JSBSim Flight Dynamics Model  1.1.11 (13 Feb 2022)
An Open Source Flight Dynamics and Control Software Library in C++
FGAtmosphere Class Referenceabstract

Detailed Description

Models an empty, abstract base atmosphere class.

Properties

  • atmosphere/T-R The current modeled temperature in degrees Rankine.
  • atmosphere/rho-slugs_ft3
  • atmosphere/P-psf
  • atmosphere/a-fps
  • atmosphere/T-sl-R
  • atmosphere/rho-sl-slugs_ft3
  • atmosphere/P-sl-psf
  • atmosphere/a-sl-fps
  • atmosphere/theta
  • atmosphere/sigma
  • atmosphere/delta
  • atmosphere/a-ratio
Author
Jon Berndt

Definition at line 76 of file FGAtmosphere.h.

#include <FGAtmosphere.h>

+ Inheritance diagram for FGAtmosphere:
+ Collaboration diagram for FGAtmosphere:

Classes

struct  Inputs
 

Public Types

enum  ePressure {
  eNoPressUnit =0, ePSF, eMillibars, ePascals,
  eInchesHg
}
 Enums for specifying pressure units.
 
enum  eTemperature {
  eNoTempUnit =0, eFahrenheit, eCelsius, eRankine,
  eKelvin
}
 Enums for specifying temperature units.
 
- Public Types inherited from FGJSBBase
enum  { eL = 1, eM, eN }
 Moments L, M, N.
 
enum  { eP = 1, eQ, eR }
 Rates P, Q, R.
 
enum  { eU = 1, eV, eW }
 Velocities U, V, W.
 
enum  { eX = 1, eY, eZ }
 Positions X, Y, Z.
 
enum  { ePhi = 1, eTht, ePsi }
 Euler angles Phi, Theta, Psi.
 
enum  { eDrag = 1, eSide, eLift }
 Stability axis forces, Drag, Side force, Lift.
 
enum  { eRoll = 1, ePitch, eYaw }
 Local frame orientation Roll, Pitch, Yaw.
 
enum  { eNorth = 1, eEast, eDown }
 Local frame position North, East, Down.
 
enum  { eLat = 1, eLong, eRad }
 Locations Radius, Latitude, Longitude.
 
enum  {
  inNone = 0, inDegrees, inRadians, inMeters,
  inFeet
}
 Conversion specifiers.
 

Public Member Functions

 FGAtmosphere (FGFDMExec *)
 Constructor.
 
virtual ~FGAtmosphere ()
 Destructor.
 
bool InitModel (void) override
 
bool Run (bool Holding) override
 Runs the atmosphere forces model; called by the Executive. More...
 
Temperature access functions.

There are several ways to get the temperature, and several modeled temperature values that can be retrieved.

virtual double GetTemperature () const
 Returns the actual, modeled temperature at the current altitude in degrees Rankine. More...
 
virtual double GetTemperature (double altitude) const =0
 Returns the actual modeled temperature in degrees Rankine at a specified altitude. More...
 
virtual double GetTemperatureSL () const
 Returns the actual, modeled sea level temperature in degrees Rankine. More...
 
virtual double GetTemperatureRatio () const
 Returns the ratio of the at-current-altitude temperature as modeled over the sea level value.
 
virtual double GetTemperatureRatio (double h) const
 Returns the ratio of the temperature as modeled at the supplied altitude over the sea level value.
 
virtual void SetTemperatureSL (double t, eTemperature unit=eFahrenheit)
 Sets the Sea Level temperature. More...
 
virtual void SetTemperature (double t, double h, eTemperature unit=eFahrenheit)=0
 Sets the temperature at the supplied altitude. More...
 
Pressure access functions.
virtual double GetPressure (void) const
 Returns the pressure in psf.
 
virtual double GetPressure (double altitude) const =0
 Returns the pressure at a specified altitude in psf.
 
virtual double GetPressureSL (ePressure to=ePSF) const
 
virtual double GetPressureRatio (void) const
 Returns the ratio of at-altitude pressure over the sea level value.
 
virtual void SetPressureSL (ePressure unit, double pressure)
 Sets the sea level pressure for modeling. More...
 
Density access functions.
virtual double GetDensity (void) const
 Returns the density in slugs/ft^3. More...
 
virtual double GetDensity (double altitude) const
 Returns the density in slugs/ft^3 at a given altitude in ft.
 
virtual double GetDensitySL (void) const
 Returns the sea level density in slugs/ft^3.
 
virtual double GetDensityRatio (void) const
 Returns the ratio of at-altitude density over the sea level value.
 
Speed of sound access functions.
virtual double GetSoundSpeed (void) const
 Returns the speed of sound in ft/sec.
 
virtual double GetSoundSpeed (double altitude) const
 Returns the speed of sound in ft/sec at a given altitude in ft.
 
virtual double GetSoundSpeedSL (void) const
 Returns the sea level speed of sound in ft/sec.
 
virtual double GetSoundSpeedRatio (void) const
 Returns the ratio of at-altitude sound speed over the sea level value.
 
- Public Member Functions inherited from FGModel
 FGModel (FGFDMExec *)
 Constructor.
 
 ~FGModel () override
 Destructor.
 
virtual SGPath FindFullPathName (const SGPath &path) const
 
FGFDMExecGetExec (void)
 
const std::string & GetName (void)
 
unsigned int GetRate (void)
 Get the output rate for the model in frames.
 
bool InitModel (void) override
 
virtual bool Load (Element *el)
 
void SetPropertyManager (FGPropertyManager *fgpm)
 
void SetRate (unsigned int tt)
 Set the ouput rate for the model in frames.
 
- Public Member Functions inherited from FGModelFunctions
std::string GetFunctionStrings (const std::string &delimeter) const
 Gets the strings for the current set of functions. More...
 
std::string GetFunctionValues (const std::string &delimeter) const
 Gets the function values. More...
 
FGFunctionGetPreFunction (const std::string &name)
 Get one of the "pre" function. More...
 
bool Load (Element *el, FGFDMExec *fdmex, std::string prefix="")
 
void PostLoad (Element *el, FGFDMExec *fdmex, std::string prefix="")
 
void PreLoad (Element *el, FGFDMExec *fdmex, std::string prefix="")
 
void RunPostFunctions (void)
 
void RunPreFunctions (void)
 
- Public Member Functions inherited from FGJSBBase
 FGJSBBase ()
 Constructor for FGJSBBase.
 
virtual ~FGJSBBase ()
 Destructor for FGJSBBase.
 
void PutMessage (const Message &msg)
 Places a Message structure on the Message queue. More...
 
void PutMessage (const std::string &text)
 Creates a message with the given text and places it on the queue. More...
 
void PutMessage (const std::string &text, bool bVal)
 Creates a message with the given text and boolean value and places it on the queue. More...
 
void PutMessage (const std::string &text, int iVal)
 Creates a message with the given text and integer value and places it on the queue. More...
 
void PutMessage (const std::string &text, double dVal)
 Creates a message with the given text and double value and places it on the queue. More...
 
int SomeMessages (void) const
 Reads the message on the queue (but does not delete it). More...
 
void ProcessMessage (void)
 Reads the message on the queue and removes it from the queue. More...
 
MessageProcessNextMessage (void)
 Reads the next message on the queue and removes it from the queue. More...
 
void disableHighLighting (void)
 Disables highlighting in the console output.
 

Viscosity access functions.

struct JSBSim::FGAtmosphere::Inputs in
 
static constexpr double StdDaySLtemperature = 518.67
 
static constexpr double StdDaySLpressure = 2116.228
 
static const double StdDaySLsoundspeed = sqrt(SHRatio*Reng*StdDaySLtemperature)
 
double SLtemperature
 
double SLdensity
 
double SLpressure
 
double SLsoundspeed
 
double Temperature
 
double Density
 
double Pressure
 
double Soundspeed
 
double PressureAltitude
 
double DensityAltitude
 
double Viscosity
 
double KinematicViscosity
 
static constexpr double SutherlandConstant = 198.72
 
static constexpr double Beta = 2.269690E-08
 
virtual double GetAbsoluteViscosity (void) const
 Returns the absolute viscosity.
 
virtual double GetKinematicViscosity (void) const
 Returns the kinematic viscosity.
 
virtual double GetDensityAltitude () const
 
virtual double GetPressureAltitude () const
 
virtual void Calculate (double altitude)
 Calculate the atmosphere for the given altitude.
 
virtual double CalculateDensityAltitude (double density, double geometricAlt)
 Calculates the density altitude given any temperature or pressure bias. More...
 
virtual double CalculatePressureAltitude (double pressure, double geometricAlt)
 Calculates the pressure altitude given any temperature or pressure bias. More...
 
double ConvertToRankine (double t, eTemperature unit) const
 Converts to Rankine from one of several unit systems.
 
double ConvertFromRankine (double t, eTemperature unit) const
 Converts from Rankine to one of several unit systems.
 
double ConvertToPSF (double t, ePressure unit=ePSF) const
 Converts to PSF (pounds per square foot) from one of several unit systems.
 
double ConvertFromPSF (double t, ePressure unit=ePSF) const
 Converts from PSF (pounds per square foot) to one of several unit systems.
 

ISA constants

static constexpr double Rstar = 8.31432 * kgtoslug / KelvinToRankine(fttom * fttom)
 Universal gas constant - ft*lbf/R/mol.
 
static constexpr double Mair = 28.9645 * kgtoslug / 1000.0
 Mean molecular weight for air - slug/mol.
 
static constexpr double g0 = 9.80665 / fttom
 Sea-level acceleration of gravity - ft/s^2. More...
 
static double Reng = Rstar / Mair
 Specific gas constant for air - ft*lbf/slug/R.
 
static constexpr double SHRatio = 1.4
 
virtual void bind (void)
 
void Debug (int from) override
 

Additional Inherited Members

- Static Public Member Functions inherited from FGJSBBase
static const std::string & GetVersion (void)
 Returns the version number of JSBSim. More...
 
static constexpr double KelvinToFahrenheit (double kelvin)
 Converts from degrees Kelvin to degrees Fahrenheit. More...
 
static constexpr double CelsiusToRankine (double celsius)
 Converts from degrees Celsius to degrees Rankine. More...
 
static constexpr double RankineToCelsius (double rankine)
 Converts from degrees Rankine to degrees Celsius. More...
 
static constexpr double KelvinToRankine (double kelvin)
 Converts from degrees Kelvin to degrees Rankine. More...
 
static constexpr double RankineToKelvin (double rankine)
 Converts from degrees Rankine to degrees Kelvin. More...
 
static constexpr double FahrenheitToCelsius (double fahrenheit)
 Converts from degrees Fahrenheit to degrees Celsius. More...
 
static constexpr double CelsiusToFahrenheit (double celsius)
 Converts from degrees Celsius to degrees Fahrenheit. More...
 
static constexpr double CelsiusToKelvin (double celsius)
 Converts from degrees Celsius to degrees Kelvin. More...
 
static constexpr double KelvinToCelsius (double kelvin)
 Converts from degrees Kelvin to degrees Celsius. More...
 
static constexpr double FeetToMeters (double measure)
 Converts from feet to meters. More...
 
static double PitotTotalPressure (double mach, double p)
 Compute the total pressure in front of the Pitot tube. More...
 
static double MachFromImpactPressure (double qc, double p)
 Compute the Mach number from the differential pressure (qc) and the static pressure. More...
 
static double VcalibratedFromMach (double mach, double p)
 Calculate the calibrated airspeed from the Mach number. More...
 
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). More...
 
static bool EqualToRoundoff (double a, double b)
 Finite precision comparison. More...
 
static bool EqualToRoundoff (float a, float b)
 Finite precision comparison. More...
 
static bool EqualToRoundoff (float a, double b)
 Finite precision comparison. More...
 
static bool EqualToRoundoff (double a, float b)
 Finite precision comparison. More...
 
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 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 FGModel
bool Upload (Element *el, bool preLoad)
 Uploads this model in memory. More...
 
- Static Protected Member Functions inherited from FGJSBBase
static std::string CreateIndexedPropertyName (const std::string &Property, int index)
 
- Protected Attributes inherited from FGModel
unsigned int exe_ctr
 
FGFDMExecFDMExec
 
std::string Name
 
FGPropertyManagerPropertyManager
 
unsigned int rate
 
- Protected Attributes inherited from FGModelFunctions
FGPropertyReader LocalProperties
 
std::vector< FGFunction * > PostFunctions
 
std::vector< FGFunction * > PreFunctions
 
- Static Protected Attributes inherited from FGJSBBase
static Message localMsg
 
static std::queue< MessageMessages
 
static unsigned int messageId = 0
 
static constexpr double radtodeg = 180. / M_PI
 
static constexpr double degtorad = M_PI / 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. More...
 
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
 

Member Function Documentation

◆ CalculateDensityAltitude()

virtual double CalculateDensityAltitude ( double  density,
double  geometricAlt 
)
inlineprotectedvirtual

Calculates the density altitude given any temperature or pressure bias.

Calculated density for the specified geometric altitude given any temperature or pressure biases is passed in.

Parameters
density
geometricAlt

Reimplemented in FGStandardAtmosphere.

Definition at line 236 of file FGAtmosphere.h.

236 { return geometricAlt; }
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◆ CalculatePressureAltitude()

virtual double CalculatePressureAltitude ( double  pressure,
double  geometricAlt 
)
inlineprotectedvirtual

Calculates the pressure altitude given any temperature or pressure bias.

Calculated pressure for the specified geometric altitude given any temperature or pressure biases is passed in.

Parameters
pressure
geometricAlt

Reimplemented in FGStandardAtmosphere.

Definition at line 243 of file FGAtmosphere.h.

243 { return geometricAlt; }
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◆ GetDensity()

virtual double GetDensity ( void  ) const
inlinevirtual

Returns the density in slugs/ft^3.

This function may only be used if Run() is called first.

Definition at line 167 of file FGAtmosphere.h.

167 {return Density;}
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◆ GetTemperature() [1/2]

virtual double GetTemperature ( ) const
inlinevirtual

Returns the actual, modeled temperature at the current altitude in degrees Rankine.

Returns
Modeled temperature in degrees Rankine.

Definition at line 109 of file FGAtmosphere.h.

109 {return Temperature;}
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◆ GetTemperature() [2/2]

virtual double GetTemperature ( double  altitude) const
pure virtual

Returns the actual modeled temperature in degrees Rankine at a specified altitude.

Parameters
altitudeThe altitude above sea level (ASL) in feet.
Returns
Modeled temperature in degrees Rankine at the specified altitude.

Implemented in FGStandardAtmosphere.

◆ GetTemperatureSL()

virtual double GetTemperatureSL ( ) const
inlinevirtual

Returns the actual, modeled sea level temperature in degrees Rankine.

Returns
The modeled temperature in degrees Rankine at sea level.

Definition at line 118 of file FGAtmosphere.h.

118 { return SLtemperature; }

◆ Run()

bool Run ( bool  Holding)
overridevirtual

Runs the atmosphere forces model; called by the Executive.

Can pass in a value indicating if the executive is directing the simulation to Hold.

Parameters
Holdingif 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 FGModel.

Reimplemented in MSIS.

Definition at line 94 of file FGAtmosphere.cpp.

95 {
96  if (FGModel::Run(Holding)) return true;
97  if (Holding) return false;
98 
99  Calculate(in.altitudeASL);
100 
101  Debug(2);
102  return false;
103 }
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◆ SetPressureSL()

void SetPressureSL ( ePressure  unit,
double  pressure 
)
virtual

Sets the sea level pressure for modeling.

Parameters
pressureThe pressure in the units specified.
unitthe unit of measure that the specified pressure is supplied in.

Reimplemented in FGStandardAtmosphere.

Definition at line 135 of file FGAtmosphere.cpp.

136 {
137  double press = ConvertToPSF(pressure, unit);
138 
139  SLpressure = press;
140 }
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◆ SetTemperature()

virtual void SetTemperature ( double  t,
double  h,
eTemperature  unit = eFahrenheit 
)
pure virtual

Sets the temperature at the supplied altitude.

Parameters
tThe temperature value in the unit provided.
hThe altitude in feet above sea level.
unitThe unit of the temperature.

Implemented in FGStandardAtmosphere.

◆ SetTemperatureSL()

void SetTemperatureSL ( double  t,
eTemperature  unit = eFahrenheit 
)
virtual

Sets the Sea Level temperature.

Parameters
tthe temperature value in the unit provided.
unitthe unit of the temperature.

Reimplemented in FGStandardAtmosphere.

Definition at line 162 of file FGAtmosphere.cpp.

163 {
164  SLtemperature = ConvertToRankine(t, unit);
165 }
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Member Data Documentation

◆ g0

constexpr double g0 = 9.80665 / fttom
staticconstexprprotected

Sea-level acceleration of gravity - ft/s^2.

This constant is defined to compute the International Standard Atmosphere. It is by definition the sea level gravity at a latitude of 45deg. This value is fixed whichever gravity model is used by FGInertial.

Definition at line 268 of file FGAtmosphere.h.


The documentation for this class was generated from the following files:
JSBSim::FGAtmosphere::ConvertToRankine
double ConvertToRankine(double t, eTemperature unit) const
Converts to Rankine from one of several unit systems.
Definition: FGAtmosphere.cpp:169
JSBSim::FGAtmosphere::ConvertToPSF
double ConvertToPSF(double t, ePressure unit=ePSF) const
Converts to PSF (pounds per square foot) from one of several unit systems.
Definition: FGAtmosphere.cpp:221
JSBSim::FGAtmosphere::Calculate
virtual void Calculate(double altitude)
Calculate the atmosphere for the given altitude.
Definition: FGAtmosphere.cpp:107
JSBSim::FGModel::Run
virtual bool Run(bool Holding)
Runs the model; called by the Executive.
Definition: FGModel.cpp:89