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JSBSim::FGPropulsion Class Reference

Propulsion management class. More...

#include <FGPropulsion.h>

Inherits JSBSim::FGModel.

Public Member Functions

 FGPropulsion (FGFDMExec *)
 Constructor.
 
 ~FGPropulsion () override
 Destructor.
 
bool Run (bool Holding) override
 Executes the propulsion model.
 
bool InitModel (void) override
 
bool Load (Element *el) override
 Loads the propulsion system (engine[s] and tank[s]).
 
unsigned int GetNumEngines (void) const
 Retrieves the number of engines defined for the aircraft.
 
FGEngineGetEngine (unsigned int index) const
 Retrieves an engine object pointer from the list of engines.
 
unsigned int GetNumTanks (void) const
 Retrieves the number of tanks defined for the aircraft.
 
FGTankGetTank (unsigned int index) const
 Retrieves a tank object pointer from the list of tanks.
 
int GetnumSelectedFuelTanks (void) const
 Returns the number of fuel tanks currently actively supplying fuel.
 
int GetnumSelectedOxiTanks (void) const
 Returns the number of oxidizer tanks currently actively supplying oxidizer.
 
bool GetSteadyState (void)
 Loops the engines until thrust output steady (used for trimming)
 
void InitRunning (int n)
 Sets up the engines as running.
 
std::string GetPropulsionStrings (const std::string &delimiter) const
 
std::string GetPropulsionValues (const std::string &delimiter) const
 
std::string GetPropulsionTankReport ()
 
const FGColumnVector3GetForces (void) const
 
double GetForces (int n) const
 
const FGColumnVector3GetMoments (void) const
 
double GetMoments (int n) const
 
double Transfer (int source, int target, double amount)
 
void DoRefuel (double time_slice)
 
void DumpFuel (double time_slice)
 
const FGColumnVector3GetTanksMoment (void)
 
double GetTanksWeight (void) const
 
SGPath FindFullPathName (const SGPath &path) const override
 
int GetActiveEngine (void) const
 
bool GetFuelFreeze (void) const
 
void SetMagnetos (int setting)
 
void SetStarter (int setting)
 
int GetStarter (void) const
 
void SetCutoff (int setting=0)
 
int GetCutoff (void) const
 
void SetActiveEngine (int engine)
 
void SetFuelFreeze (bool f)
 
const FGMatrix33CalculateTankInertias (void)
 
- Public Member Functions inherited from JSBSim::FGModel
 FGModel (FGFDMExec *)
 Constructor.
 
 ~FGModel () override
 Destructor.
 
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.
 
FGFDMExecGetExec (void)
 
void SetPropertyManager (FGPropertyManager *fgpm)
 
const std::string & GetName (void)
 
- 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.
 
FGFunctionGetPreFunction (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.
 
MessageProcessNextMessage (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 FGEngine::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
 
FGFDMExecFDMExec
 
FGPropertyManagerPropertyManager
 
- Protected Attributes inherited from JSBSim::FGModelFunctions
std::vector< FGFunction * > PreFunctions
 
std::vector< FGFunction * > PostFunctions
 
FGPropertyReader LocalProperties
 
static Message localMsg
 
static std::queue< MessageMessages
 
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

Propulsion management class.

The Propulsion class is the container for the entire propulsion system, which is comprised of engines, and tanks. Once the Propulsion class gets the config file, it reads in the <propulsion> section. Then:

  1. The appropriate engine type instance is created
  2. At least one tank object is created, and is linked to an engine.

At Run time each engine's Calculate() method is called.

Configuration File Format:

<propulsion>
<engine file="{string}">
... see FGEngine, FGThruster, and class for engine type ...
</engine>
... more engines ...
<tank type="{FUEL | OXIDIZER}">
... see FGTank ...
</tank>
... more tanks ...
<dump-rate unit="{LBS/MIN | KG/MIN}"> {number} </dump-rate>
<refuel-rate unit="{LBS/MIN | KG/MIN}"> {number} </refuel-rate>
</propulsion>
Base class for all engines.
Definition FGEngine.h:104
unsigned int rate
Definition FGModel.h:102
Models a fuel tank.
Definition FGTank.h:202
Base class for specific thrusting devices such as propellers, nozzles, etc.
Definition FGThruster.h:77
Author
Jon S. Berndt
See also
FGEngine FGTank

Definition at line 99 of file FGPropulsion.h.

Constructor & Destructor Documentation

◆ FGPropulsion()

JSBSim::FGPropulsion::FGPropulsion ( FGFDMExec * exec)

Constructor.

Definition at line 70 of file FGPropulsion.cpp.

◆ ~FGPropulsion()

JSBSim::FGPropulsion::~FGPropulsion ( )
override

Destructor.

Definition at line 94 of file FGPropulsion.cpp.

Member Function Documentation

◆ CalculateTankInertias()

const FGMatrix33 & JSBSim::FGPropulsion::CalculateTankInertias ( void )

Definition at line 578 of file FGPropulsion.cpp.

◆ DoRefuel()

void JSBSim::FGPropulsion::DoRefuel ( double time_slice)

Definition at line 747 of file FGPropulsion.cpp.

◆ DumpFuel()

void JSBSim::FGPropulsion::DumpFuel ( double time_slice)

Definition at line 769 of file FGPropulsion.cpp.

◆ FindFullPathName()

SGPath JSBSim::FGPropulsion::FindFullPathName ( const SGPath & path) const
overridevirtual

Reimplemented from JSBSim::FGModel.

Definition at line 458 of file FGPropulsion.cpp.

◆ GetActiveEngine()

int JSBSim::FGPropulsion::GetActiveEngine ( void ) const
inline

Definition at line 177 of file FGPropulsion.h.

◆ GetCutoff()

int JSBSim::FGPropulsion::GetCutoff ( void ) const

Definition at line 683 of file FGPropulsion.cpp.

◆ GetEngine()

FGEngine * JSBSim::FGPropulsion::GetEngine ( unsigned int index) const
inline

Retrieves an engine object pointer from the list of engines.

Parameters
indexthe engine index within the vector container
Returns
the address of the specific engine, or zero if no such engine is available

Definition at line 133 of file FGPropulsion.h.

◆ GetForces() [1/2]

double JSBSim::FGPropulsion::GetForces ( int n) const
inline

Definition at line 165 of file FGPropulsion.h.

◆ GetForces() [2/2]

const FGColumnVector3 & JSBSim::FGPropulsion::GetForces ( void ) const
inline

Definition at line 164 of file FGPropulsion.h.

◆ GetFuelFreeze()

bool JSBSim::FGPropulsion::GetFuelFreeze ( void ) const
inline

Definition at line 178 of file FGPropulsion.h.

◆ GetMoments() [1/2]

double JSBSim::FGPropulsion::GetMoments ( int n) const
inline

Definition at line 167 of file FGPropulsion.h.

◆ GetMoments() [2/2]

const FGColumnVector3 & JSBSim::FGPropulsion::GetMoments ( void ) const
inline

Definition at line 166 of file FGPropulsion.h.

◆ GetNumEngines()

unsigned int JSBSim::FGPropulsion::GetNumEngines ( void ) const
inline

Retrieves the number of engines defined for the aircraft.

Definition at line 127 of file FGPropulsion.h.

◆ GetnumSelectedFuelTanks()

int JSBSim::FGPropulsion::GetnumSelectedFuelTanks ( void ) const
inline

Returns the number of fuel tanks currently actively supplying fuel.

Definition at line 149 of file FGPropulsion.h.

◆ GetnumSelectedOxiTanks()

int JSBSim::FGPropulsion::GetnumSelectedOxiTanks ( void ) const
inline

Returns the number of oxidizer tanks currently actively supplying oxidizer.

Definition at line 152 of file FGPropulsion.h.

◆ GetNumTanks()

unsigned int JSBSim::FGPropulsion::GetNumTanks ( void ) const
inline

Retrieves the number of tanks defined for the aircraft.

Definition at line 138 of file FGPropulsion.h.

◆ GetPropulsionStrings()

string JSBSim::FGPropulsion::GetPropulsionStrings ( const std::string & delimiter) const

Definition at line 471 of file FGPropulsion.cpp.

◆ GetPropulsionTankReport()

string JSBSim::FGPropulsion::GetPropulsionTankReport ( )

Definition at line 525 of file FGPropulsion.cpp.

◆ GetPropulsionValues()

string JSBSim::FGPropulsion::GetPropulsionValues ( const std::string & delimiter) const

Definition at line 498 of file FGPropulsion.cpp.

◆ GetStarter()

int JSBSim::FGPropulsion::GetStarter ( void ) const

Definition at line 635 of file FGPropulsion.cpp.

◆ GetSteadyState()

bool JSBSim::FGPropulsion::GetSteadyState ( void )

Loops the engines until thrust output steady (used for trimming)

Definition at line 279 of file FGPropulsion.cpp.

◆ GetTank()

FGTank * JSBSim::FGPropulsion::GetTank ( unsigned int index) const
inline

Retrieves a tank object pointer from the list of tanks.

Parameters
indexthe tank index within the vector container
Returns
the address of the specific tank, or zero if no such tank is available

Definition at line 144 of file FGPropulsion.h.

◆ GetTanksMoment()

const FGColumnVector3 & JSBSim::FGPropulsion::GetTanksMoment ( void )

Definition at line 556 of file FGPropulsion.cpp.

◆ GetTanksWeight()

double JSBSim::FGPropulsion::GetTanksWeight ( void ) const

Definition at line 567 of file FGPropulsion.cpp.

◆ InitModel()

bool JSBSim::FGPropulsion::InitModel ( void )
overridevirtual

Reimplemented from JSBSim::FGModel.

Definition at line 105 of file FGPropulsion.cpp.

◆ InitRunning()

void JSBSim::FGPropulsion::InitRunning ( int n)

Sets up the engines as running.

Definition at line 329 of file FGPropulsion.cpp.

◆ Load()

bool JSBSim::FGPropulsion::Load ( Element * el)
overridevirtual

Loads the propulsion system (engine[s] and tank[s]).

Characteristics of the propulsion system are read in from the config file.

Parameters
elpointer to an XML element that contains the engine information.
Returns
true if successfully loaded, otherwise false

Reimplemented from JSBSim::FGModel.

Definition at line 357 of file FGPropulsion.cpp.

◆ Run()

bool JSBSim::FGPropulsion::Run ( bool Holding)
overridevirtual

Executes the propulsion model.

The initial plan for the FGPropulsion class calls for Run() to be executed, calculating the power available from the engine. 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 JSBSim::FGModel.

Definition at line 127 of file FGPropulsion.cpp.

◆ SetActiveEngine()

void JSBSim::FGPropulsion::SetActiveEngine ( int engine)

Definition at line 718 of file FGPropulsion.cpp.

◆ SetCutoff()

void JSBSim::FGPropulsion::SetCutoff ( int setting = 0)

Definition at line 650 of file FGPropulsion.cpp.

◆ SetFuelFreeze()

void JSBSim::FGPropulsion::SetFuelFreeze ( bool f)

Definition at line 791 of file FGPropulsion.cpp.

◆ SetMagnetos()

void JSBSim::FGPropulsion::SetMagnetos ( int setting)

Definition at line 599 of file FGPropulsion.cpp.

◆ SetStarter()

void JSBSim::FGPropulsion::SetStarter ( int setting)

Definition at line 616 of file FGPropulsion.cpp.

◆ Transfer()

double JSBSim::FGPropulsion::Transfer ( int source,
int target,
double amount )

Definition at line 728 of file FGPropulsion.cpp.

Member Data Documentation

◆ in

struct FGEngine::Inputs JSBSim::FGPropulsion::in

Definition at line 189 of file FGPropulsion.h.


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