMach (double aAltitude_ft, double aSpeed_mach) const
double CalcKtasFromFps (double aSpeed_fps) const
double CalcKcasFromKtas (double aAltitude_ft, double aSpeed_ktas) const
double CalcKcasFromMach (double aAltitude_ft, double aSpeed_mach) const
double CalcKcasFromFps (double aAltitude_ft, double aSpeed_fps) const
double CalcMachFromKcas (double aAltitude_ft, double aSpeed_kcas) const
double CalcMachFromKtas (double aAltitude_ft, double aSpeed_ktas) const
double CalcMachFromFps (double aAltitude_ft, double aSpeed_fps) const
double CalcFpsFromKcas (double aAltitude_ft, double aSpeed_kcas) const
double CalcFpsFromKtas (double aSpeed_ktas) const
double CalcFpsFromMach (double aAltitude_ft, double aSpeed_mach) const
double CalcDynamicPressure_lbft2 (double aAltitude_ft, double aSpeed_fps) const
double CalcFpsFromAltitudeDynamicPressure (double aAltitude_ft, double aPressure_lbft2) const
bool ContrailAltitudeBand_ft (double &aLowAltitude_ft, double &aHighAltitude_ft) const
bool WithinContrailAltitudeBand (double aAltitude_ft) const
bool ProcessInput (UtInput &aInput)

Detailed Description

P6DofAtmosphere provides atmospheric data for Pseudo 6DOF objects.

Constructor & Destructor Documentation

◆ P6DofAtmosphere() [1/2]

P6DofAtmosphere::P6DofAtmosphere ( )

Referenced by Clone(), operator=(), and ~P6DofAtmosphere().

◆ P6DofAtmosphere() [2/2]

P6DofAtmosphere::P6DofAtmosphere ( const std::string & aFilename)
explicit

References ProcessInput().

◆ ~P6DofAtmosphere()

P6DofAtmosphere::~P6DofAtmosphere ( )
default

References AirDensityAtAltitude(), CalcDynamicPressure_lbft2(), CalcFpsFromAltitudeDynamicPressure(), CalcFpsFromKcas(), CalcFpsFromKtas(), CalcFpsFromMach(), CalcKcasFromFps(), CalcKcasFromKtas(), CalcKcasFromMach(), CalcKtasFromFps(), CalcKtasFromKcas(), CalcKtasFromMach(), CalcMachAtAltitude(), CalcMachFromFps(), CalcMachFromKcas(), CalcMachFromKtas(), ContrailAltitudeBand_ft(), DensityRatioAtAltitude(), GetAeroParametersAtAltitude(), P6DofAtmosphere(), ProcessInput(), SpeedOfSoundAtAltitude_fps(), StaticPressureAtAltitude(), StaticPressureRatioAtAltitude(), TemperatureAtAltitude_F(), TemperatureAtAltitude_R(), TemperatureRatioAtAltitude(), and WithinContrailAltitudeBand().

Member Function Documentation

◆ AirDensityAtAltitude()

double P6DofAtmosphere::AirDensityAtAltitude ( double aAltitude_ft) const

Referenced by CalcDynamicPressure_lbft2(), CalcFpsFromAltitudeDynamicPressure(), CalcFpsFromKcas(), CalcKcasFromFps(), DensityRatioAtAltitude(), GetAeroParametersAtAltitude(), and ~P6DofAtmosphere().

◆ CalcDynamicPressure_lbft2()

double P6DofAtmosphere::CalcDynamicPressure_lbft2 ( double aAltitude_ft,
double aSpeed_fps ) const

References AirDensityAtAltitude().

Referenced by WsfP6DOF_MoverTestObject::AlphaAtDesiredDrag(), WsfP6DOF_MoverTestObject::AlphaAtDesiredDrag(), WsfP6DOF_MoverTestObject::CalcLevelFlightDragAndAlpha(), P6DofVehicle::CalculateCmAreaForCoreAndControls(), WsfP6DOF_MoverTestObject::FuelBurnAtRequiredThrust(), WsfP6DOF_MoverTestObject::FuelBurnAtThrottleSetting(), WsfP6DOF_MoverTestObject::GetPitchingMoment(), WsfP6DOF_MoverTestObject::MaxInstantaneousGLoad(), WsfP6DOF_MoverTestObject::ThrottleSettingToProduceThrust(), WsfP6DOF_MoverTestObject::ThrustAtThrottleSetting(), WsfP6DOF_MoverTestObject::TurnRateAt(), WsfP6DOF_MoverTestObject::TurnRateWithConditions(), UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcFpsFromAltitudeDynamicPressure()

double P6DofAtmosphere::CalcFpsFromAltitudeDynamicPressure ( double aAltitude_ft,
double aPressure_lbft2 ) const

References AirDensityAtAltitude().

Referenced by UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcFpsFromKcas()

double P6DofAtmosphere::CalcFpsFromKcas ( double aAltitude_ft,
double aSpeed_kcas ) const

References AirDensityAtAltitude().

Referenced by CalcKtasFromKcas(), CalcMachFromKcas(), P6DofPilotObject::SetPositionToPlannedWaypoint(), P6DofPilotObject::SetPositionToTempWaypoint(), UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcFpsFromKtas()

double P6DofAtmosphere::CalcFpsFromKtas ( double aSpeed_ktas) const

Referenced by CalcKcasFromKtas(), CalcMachFromKtas(), P6DofPilotObject::SetPositionToPlannedWaypoint(), P6DofPilotObject::SetPositionToTempWaypoint(), UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcFpsFromMach()

double P6DofAtmosphere::CalcFpsFromMach ( double aAltitude_ft,
double aSpeed_mach ) const

References SpeedOfSoundAtAltitude_fps().

Referenced by WsfP6DOF_MoverTestObject::AlphaAtDesiredDrag(), CalcKcasFromMach(), CalcKtasFromMach(), WsfP6DOF_MoverTestObject::CalcLevelFlightDragAndAlpha(), P6DofVehicle::CalculateCmAreaForCoreAndControls(), WsfP6DOF_MoverTestObject::FuelBurnAtRequiredThrust(), WsfP6DOF_MoverTestObject::FuelBurnAtThrottleSetting(), WsfP6DOF_MoverTestObject::GetPitchingMoment(), WsfP6DOF_MoverTestObject::MaxInstantaneousGLoad(), P6DofPilotObject::SetPositionToPlannedWaypoint(), P6DofPilotObject::SetPositionToTempWaypoint(), WsfP6DOF_MoverTestObject::ThrottleSettingToProduceThrust(), WsfP6DOF_MoverTestObject::ThrustAtThrottleSetting(), UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcKcasFromFps()

double P6DofAtmosphere::CalcKcasFromFps ( double aAltitude_ft,
double aSpeed_fps ) const

References AirDensityAtAltitude().

Referenced by CalcKcasFromKtas(), CalcKcasFromMach(), P6DofKinematicState::CalculateSecondaryParameters(), P6DofKinematicState::UpdateAeroState(), UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcKcasFromKtas()

double P6DofAtmosphere::CalcKcasFromKtas ( double aAltitude_ft,
double aSpeed_ktas ) const

References CalcFpsFromKtas(), and CalcKcasFromFps().

Referenced by UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcKcasFromMach()

double P6DofAtmosphere::CalcKcasFromMach ( double aAltitude_ft,
double aSpeed_mach ) const

References CalcFpsFromMach(), and CalcKcasFromFps().

Referenced by UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcKtasFromFps()

double P6DofAtmosphere::CalcKtasFromFps ( double aSpeed_fps) const

Referenced by CalcKtasFromKcas(), CalcKtasFromMach(), P6DofKinematicState::CalculateSecondaryParameters(), P6DofKinematicState::UpdateAeroState(), UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcKtasFromKcas()

double P6DofAtmosphere::CalcKtasFromKcas ( double aAltitude_ft,
double aSpeed_kcas ) const

References CalcFpsFromKcas(), and CalcKtasFromFps().

Referenced by UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcKtasFromMach()

double P6DofAtmosphere::CalcKtasFromMach ( double aAltitude_ft,
double aSpeed_mach ) const

References CalcFpsFromMach(), and CalcKtasFromFps().

Referenced by UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcMachAtAltitude()

double P6DofAtmosphere::CalcMachAtAltitude ( double aAltitude_ft,
double aSpeed_fps ) const

References SpeedOfSoundAtAltitude_fps().

Referenced by CalcMachFromFps(), GetAeroParametersAtAltitude(), and ~P6DofAtmosphere().

◆ CalcMachFromFps()

double P6DofAtmosphere::CalcMachFromFps ( double aAltitude_ft,
double aSpeed_fps ) const

References CalcMachAtAltitude().

Referenced by WsfP6DOF_MoverTestObject::AlphaAtDesiredDrag(), CalcMachFromKcas(), CalcMachFromKtas(), WsfP6DOF_MoverTestObject::TurnRateAt(), WsfP6DOF_MoverTestObject::TurnRateWithConditions(), UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcMachFromKcas()

double P6DofAtmosphere::CalcMachFromKcas ( double aAltitude_ft,
double aSpeed_kcas ) const

References CalcFpsFromKcas(), and CalcMachFromFps().

Referenced by UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ CalcMachFromKtas()

double P6DofAtmosphere::CalcMachFromKtas ( double aAltitude_ft,
double aSpeed_ktas ) const

References CalcFpsFromKtas(), and CalcMachFromFps().

Referenced by UT_DEFINE_SCRIPT_METHOD(), and ~P6DofAtmosphere().

◆ Clone()

P6DofAtmosphere * P6DofAtmosphere::Clone ( ) const

References P6DofAtmosphere().

Referenced by operator=().

◆ ContrailAltitudeBand_ft()

bool P6DofAtmosphere::ContrailAltitudeBand_ft ( double & aLowAltitude_ft,
double & aHighAltitude_ft ) const

Referenced by ~P6DofAtmosphere().

◆ DensityRatioAtAltitude()

double P6DofAtmosphere::DensityRatioAtAltitude ( double aAltitude_ft) const

References AirDensityAtAltitude().

Referenced by ~P6DofAtmosphere().

◆ GetAeroParametersAtAltitude()

void P6DofAtmosphere::GetAeroParametersAtAltitude ( double aAltitude_ft,
double aSpeed_fps,
double & aAirDensity,
double & aDynamicPressure_psf,
double & aStaticPressure_psf,
double & aMach ) const

References AirDensityAtAltitude(), CalcMachAtAltitude(), and StaticPressureAtAltitude().

Referenced by P6DofKinematicState::CalculateSecondaryParameters(), WsfP6DOF_Mover::GetAeroParametersAtAltitude(), and ~P6DofAtmosphere().

◆ operator=()

P6DofAtmosphere & P6DofAtmosphere::operator= ( const P6DofAtmosphere & other)
delete

References Clone(), and P6DofAtmosphere().

◆ ProcessInput()

bool P6DofAtmosphere::ProcessInput ( UtInput & aInput)

Referenced by P6DofAtmosphere(), and ~P6DofAtmosphere().

◆ SpeedOfSoundAtAltitude_fps()

double P6DofAtmosphere::SpeedOfSoundAtAltitude_fps ( double aAltitude_ft) const

Referenced by CalcFpsFromMach(), CalcMachAtAltitude(), WsfP6DOF_Mover::GetAeroParametersAtAltitude(), WsfP6DOF_Mover::WriteKinematicStatus(), and ~P6DofAtmosphere().

◆ StaticPressureAtAltitude()

double P6DofAtmosphere::StaticPressureAtAltitude ( double aAltitude_ft) const

Referenced by WsfP6DOF_MoverTestObject::FuelBurnAtRequiredThrust(), WsfP6DOF_MoverTestObject::FuelBurnAtThrottleSetting(), GetAeroParametersAtAltitude(), StaticPressureRatioAtAltitude(), WsfP6DOF_MoverTestObject::ThrottleSettingToProduceThrust(), WsfP6DOF_MoverTestObject::ThrustAtThrottleSetting(), and ~P6DofAtmosphere().

◆ StaticPressureRatioAtAltitude()

double P6DofAtmosphere::StaticPressureRatioAtAltitude ( double aAltitude_ft) const

References StaticPressureAtAltitude().

Referenced by ~P6DofAtmosphere().

◆ TemperatureAtAltitude_F()

double P6DofAtmosphere::TemperatureAtAltitude_F ( double aAltitude_ft) const

References TemperatureAtAltitude_R().

Referenced by TemperatureRatioAtAltitude(), and ~P6DofAtmosphere().

◆ TemperatureAtAltitude_R()

double P6DofAtmosphere::TemperatureAtAltitude_R ( double aAltitude_ft) const

Referenced by TemperatureAtAltitude_F(), and ~P6DofAtmosphere().

◆ TemperatureRatioAtAltitude()

double P6DofAtmosphere::TemperatureRatioAtAltitude ( double aAltitude_ft) const

References TemperatureAtAltitude_F().

Referenced by ~P6DofAtmosphere().

◆ WithinContrailAltitudeBand()

bool P6DofAtmosphere::WithinContrailAltitudeBand ( double aAltitude_ft) const

Referenced by P6DofVehicle::WithinContrailAltitudeBand(), and ~P6DofAtmosphere().

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