class DtAirspeedCalculator:

DtAirspeedCalculator provides an interface for calculating true air speed, indicated air speed and mach.

Public Member Functions
	DtAirspeedCalculator ()

	DtAirspeedCalculator (const DtAirspeedCalculator &orig)

virtual	~DtAirspeedCalculator ()

const DtAirspeedCalculator &	operator= (const DtAirspeedCalculator &orig)

virtual void	convertSpeedtoAllAirSpeeds (const DtSimObject *stateRep, double &groundSpeed, double &trueAirSpeed, double &indicatedAirSpeed, double &machSpeed, double currentAlt, DtAirSpeedType currentSpeedType)

virtual double	tasFromGroundSpeed (const double groundSpeed, const double heading, const double windSpeed, const double windDirection) const

virtual double	iasFromTas (const double trueAirspeed, const double altitude) const

virtual double	machFromTas (const double trueAirspeed, const double temperature, const double pressure) const

virtual double	machFromTas (const double trueAirspeed, const double temperature, const double pressure, const double altitude) const

virtual double	groundSpeedFromTas (const double tas, const double heading, const double windSpeed, const double windDirection) const

virtual double	tasFromIas (const double indicatedAirspeed, const double altitude) const

virtual double	tasFromMach (const double trueAirspeed, const double temperature, const double pressure) const

virtual double	tasFromMach (const double trueAirspeed, const double temperature, const double pressure, const double altitude) const

Static Public Member Functions
static DtAirspeedCalculator *	creator ()

Constructor & Destructor Documentation

DtAirspeedCalculator::DtAirspeedCalculator ( )

Default constructor; assumes a maximum population of 100 samples.

DtAirspeedCalculator::DtAirspeedCalculator ( const DtAirspeedCalculator & orig )

copy constructor

virtual DtAirspeedCalculator::~DtAirspeedCalculator ( )

virtual

destructor

Member Function Documentation

static DtAirspeedCalculator* DtAirspeedCalculator::creator ( )

static

const DtAirspeedCalculator& DtAirspeedCalculator::operator= ( const DtAirspeedCalculator & orig )

assignment operator

virtual void DtAirspeedCalculator::convertSpeedtoAllAirSpeeds	(	const DtSimObject *	stateRep,
		double &	groundSpeed,
		double &	trueAirSpeed,
		double &	indicatedAirSpeed,
		double &	machSpeed,
		double	currentAlt,
		DtAirSpeedType	currentSpeedType
	)

virtual

Convert a speed with an Air Type into all air Speed types taking into account entity location and environment state at that location.

virtual double DtAirspeedCalculator::tasFromGroundSpeed	(	const double	groundSpeed,
		const double	heading,
		const double	windSpeed,
		const double	windDirection
	)		const

virtual

true air speed from ground speed in meters per second groundSpeed and windSpeed is meters per second heading and windDirection are radians

Parameters

heading	forward component only
windSpeed	dir entity is facing

virtual double DtAirspeedCalculator::iasFromTas	(	const double	trueAirspeed,
		const double	altitude
	)		const

virtual

indicated air speed from true air speed in meters per second This implementation uses the 2% loss per 305m of altitude rule of thumb. trueAirSpeed is meters per second altitude is meters

virtual double DtAirspeedCalculator::machFromTas	(	const double	trueAirspeed,
		const double	temperature,
		const double	pressure
	)		const

virtual

mach from true air speed trueAirspeed is meters per second temperature is in Celcius pressure is in kPa

virtual double DtAirspeedCalculator::machFromTas	(	const double	trueAirspeed,
		const double	temperature,
		const double	pressure,
		const double	altitude
	)		const

virtual

virtual double DtAirspeedCalculator::groundSpeedFromTas	(	const double	tas,
		const double	heading,
		const double	windSpeed,
		const double	windDirection
	)		const

virtual

ground speed from true air speed in meters per second groundSpeed and windSpeed is meters per second heading and windDirection are radians

Parameters

heading	forward component only
windSpeed	dir entity is facing

virtual double DtAirspeedCalculator::tasFromIas	(	const double	indicatedAirspeed,
		const double	altitude
	)		const

virtual

true air speed from indicated air speed in meters per second This implementation uses the 2% loss per 305m of altitude rule of thumb. indicatedAirspeed is meters per second altitude is meters

virtual double DtAirspeedCalculator::tasFromMach	(	const double	trueAirspeed,
		const double	temperature,
		const double	pressure
	)		const

virtual

true air speed from mach trueAirspeed is meters per second temperature is in Celcius pressure is in kPa

virtual double DtAirspeedCalculator::tasFromMach	(	const double	trueAirspeed,
		const double	temperature,
		const double	pressure,
		const double	altitude
	)		const

virtual

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

/data/exports/nrhent7-1/nightly/docs/vrForces.vrf5-0-branch/include/vrfmodel/airSpeedCalculator.h

Public Member Functions

Static Public Member Functions

Constructor & Destructor Documentation

Member Function Documentation