FlightGear: JSBSim::FGGasCell Class Reference

Models a gas cell. More...

#include <FGGasCell.h>

Classes
struct	Inputs

Public Member Functions
	FGGasCell (FGFDMExec exec, Element el, unsigned int num, const struct Inputs &input)
	Constructor.

	~FGGasCell ()

void	Calculate (double dt)
	Runs the gas cell model; called by BuoyantForces.

int	GetIndex (void) const
	Get the index of this gas cell.

const FGColumnVector3 &	GetXYZ (void) const
	Get the center of gravity location of the gas cell (including any ballonets)

double	GetXYZ (int idx) const
	Get the center of gravity location of the gas cell (including any ballonets)

double	GetMass (void) const
	Get the current mass of the gas cell (including any ballonets)

const FGMatrix33 &	GetInertia (void) const
	Get the moments of inertia of the gas cell (including any ballonets)

const FGColumnVector3 &	GetMassMoment (void) const
	Get the moment due to mass of the gas cell (including any ballonets)

double	GetTemperature (void) const
	Get the current gas temperature inside the gas cell.

double	GetPressure (void) const
	Get the current gas pressure inside the gas cell.

Public Member Functions inherited from JSBSim::FGForce
	FGForce (FGFDMExec *FDMExec)
	Constructor.

	FGForce (const FGForce &force)

virtual	~FGForce ()
	Destructor.

virtual const FGColumnVector3 &	GetBodyForces (void)

double	GetBodyXForce (void) const

double	GetBodyYForce (void) const

double	GetBodyZForce (void) const

const FGColumnVector3 &	GetMoments (void) const

void	SetLocation (double x, double y, double z)

void	SetActingLocation (double x, double y, double z)
	Acting point of application.

void	SetLocationX (double x)

void	SetLocationY (double y)

void	SetLocationZ (double z)

double	SetActingLocationX (double x)

double	SetActingLocationY (double y)

double	SetActingLocationZ (double z)

void	SetLocation (const FGColumnVector3 &vv)

void	SetActingLocation (const FGColumnVector3 &vv)

double	GetLocationX (void) const

double	GetLocationY (void) const

double	GetLocationZ (void) const

double	GetActingLocationX (void) const

double	GetActingLocationY (void) const

double	GetActingLocationZ (void) const

const FGColumnVector3 &	GetLocation (void) const

const FGColumnVector3 &	GetActingLocation (void) const

void	SetAnglesToBody (double broll, double bpitch, double byaw)

void	SetAnglesToBody (const FGColumnVector3 &vv)

void	UpdateCustomTransformMatrix (void)

void	SetPitch (double pitch)

void	SetYaw (double yaw)

double	GetPitch (void) const

double	GetYaw (void) const

const FGColumnVector3 &	GetAnglesToBody (void) const

double	GetAnglesToBody (int axis) const

void	SetTransformType (TransformType ii)

TransformType	GetTransformType (void) const

const FGMatrix33 &	Transform (void) const

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
const struct Inputs &	in

Additional Inherited Members
Public Types inherited from JSBSim::FGForce
enum	TransformType { tNone , tWindBody , tLocalBody , tCustom }

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

static std::string	CreateIndexedPropertyName (const std::string &Property, int index)

Protected Attributes inherited from JSBSim::FGForce
FGFDMExec *	fdmex

FGMassBalance *	MassBalance

FGColumnVector3	vFn

FGColumnVector3	vMn

FGColumnVector3	vOrient

TransformType	ttype

FGColumnVector3	vXYZn

FGColumnVector3	vActingXYZn

FGMatrix33	mT

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/(fttomfttomfttom)

static constexpr double	in3tom3 = inchtoftinchtoftinchtoft/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

Models a gas cell.

Author: Anders Gidenstam

Configuration File Format:

<buoyant_forces>
  <gas_cell type="{HYDROGEN | HELIUM | AIR}">
    <location unit="{M | IN}">
      <x> {number} </x>
      <y> {number} </y>
      <z> {number} </z>
    </location>
    <x_width unit="{M | IN}"> {number} </x_width>
    <y_radius unit="{M | IN}"> {number} </y_radius>
    <z_radius unit="{M | IN}"> {number} </z_radius>
    <max_overpressure unit="{PA | PSI}"> {number} </max_overpressure>
    <valve_coefficient unit="{M4*SEC/KG | FT4*SEC/SLUG}"> {number} </valve_coefficient>
    <fullness> {number} </fullness>  
    <heat>
      {heat transfer coefficients} [lbs ft / sec]
    </heat>
    <ballonet>
      <location unit="{M | IN}">
        <x> {number} </x>
        <y> {number} </y>
        <z> {number} </z>
      </location>
      <x_width unit="{M | IN}"> {number} </x_width>
      <y_radius unit="{M | IN}"> {number} </y_radius>
      <z_radius unit="{M | IN}"> {number} </z_radius>
      <max_overpressure unit="{PA | PSI}"> {number} </max_overpressure>
      <valve_coefficient unit="{M4*SEC/KG | FT4*SEC/SLUG}"> {number} </valve_coefficient>
      <fullness> {number} </fullness>  
      <heat>
       {heat transfer coefficients} [lb ft / (sec Rankine)]
      </heat>
      <blower_input>
       {input air flow function} [ft^3 / sec]
      </blower_input>
    </ballonet>
  </gas_cell>
</buoyant_forces>

Definition of the gas cell configuration file parameters:

type - One of HYDROGEN, HELIUM or AIR.
location - Location of cell center in the aircraft's structural frame. Currently this is were the forces of the cell is applied.
{x|y|z}_radius - Radius along in the respective direction (both ends).
{x|y|z}_width - Width in the respective direction. NOTE: A 'x', 'y', 'z'-radius/width combination must be specified.
fullness - Initial fullness of the cell, normally [0,1], values >1 initialize the cell at pressure.
max_overpressure - Maximum cell overpressure (excess is automatically valved off).
valve_coefficient - Capacity of the manual valve. The valve is considered to be located at the top of the cell. The valve coefficient determine the flow out of the cell according to: dVolume/dt = ValveCoefficient * DeltaPressure.
heat - Zero or more FGFunction:s describing the heat flow from the atmosphere into the gas cell. Unit: [lb ft / (sec Rankine)]. If there are no heat transfer functions at all the gas cell temperature will equal that of the surrounding atmosphere. A constant function returning 0 results in adiabatic behaviour.
ballonet - Zero or more ballonets, i.e. air bags inside the gas cell. Ballonets are used to maintain the volume of the gas cell and keep its internal pressure higher than that of the surrounding environment.
- location - Location of ballonet center in the aircraft's structural frame.
- {x|y|z}_radius - Radius along in the respective direction (both ends).
- {x|y|z}_width - Width in the respective direction.
- max_overpressure - Maximum ballonet overpressure (excess is automatically valved off).
- valve_coefficient - Capacity of the exit valve between the ballonet and the atmosphere. The valve coefficient determine the flow out of the cell according to: dVolume/dt = ValveCoefficient * DeltaPressure.
- heat - Zero or more FGFunction:s describing the heat flow from the enclosing gas cell into the ballonet. Unit: [lb ft / (sec Rankine)]
- blower_input - One FGFunction describing the air flow into the ballonet. Unit: [ft³ / sec] (at the temperature and pressure of the ballonet.)

Definition at line 166 of file FGGasCell.h.

Constructor & Destructor Documentation

◆ FGGasCell()

JSBSim::FGGasCell::FGGasCell	(	FGFDMExec *	exec,
		Element *	el,
		unsigned int	num,
		const struct Inputs &	input )

Constructor.

Parameters

exec	Executive a pointer to the parent executive object
el	Pointer to configuration file XML node
num	Gas cell index number.

Definition at line 60 of file FGGasCell.cpp.

◆ ~FGGasCell()

JSBSim::FGGasCell::~FGGasCell ( )

Definition at line 240 of file FGGasCell.cpp.

Member Function Documentation

◆ Calculate()

void JSBSim::FGGasCell::Calculate ( double dt )

Runs the gas cell model; called by BuoyantForces.

Definition at line 255 of file FGGasCell.cpp.

◆ GetIndex()

int JSBSim::FGGasCell::GetIndex ( void ) const

inline

Get the index of this gas cell.

Returns: gas cell index.

Definition at line 190 of file FGGasCell.h.

◆ GetInertia()

const FGMatrix33 & JSBSim::FGGasCell::GetInertia ( void ) const

inline

Get the moments of inertia of the gas cell (including any ballonets)

Returns: moments of inertia matrix in the body frame in slug ft².

Definition at line 209 of file FGGasCell.h.

◆ GetMass()

double JSBSim::FGGasCell::GetMass ( void ) const

inline

Get the current mass of the gas cell (including any ballonets)

Returns: gas mass in slug.

Definition at line 204 of file FGGasCell.h.

◆ GetMassMoment()

const FGColumnVector3 & JSBSim::FGGasCell::GetMassMoment ( void ) const

inline

Get the moment due to mass of the gas cell (including any ballonets)

Note that the buoyancy of the gas cell is handled separately by the FGForce part and not included here.

Returns: moment vector in the structural frame in lbs in.

Definition at line 216 of file FGGasCell.h.

◆ GetPressure()

double JSBSim::FGGasCell::GetPressure ( void ) const

inline

Get the current gas pressure inside the gas cell.

Returns: gas pressure in lbs / ft².

Definition at line 224 of file FGGasCell.h.

◆ GetTemperature()

double JSBSim::FGGasCell::GetTemperature ( void ) const

inline

Get the current gas temperature inside the gas cell.

Returns: gas temperature in Rankine.

Definition at line 220 of file FGGasCell.h.

◆ GetXYZ() [1/2]

double JSBSim::FGGasCell::GetXYZ ( int idx ) const

inline

Get the center of gravity location of the gas cell (including any ballonets)

Returns: CoG location in the structural frame in inches.

Definition at line 200 of file FGGasCell.h.

◆ GetXYZ() [2/2]

const FGColumnVector3 & JSBSim::FGGasCell::GetXYZ ( void ) const

inline

Get the center of gravity location of the gas cell (including any ballonets)

Returns: CoG location in the structural frame in inches.

Definition at line 195 of file FGGasCell.h.

Member Data Documentation

◆ in

const struct Inputs& JSBSim::FGGasCell::in

Definition at line 226 of file FGGasCell.h.

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

Classes

Public Member Functions

Public Attributes

Additional Inherited Members

Detailed Description

Configuration File Format:

Constructor & Destructor Documentation

◆ FGGasCell()

◆ ~FGGasCell()

Member Function Documentation

◆ Calculate()

◆ GetIndex()

◆ GetInertia()

◆ GetMass()

◆ GetMassMoment()

◆ GetPressure()

◆ GetTemperature()

◆ GetXYZ() [1/2]

◆ GetXYZ() [2/2]

Member Data Documentation

◆ in