|
enum | phaseType {
tpOff
, tpRun
, tpSpinUp
, tpStart
,
tpTrim
} |
|
enum | EngineType {
etUnknown
, etRocket
, etPiston
, etTurbine
,
etTurboprop
, etElectric
} |
|
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...
|
|
|
| FGTurboProp (FGFDMExec *Executive, Element *el, int engine_number, struct Inputs &input) |
| Constructor.
|
|
| ~FGTurboProp () |
| Destructor.
|
|
void | Calculate (void) |
| Calculates the thrust of the engine, and other engine functions.
|
|
double | CalcFuelNeed (void) |
| The fuel need is calculated based on power levels and flow rate for that power level.
|
|
double | GetPowerAvailable (void) const |
|
double | GetRPM (void) const |
|
double | GetIeluThrottle (void) const |
|
bool | GetIeluIntervent (void) const |
|
double | Seek (double *var, double target, double accel, double decel) |
|
double | ExpSeek (double *var, double target, double accel, double decel) |
|
phaseType | GetPhase (void) const |
|
bool | GetReversed (void) const |
|
bool | GetCutoff (void) const |
|
double | GetN1 (void) const |
|
double | GetITT (void) const |
|
double | GetEngStarting (void) const |
|
double | getOilPressure_psi () const |
|
double | getOilTemp_degF (void) |
|
bool | GetGeneratorPower (void) const |
|
int | GetCondition (void) const |
|
void | SetPhase (phaseType p) |
|
void | SetReverse (bool reversed) |
|
void | SetCutoff (bool cutoff) |
|
void | SetGeneratorPower (bool gp) |
|
void | SetCondition (bool c) |
|
int | InitRunning (void) |
|
std::string | GetEngineLabels (const std::string &delimiter) |
|
std::string | GetEngineValues (const std::string &delimiter) |
|
| FGEngine (int engine_number, struct Inputs &input) |
|
| ~FGEngine () override |
|
EngineType | GetType (void) const |
|
virtual const std::string & | GetName (void) const |
|
virtual double | GetThrottleMin (void) const |
|
virtual double | GetThrottleMax (void) const |
|
virtual bool | GetStarter (void) const |
|
virtual double | getFuelFlow_gph () const |
|
virtual double | getFuelFlow_pph () const |
|
virtual double | GetFuelFlowRate (void) const |
|
virtual double | GetFuelFlowRateGPH (void) const |
|
virtual double | GetFuelUsedLbs (void) const |
|
virtual bool | GetStarved (void) const |
|
virtual bool | GetRunning (void) const |
|
virtual bool | GetCranking (void) const |
|
virtual void | SetStarved (bool tt) |
|
virtual void | SetStarved (void) |
|
virtual void | SetRunning (bool bb) |
|
virtual void | SetName (const std::string &name) |
|
virtual void | SetFuelFreeze (bool f) |
|
virtual void | SetFuelDensity (double d) |
|
virtual void | SetStarter (bool s) |
|
virtual void | ResetToIC (void) |
| Resets the Engine parameters to the initial conditions.
|
|
virtual double | GetThrust (void) const |
|
virtual double | CalcOxidizerNeed (void) |
|
virtual double | GetPowerAvailable (void) |
|
virtual const FGColumnVector3 & | GetBodyForces (void) |
|
virtual const FGColumnVector3 & | GetMoments (void) |
|
void | LoadThruster (FGFDMExec *exec, Element *el) |
|
FGThruster * | GetThruster (void) const |
|
unsigned int | GetSourceTank (unsigned int i) const |
|
size_t | GetNumSourceTanks () const |
|
void | LoadThrusterInputs () |
|
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.
|
|
| 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.
|
|
|
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) |
|
struct Inputs & | in |
|
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 |
|
bool | Load (FGFDMExec *exec, Element *el) |
|
void | Debug (int from) |
|
virtual bool | InitModel (void) |
|
static std::string | CreateIndexedPropertyName (const std::string &Property, int index) |
|
std::string | Name |
|
const int | EngineNumber |
|
EngineType | Type |
|
double | SLFuelFlowMax |
|
double | MaxThrottle |
|
double | MinThrottle |
|
double | FuelExpended |
|
double | FuelFlowRate |
|
double | PctPower |
|
bool | Starter |
|
bool | Starved |
|
bool | Running |
|
bool | Cranking |
|
bool | FuelFreeze |
|
double | FuelFlow_gph |
|
double | FuelFlow_pph |
|
double | FuelUsedLbs |
|
double | FuelDensity |
|
FGThruster * | Thruster |
|
std::vector< int > | SourceTanks |
|
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 |
|
Turboprop engine model.
For an example of this model in use see the file: engine/engtm601.xml
Configuration parameters:
milthrust [LBS]
idlen1 [%]
maxn1 [%]
betarangeend[%]
if ThrottleCmd < betarangeend/100.0 then engine power=idle, propeller pitch
is controled by ThrottleCmd (between MINPITCH and REVERSEPITCH).
if ThrottleCmd > betarangeend/100.0 then engine power increases up to max reverse power
reversemaxpower [%]
max engine power in reverse mode
maxpower [HP]
psfc power specific fuel consumption [pph/HP] for N1=100%
n1idle_max_delay [-] time constant for N1 change
maxstartenginetime [sec]
after this time the automatic starting cycle is interrupted when the engine
doesn't start (0=automatic starting not present)
startern1 [%]
when starting starter spin up engine to this spin
ielumaxtorque [lb.ft]
if torque>ielumaxtorque limiters decrease the throttle
(ielu = Integrated Electronic Limiter Unit)
itt_delay [-] time constant for ITT change
(ITT = Inter Turbine Temperature)
Definition at line 92 of file FGTurboProp.h.