JSBSim::FGAuxiliary Class Reference

Encapsulates various uncategorized scheduled functions. More...

#include <FGAuxiliary.h>

Inherits JSBSim::FGModel.

Classes
struct	Inputs

Public Member Functions
	FGAuxiliary (FGFDMExec *Executive)
	Constructor.
	~FGAuxiliary ()
	Destructor.
bool	InitModel (void) override
bool	Run (bool Holding) override
	Runs the Auxiliary routines; called by the Executive Can pass in a value indicating if the executive is directing the simulation to Hold.
double	GetVcalibratedFPS (void) const
	Returns Calibrated airspeed in feet/second.
double	GetVcalibratedKTS (void) const
	Returns Calibrated airspeed in knots.
double	GetVequivalentFPS (void) const
	Returns equivalent airspeed in feet/second.
double	GetVequivalentKTS (void) const
	Returns equivalent airspeed in knots.
double	GetVtrueFPS () const
	Returns the true airspeed in feet per second.
double	GetVtrueKTS () const
	Returns the true airspeed in knots.
double	GetTotalPressure (void) const
	Returns the total pressure.
double	GetTotalTemperature (void) const
	Returns the total temperature.
double	GetTAT_C (void) const
double	GetPilotAccel (int idx) const
double	GetNpilot (int idx) const
double	GetAeroPQR (int axis) const
double	GetEulerRates (int axis) const
const FGColumnVector3 &	GetPilotAccel (void) const
const FGColumnVector3 &	GetNpilot (void) const
const FGColumnVector3 &	GetNcg (void) const
double	GetNcg (int idx) const
double	GetNlf (void) const
const FGColumnVector3 &	GetAeroPQR (void) const
const FGColumnVector3 &	GetEulerRates (void) const
const FGColumnVector3 &	GetAeroUVW (void) const
const FGLocation &	GetLocationVRP (void) const
double	GetAeroUVW (int idx) const
double	Getalpha (void) const
double	Getbeta (void) const
double	Getadot (void) const
double	Getbdot (void) const
double	GetMagBeta (void) const
double	Getalpha (int unit) const
double	Getbeta (int unit) const
double	Getadot (int unit) const
double	Getbdot (int unit) const
double	GetMagBeta (int unit) const
const FGMatrix33 &	GetTw2b (void) const
	Calculates and returns the wind-to-body axis transformation matrix.
const FGMatrix33 &	GetTb2w (void) const
	Calculates and returns the body-to-wind axis transformation matrix.
double	Getqbar (void) const
double	GetqbarUW (void) const
double	GetqbarUV (void) const
double	GetReynoldsNumber (void) const
double	GetVt (void) const
	Gets the magnitude of total vehicle velocity including wind effects in feet per second.
double	GetVground (void) const
	Gets the ground speed in feet per second.
double	GetMach (void) const
	Gets the Mach number.
double	GetMachU (void) const
	The mach number calculated using the vehicle X axis velocity.
double	GetNx (void) const
	The longitudinal acceleration in g's of the aircraft center of gravity.
double	GetNy (void) const
	The lateral acceleration in g's of the aircraft center of gravity.
double	GetNz (void) const
	The vertical acceleration in g's of the aircraft center of gravity.
const FGColumnVector3 &	GetNwcg (void) const
double	GetHOverBCG (void) const
double	GetHOverBMAC (void) const
double	GetGamma (void) const
double	GetGroundTrack (void) const
double	GetGamma (int unit) const
void	SetDayOfYear (int doy)
void	SetSecondsInDay (double sid)
int	GetDayOfYear (void) const
double	GetSecondsInDay (void) const
double	GetLongitudeRelativePosition (void) const
double	GetLatitudeRelativePosition (void) const
double	GetDistanceRelativePosition (void) const
void	SetAeroPQR (const FGColumnVector3 &tt)
Public Member Functions inherited from JSBSim::FGModel
	FGModel (FGFDMExec *)
	Constructor.
	~FGModel () override
	Destructor.
bool	InitModel (void) override
void	SetRate (unsigned int tt)
	Set the ouput rate for the model in frames.
unsigned int	GetRate (void)
	Get the output rate for the model in frames.
FGFDMExec *	GetExec (void)
void	SetPropertyManager (FGPropertyManager *fgpm)
virtual SGPath	FindFullPathName (const SGPath &path) const
const std::string &	GetName (void)
virtual bool	Load (Element *el)
Public Member Functions inherited from JSBSim::FGModelFunctions
virtual	~FGModelFunctions ()
void	RunPreFunctions (void)
void	RunPostFunctions (void)
bool	Load (Element *el, FGFDMExec *fdmex, std::string prefix="")
void	PreLoad (Element *el, FGFDMExec *fdmex, std::string prefix="")
void	PostLoad (Element *el, FGFDMExec *fdmex, std::string prefix="")
std::string	GetFunctionStrings (const std::string &delimeter) const
	Gets the strings for the current set of functions.
std::string	GetFunctionValues (const std::string &delimeter) const
	Gets the function values.
FGFunction *	GetPreFunction (const std::string &name)
	Get one of the "pre" function.
Public Member Functions inherited from JSBSim::FGJSBBase
	FGJSBBase ()
	Constructor for FGJSBBase.
virtual	~FGJSBBase ()
	Destructor for FGJSBBase.
void	PutMessage (const Message &msg)
	Places a Message structure on the Message queue.
void	PutMessage (const std::string &text)
	Creates a message with the given text and places it on the queue.
void	PutMessage (const std::string &text, bool bVal)
	Creates a message with the given text and boolean value and places it on the queue.
void	PutMessage (const std::string &text, int iVal)
	Creates a message with the given text and integer value and places it on the queue.
void	PutMessage (const std::string &text, double dVal)
	Creates a message with the given text and double value and places it on the queue.
int	SomeMessages (void) const
	Reads the message on the queue (but does not delete it).
void	ProcessMessage (void)
	Reads the message on the queue and removes it from the queue.
Message *	ProcessNextMessage (void)
	Reads the next message on the queue and removes it from the queue.
void	disableHighLighting (void)
	Disables highlighting in the console output.

Public Attributes
struct JSBSim::FGAuxiliary::Inputs	in

Additional Inherited Members
Public Types inherited from JSBSim::FGJSBBase
enum	{ eL = 1 , eM , eN }
	Moments L, M, N. More...
enum	{ eP = 1 , eQ , eR }
	Rates P, Q, R. More...
enum	{ eU = 1 , eV , eW }
	Velocities U, V, W. More...
enum	{ eX = 1 , eY , eZ }
	Positions X, Y, Z. More...
enum	{ ePhi = 1 , eTht , ePsi }
	Euler angles Phi, Theta, Psi. More...
enum	{ eDrag = 1 , eSide , eLift }
	Stability axis forces, Drag, Side force, Lift. More...
enum	{ eRoll = 1 , ePitch , eYaw }
	Local frame orientation Roll, Pitch, Yaw. More...
enum	{ eNorth = 1 , eEast , eDown }
	Local frame position North, East, Down. More...
enum	{ eLat = 1 , eLong , eRad }
	Locations Radius, Latitude, Longitude. More...
enum	{   inNone = 0 , inDegrees , inRadians , inMeters ,   inFeet }
	Conversion specifiers. More...
static const std::string &	GetVersion (void)
	Returns the version number of JSBSim.
static constexpr double	KelvinToFahrenheit (double kelvin)
	Converts from degrees Kelvin to degrees Fahrenheit.
static constexpr double	CelsiusToRankine (double celsius)
	Converts from degrees Celsius to degrees Rankine.
static constexpr double	RankineToCelsius (double rankine)
	Converts from degrees Rankine to degrees Celsius.
static constexpr double	KelvinToRankine (double kelvin)
	Converts from degrees Kelvin to degrees Rankine.
static constexpr double	RankineToKelvin (double rankine)
	Converts from degrees Rankine to degrees Kelvin.
static constexpr double	FahrenheitToCelsius (double fahrenheit)
	Converts from degrees Fahrenheit to degrees Celsius.
static constexpr double	CelsiusToFahrenheit (double celsius)
	Converts from degrees Celsius to degrees Fahrenheit.
static constexpr double	CelsiusToKelvin (double celsius)
	Converts from degrees Celsius to degrees Kelvin.
static constexpr double	KelvinToCelsius (double kelvin)
	Converts from degrees Kelvin to degrees Celsius.
static constexpr double	FeetToMeters (double measure)
	Converts from feet to meters.
static double	PitotTotalPressure (double mach, double p)
	Compute the total pressure in front of the Pitot tube.
static double	MachFromImpactPressure (double qc, double p)
	Compute the Mach number from the differential pressure (qc) and the static pressure.
static double	VcalibratedFromMach (double mach, double p)
	Calculate the calibrated airspeed from the Mach number.
static double	MachFromVcalibrated (double vcas, double p)
	Calculate the Mach number from the calibrated airspeed.Based on the formulas in the US Air Force Aircraft Performance Flight Testing Manual (AFFTC-TIH-99-01).
static bool	EqualToRoundoff (double a, double b)
	Finite precision comparison.
static bool	EqualToRoundoff (float a, float b)
	Finite precision comparison.
static bool	EqualToRoundoff (float a, double b)
	Finite precision comparison.
static bool	EqualToRoundoff (double a, float b)
	Finite precision comparison.
static constexpr double	Constrain (double min, double value, double max)
	Constrain a value between a minimum and a maximum value.
static constexpr double	sign (double num)
static double	GaussianRandomNumber (void)
Static Public Attributes inherited from JSBSim::FGJSBBase
static char	highint [5] = {27, '[', '1', 'm', '\0' }
	highlights text
static char	halfint [5] = {27, '[', '2', 'm', '\0' }
	low intensity text
static char	normint [6] = {27, '[', '2', '2', 'm', '\0' }
	normal intensity text
static char	reset [5] = {27, '[', '0', 'm', '\0' }
	resets text properties
static char	underon [5] = {27, '[', '4', 'm', '\0' }
	underlines text
static char	underoff [6] = {27, '[', '2', '4', 'm', '\0' }
	underline off
static char	fgblue [6] = {27, '[', '3', '4', 'm', '\0' }
	blue text
static char	fgcyan [6] = {27, '[', '3', '6', 'm', '\0' }
	cyan text
static char	fgred [6] = {27, '[', '3', '1', 'm', '\0' }
	red text
static char	fggreen [6] = {27, '[', '3', '2', 'm', '\0' }
	green text
static char	fgdef [6] = {27, '[', '3', '9', 'm', '\0' }
	default text
static short	debug_lvl = 1
Protected Member Functions inherited from JSBSim::FGModel
bool	Upload (Element *el, bool preLoad)
	Uploads this model in memory.
static std::string	CreateIndexedPropertyName (const std::string &Property, int index)
Protected Attributes inherited from JSBSim::FGModel
unsigned int	exe_ctr
unsigned int	rate
std::string	Name
FGFDMExec *	FDMExec
FGPropertyManager *	PropertyManager
Protected Attributes inherited from JSBSim::FGModelFunctions
std::vector< FGFunction * >	PreFunctions
std::vector< FGFunction * >	PostFunctions
FGPropertyReader	LocalProperties
static Message	localMsg
static std::queue< Message >	Messages
static unsigned int	messageId = 0
static constexpr double	radtodeg = 180. / 3.14159265358979323846
static constexpr double	degtorad = 3.14159265358979323846 / 180.
static constexpr double	hptoftlbssec = 550.0
static constexpr double	psftoinhg = 0.014138
static constexpr double	psftopa = 47.88
static constexpr double	ktstofps = 1.68781
static constexpr double	fpstokts = 1.0 / ktstofps
static constexpr double	inchtoft = 1.0/12.0
static constexpr double	fttom = 0.3048
static constexpr double	m3toft3 = 1.0/(fttom*fttom*fttom)
static constexpr double	in3tom3 = inchtoft*inchtoft*inchtoft/m3toft3
static constexpr double	inhgtopa = 3386.38
static constexpr double	slugtolb = 32.174049
	Note that definition of lbtoslug by the inverse of slugtolb and not to a different constant you can also get from some tables will make lbtoslug*slugtolb == 1 up to the magnitude of roundoff.
static constexpr double	lbtoslug = 1.0/slugtolb
static constexpr double	kgtolb = 2.20462
static constexpr double	kgtoslug = 0.06852168
static const std::string	needed_cfg_version = "2.0"
static const std::string	JSBSim_version = JSBSIM_VERSION " " __DATE__ " " __TIME__
static int	gaussian_random_number_phase = 0

Detailed Description

Encapsulates various uncategorized scheduled functions.

Pilot sensed accelerations are calculated here. This is used for the coordinated turn ball instrument. Motion base platforms sometimes use the derivative of pilot sensed accelerations as the driving parameter, rather than straight accelerations.

The theory behind pilot-sensed calculations is presented:

For purposes of discussion and calculation, assume for a minute that the pilot is in space and motionless in inertial space. She will feel no accelerations. If the aircraft begins to accelerate along any axis or axes (without rotating), the pilot will sense those accelerations. If any rotational moment is applied, the pilot will sense an acceleration due to that motion in the amount:

[wdot X R] + [w X (w X R)] Term I Term II

where:

wdot = omegadot, the rotational acceleration rate vector w = omega, the rotational rate vector R = the vector from the aircraft CG to the pilot eyepoint

The sum total of these two terms plus the acceleration of the aircraft body axis gives the acceleration the pilot senses in inertial space. In the presence of a large body such as a planet, a gravity field also provides an accelerating attraction. This acceleration can be transformed from the reference frame of the planet so as to be expressed in the frame of reference of the aircraft. This gravity field accelerating attraction is felt by the pilot as a force on her tushie as she sits in her aircraft on the runway awaiting takeoff clearance.

In JSBSim the acceleration of the body frame in inertial space is given by the F = ma relation. If the vForces vector is divided by the aircraft mass, the acceleration vector is calculated. The term wdot is equivalent to the JSBSim vPQRdot vector, and the w parameter is equivalent to vPQR.

Author

Tony Peden, Jon Berndt

Definition at line 100 of file FGAuxiliary.h.

Constructor & Destructor Documentation

FGAuxiliary()

JSBSim::FGAuxiliary::FGAuxiliary ( FGFDMExec * Executive )

explicit

Constructor.

Parameters

Executive

a pointer to the parent executive object

Definition at line 60 of file FGAuxiliary.cpp.

~FGAuxiliary()

JSBSim::FGAuxiliary::~FGAuxiliary

(

)

Destructor.

Definition at line 127 of file FGAuxiliary.cpp.

Member Function Documentation

Getadot() [1/2]

double JSBSim::FGAuxiliary::Getadot ( int unit ) const

inline

Definition at line 180 of file FGAuxiliary.h.

Getadot() [2/2]

double JSBSim::FGAuxiliary::Getadot ( void ) const

inline

Definition at line 172 of file FGAuxiliary.h.

GetAeroPQR() [1/2]

double JSBSim::FGAuxiliary::GetAeroPQR ( int axis ) const

inline

Definition at line 156 of file FGAuxiliary.h.

GetAeroPQR() [2/2]

const FGColumnVector3 & JSBSim::FGAuxiliary::GetAeroPQR ( void ) const

inline

Definition at line 164 of file FGAuxiliary.h.

GetAeroUVW() [1/2]

double JSBSim::FGAuxiliary::GetAeroUVW ( int idx ) const

inline

Definition at line 169 of file FGAuxiliary.h.

GetAeroUVW() [2/2]

const FGColumnVector3 & JSBSim::FGAuxiliary::GetAeroUVW ( void ) const

inline

Definition at line 166 of file FGAuxiliary.h.

Getalpha() [1/2]

double JSBSim::FGAuxiliary::Getalpha ( int unit ) const

inline

Definition at line 176 of file FGAuxiliary.h.

Getalpha() [2/2]

double JSBSim::FGAuxiliary::Getalpha ( void ) const

inline

Definition at line 170 of file FGAuxiliary.h.

Getbdot() [1/2]

double JSBSim::FGAuxiliary::Getbdot ( int unit ) const

inline

Definition at line 182 of file FGAuxiliary.h.

Getbdot() [2/2]

double JSBSim::FGAuxiliary::Getbdot ( void ) const

inline

Definition at line 173 of file FGAuxiliary.h.

Getbeta() [1/2]

double JSBSim::FGAuxiliary::Getbeta ( int unit ) const

inline

Definition at line 178 of file FGAuxiliary.h.

Getbeta() [2/2]

double JSBSim::FGAuxiliary::Getbeta ( void ) const

inline

Definition at line 171 of file FGAuxiliary.h.

GetDayOfYear()

int JSBSim::FGAuxiliary::GetDayOfYear ( void ) const

inline

Definition at line 245 of file FGAuxiliary.h.

GetDistanceRelativePosition()

double JSBSim::FGAuxiliary::GetDistanceRelativePosition

(

void

)

const

Definition at line 297 of file FGAuxiliary.cpp.

GetEulerRates() [1/2]

double JSBSim::FGAuxiliary::GetEulerRates ( int axis ) const

inline

Definition at line 157 of file FGAuxiliary.h.

GetEulerRates() [2/2]

const FGColumnVector3 & JSBSim::FGAuxiliary::GetEulerRates ( void ) const

inline

Definition at line 165 of file FGAuxiliary.h.

GetGamma() [1/2]

double JSBSim::FGAuxiliary::GetGamma ( int unit ) const

inline

Definition at line 235 of file FGAuxiliary.h.

GetGamma() [2/2]

double JSBSim::FGAuxiliary::GetGamma ( void ) const

inline

Definition at line 232 of file FGAuxiliary.h.

GetGroundTrack()

double JSBSim::FGAuxiliary::GetGroundTrack ( void ) const

inline

Definition at line 233 of file FGAuxiliary.h.

GetHOverBCG()

double JSBSim::FGAuxiliary::GetHOverBCG ( void ) const

inline

Definition at line 229 of file FGAuxiliary.h.

GetHOverBMAC()

double JSBSim::FGAuxiliary::GetHOverBMAC ( void ) const

inline

Definition at line 230 of file FGAuxiliary.h.

GetLatitudeRelativePosition()

double JSBSim::FGAuxiliary::GetLatitudeRelativePosition

(

void

)

const

Definition at line 289 of file FGAuxiliary.cpp.

GetLocationVRP()

const FGLocation & JSBSim::FGAuxiliary::GetLocationVRP ( void ) const

inline

Definition at line 167 of file FGAuxiliary.h.

GetLongitudeRelativePosition()

double JSBSim::FGAuxiliary::GetLongitudeRelativePosition

(

void

)

const

Definition at line 281 of file FGAuxiliary.cpp.

GetMach()

double JSBSim::FGAuxiliary::GetMach ( void ) const

inline

Gets the Mach number.

Definition at line 213 of file FGAuxiliary.h.

GetMachU()

double JSBSim::FGAuxiliary::GetMachU ( void ) const

inline

The mach number calculated using the vehicle X axis velocity.

Definition at line 216 of file FGAuxiliary.h.

GetMagBeta() [1/2]

double JSBSim::FGAuxiliary::GetMagBeta ( int unit ) const

inline

Definition at line 184 of file FGAuxiliary.h.

GetMagBeta() [2/2]

double JSBSim::FGAuxiliary::GetMagBeta ( void ) const

inline

Definition at line 174 of file FGAuxiliary.h.

GetNcg() [1/2]

double JSBSim::FGAuxiliary::GetNcg ( int idx ) const

inline

Definition at line 162 of file FGAuxiliary.h.

GetNcg() [2/2]

const FGColumnVector3 & JSBSim::FGAuxiliary::GetNcg ( void ) const

inline

Definition at line 161 of file FGAuxiliary.h.

GetNlf()

double JSBSim::FGAuxiliary::GetNlf

(

void

)

const

Definition at line 271 of file FGAuxiliary.cpp.

GetNpilot() [1/2]

double JSBSim::FGAuxiliary::GetNpilot ( int idx ) const

inline

Definition at line 155 of file FGAuxiliary.h.

GetNpilot() [2/2]

const FGColumnVector3 & JSBSim::FGAuxiliary::GetNpilot ( void ) const

inline

Definition at line 160 of file FGAuxiliary.h.

GetNwcg()

const FGColumnVector3 & JSBSim::FGAuxiliary::GetNwcg ( void ) const

inline

Definition at line 227 of file FGAuxiliary.h.

GetNx()

double JSBSim::FGAuxiliary::GetNx ( void ) const

inline

The longitudinal acceleration in g's of the aircraft center of gravity.

Definition at line 219 of file FGAuxiliary.h.

GetNy()

double JSBSim::FGAuxiliary::GetNy ( void ) const

inline

The lateral acceleration in g's of the aircraft center of gravity.

Definition at line 222 of file FGAuxiliary.h.

GetNz()

double JSBSim::FGAuxiliary::GetNz ( void ) const

inline

The vertical acceleration in g's of the aircraft center of gravity.

Definition at line 225 of file FGAuxiliary.h.

GetPilotAccel() [1/2]

double JSBSim::FGAuxiliary::GetPilotAccel ( int idx ) const

inline

Definition at line 154 of file FGAuxiliary.h.

GetPilotAccel() [2/2]

const FGColumnVector3 & JSBSim::FGAuxiliary::GetPilotAccel ( void ) const

inline

Definition at line 159 of file FGAuxiliary.h.

Getqbar()

double JSBSim::FGAuxiliary::Getqbar ( void ) const

inline

Definition at line 197 of file FGAuxiliary.h.

GetqbarUV()

double JSBSim::FGAuxiliary::GetqbarUV ( void ) const

inline

Definition at line 199 of file FGAuxiliary.h.

GetqbarUW()

double JSBSim::FGAuxiliary::GetqbarUW ( void ) const

inline

Definition at line 198 of file FGAuxiliary.h.

GetReynoldsNumber()

double JSBSim::FGAuxiliary::GetReynoldsNumber ( void ) const

inline

Definition at line 200 of file FGAuxiliary.h.

GetSecondsInDay()

double JSBSim::FGAuxiliary::GetSecondsInDay ( void ) const

inline

Definition at line 246 of file FGAuxiliary.h.

GetTAT_C()

double JSBSim::FGAuxiliary::GetTAT_C ( void ) const

inline

Definition at line 152 of file FGAuxiliary.h.

GetTb2w()

const FGMatrix33 & JSBSim::FGAuxiliary::GetTb2w ( void ) const

inline

Calculates and returns the body-to-wind axis transformation matrix.

Returns

a reference to the wind-to-body transformation matrix.

Definition at line 195 of file FGAuxiliary.h.

GetTotalPressure()

double JSBSim::FGAuxiliary::GetTotalPressure ( void ) const

inline

Returns the total pressure.

Total pressure is freestream total pressure for subsonic only. For supersonic it is the 1D total pressure behind a normal shock.

Definition at line 141 of file FGAuxiliary.h.

GetTotalTemperature()

double JSBSim::FGAuxiliary::GetTotalTemperature ( void ) const

inline

Returns the total temperature.

The total temperature ("tat", isentropic flow) is calculated:

tat = in.Temperature*(1 + 0.2*Mach*Mach)

(where "in.Temperature" is standard temperature calculated by the atmosphere model)

Definition at line 151 of file FGAuxiliary.h.

GetTw2b()

const FGMatrix33 & JSBSim::FGAuxiliary::GetTw2b ( void ) const

inline

Calculates and returns the wind-to-body axis transformation matrix.

Returns

a reference to the wind-to-body transformation matrix.

Definition at line 190 of file FGAuxiliary.h.

GetVcalibratedFPS()

double JSBSim::FGAuxiliary::GetVcalibratedFPS ( void ) const

inline

Returns Calibrated airspeed in feet/second.

Definition at line 125 of file FGAuxiliary.h.

GetVcalibratedKTS()

double JSBSim::FGAuxiliary::GetVcalibratedKTS ( void ) const

inline

Returns Calibrated airspeed in knots.

Definition at line 127 of file FGAuxiliary.h.

GetVequivalentFPS()

double JSBSim::FGAuxiliary::GetVequivalentFPS ( void ) const

inline

Returns equivalent airspeed in feet/second.

Definition at line 129 of file FGAuxiliary.h.

GetVequivalentKTS()

double JSBSim::FGAuxiliary::GetVequivalentKTS ( void ) const

inline

Returns equivalent airspeed in knots.

Definition at line 131 of file FGAuxiliary.h.

GetVground()

double JSBSim::FGAuxiliary::GetVground ( void ) const

inline

Gets the ground speed in feet per second.

The magnitude is the square root of the sum of the squares (RSS) of the vehicle north and east velocity components.

Returns

The magnitude of the vehicle velocity in the horizontal plane.

Definition at line 210 of file FGAuxiliary.h.

GetVt()

double JSBSim::FGAuxiliary::GetVt ( void ) const

inline

Gets the magnitude of total vehicle velocity including wind effects in feet per second.

Definition at line 204 of file FGAuxiliary.h.

GetVtrueFPS()

double JSBSim::FGAuxiliary::GetVtrueFPS ( ) const

inline

Returns the true airspeed in feet per second.

Definition at line 133 of file FGAuxiliary.h.

GetVtrueKTS()

double JSBSim::FGAuxiliary::GetVtrueKTS ( ) const

inline

Returns the true airspeed in knots.

Definition at line 135 of file FGAuxiliary.h.

InitModel()

bool JSBSim::FGAuxiliary::InitModel ( void )

overridevirtual

Reimplemented from JSBSim::FGModelFunctions.

Definition at line 94 of file FGAuxiliary.cpp.

Run()

bool JSBSim::FGAuxiliary::Run ( bool Holding )

overridevirtual

Runs the Auxiliary routines; called by the Executive Can pass in a value indicating if the executive is directing the simulation to Hold.

Parameters

Holding

if true, the executive has been directed to hold the sim from advancing time. Some models may ignore this flag, such as the Input model, which may need to be active to listen on a socket for the "Resume" command to be given.

Returns

false if no error

Reimplemented from JSBSim::FGModel.

Definition at line 134 of file FGAuxiliary.cpp.

SetAeroPQR()

void JSBSim::FGAuxiliary::SetAeroPQR ( const FGColumnVector3 & tt )

inline

Definition at line 252 of file FGAuxiliary.h.

SetDayOfYear()

void JSBSim::FGAuxiliary::SetDayOfYear ( int doy )

inline

Definition at line 242 of file FGAuxiliary.h.

SetSecondsInDay()

void JSBSim::FGAuxiliary::SetSecondsInDay ( double sid )

inline

Definition at line 243 of file FGAuxiliary.h.

Member Data Documentation

in

struct JSBSim::FGAuxiliary::Inputs JSBSim::FGAuxiliary::in

---

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

• FGAuxiliary.h
• FGAuxiliary.cpp