FlightGear next
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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. | |
FGEngine * | GetEngine (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. | |
FGTank * | GetTank (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 FGColumnVector3 & | GetForces (void) const |
double | GetForces (int n) const |
const FGColumnVector3 & | GetMoments (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 FGColumnVector3 & | GetTanksMoment (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 FGMatrix33 & | CalculateTankInertias (void) |
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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. | |
FGFDMExec * | GetExec (void) |
void | SetPropertyManager (FGPropertyManager *fgpm) |
const std::string & | GetName (void) |
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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. | |
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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 FGEngine::Inputs | in |
Additional Inherited Members | |
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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) |
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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 |
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bool | Upload (Element *el, bool preLoad) |
Uploads this model in memory. | |
static std::string | CreateIndexedPropertyName (const std::string &Property, int index) |
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unsigned int | exe_ctr |
unsigned int | rate |
std::string | Name |
FGFDMExec * | FDMExec |
FGPropertyManager * | PropertyManager |
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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 |
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:
At Run time each engine's Calculate() method is called.
Definition at line 99 of file FGPropulsion.h.
JSBSim::FGPropulsion::FGPropulsion | ( | FGFDMExec * | exec | ) |
Constructor.
Definition at line 70 of file FGPropulsion.cpp.
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Destructor.
Definition at line 94 of file FGPropulsion.cpp.
const FGMatrix33 & JSBSim::FGPropulsion::CalculateTankInertias | ( | void | ) |
Definition at line 578 of file FGPropulsion.cpp.
void JSBSim::FGPropulsion::DoRefuel | ( | double | time_slice | ) |
Definition at line 747 of file FGPropulsion.cpp.
void JSBSim::FGPropulsion::DumpFuel | ( | double | time_slice | ) |
Definition at line 769 of file FGPropulsion.cpp.
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Reimplemented from JSBSim::FGModel.
Definition at line 458 of file FGPropulsion.cpp.
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Definition at line 177 of file FGPropulsion.h.
int JSBSim::FGPropulsion::GetCutoff | ( | void | ) | const |
Definition at line 683 of file FGPropulsion.cpp.
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Retrieves an engine object pointer from the list of engines.
index | the engine index within the vector container |
Definition at line 133 of file FGPropulsion.h.
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Definition at line 165 of file FGPropulsion.h.
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Definition at line 164 of file FGPropulsion.h.
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Definition at line 178 of file FGPropulsion.h.
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Definition at line 167 of file FGPropulsion.h.
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Definition at line 166 of file FGPropulsion.h.
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Retrieves the number of engines defined for the aircraft.
Definition at line 127 of file FGPropulsion.h.
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Returns the number of fuel tanks currently actively supplying fuel.
Definition at line 149 of file FGPropulsion.h.
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Returns the number of oxidizer tanks currently actively supplying oxidizer.
Definition at line 152 of file FGPropulsion.h.
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Retrieves the number of tanks defined for the aircraft.
Definition at line 138 of file FGPropulsion.h.
string JSBSim::FGPropulsion::GetPropulsionStrings | ( | const std::string & | delimiter | ) | const |
Definition at line 471 of file FGPropulsion.cpp.
string JSBSim::FGPropulsion::GetPropulsionTankReport | ( | ) |
Definition at line 525 of file FGPropulsion.cpp.
string JSBSim::FGPropulsion::GetPropulsionValues | ( | const std::string & | delimiter | ) | const |
Definition at line 498 of file FGPropulsion.cpp.
int JSBSim::FGPropulsion::GetStarter | ( | void | ) | const |
Definition at line 635 of file FGPropulsion.cpp.
bool JSBSim::FGPropulsion::GetSteadyState | ( | void | ) |
Loops the engines until thrust output steady (used for trimming)
Definition at line 279 of file FGPropulsion.cpp.
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inline |
Retrieves a tank object pointer from the list of tanks.
index | the tank index within the vector container |
Definition at line 144 of file FGPropulsion.h.
const FGColumnVector3 & JSBSim::FGPropulsion::GetTanksMoment | ( | void | ) |
Definition at line 556 of file FGPropulsion.cpp.
double JSBSim::FGPropulsion::GetTanksWeight | ( | void | ) | const |
Definition at line 567 of file FGPropulsion.cpp.
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overridevirtual |
Reimplemented from JSBSim::FGModel.
Definition at line 105 of file FGPropulsion.cpp.
void JSBSim::FGPropulsion::InitRunning | ( | int | n | ) |
Sets up the engines as running.
Definition at line 329 of file FGPropulsion.cpp.
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overridevirtual |
Loads the propulsion system (engine[s] and tank[s]).
Characteristics of the propulsion system are read in from the config file.
el | pointer to an XML element that contains the engine information. |
Reimplemented from JSBSim::FGModel.
Definition at line 357 of file FGPropulsion.cpp.
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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.
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. |
Reimplemented from JSBSim::FGModel.
Definition at line 127 of file FGPropulsion.cpp.
void JSBSim::FGPropulsion::SetActiveEngine | ( | int | engine | ) |
Definition at line 718 of file FGPropulsion.cpp.
void JSBSim::FGPropulsion::SetCutoff | ( | int | setting = 0 | ) |
Definition at line 650 of file FGPropulsion.cpp.
void JSBSim::FGPropulsion::SetFuelFreeze | ( | bool | f | ) |
Definition at line 791 of file FGPropulsion.cpp.
void JSBSim::FGPropulsion::SetMagnetos | ( | int | setting | ) |
Definition at line 599 of file FGPropulsion.cpp.
void JSBSim::FGPropulsion::SetStarter | ( | int | setting | ) |
Definition at line 616 of file FGPropulsion.cpp.
double JSBSim::FGPropulsion::Transfer | ( | int | source, |
int | target, | ||
double | amount ) |
Definition at line 728 of file FGPropulsion.cpp.
struct FGEngine::Inputs JSBSim::FGPropulsion::in |
Definition at line 189 of file FGPropulsion.h.