|
| FGAircraft (FGFDMExec *Executive) |
| Constructor.
|
|
| ~FGAircraft () override |
| Destructor.
|
|
bool | Run (bool Holding) override |
| Runs the Aircraft model; called by the Executive Can pass in a value indicating if the executive is directing the simulation to Hold.
|
|
bool | InitModel (void) override |
|
bool | Load (Element *el) override |
| Loads the aircraft.
|
|
const std::string & | GetAircraftName (void) const |
| Gets the aircraft name.
|
|
double | GetWingArea (void) const |
| Gets the wing area.
|
|
double | GetWingSpan (void) const |
| Gets the wing span.
|
|
double | Getcbar (void) const |
| Gets the average wing chord.
|
|
double | GetWingIncidence (void) const |
|
double | GetWingIncidenceDeg (void) const |
|
double | GetHTailArea (void) const |
|
double | GetHTailArm (void) const |
|
double | GetVTailArea (void) const |
|
double | GetVTailArm (void) const |
|
double | Getlbarh (void) const |
|
double | Getlbarv (void) const |
|
double | Getvbarh (void) const |
|
double | Getvbarv (void) const |
|
const FGColumnVector3 & | GetMoments (void) const |
|
double | GetMoments (int idx) const |
|
const FGColumnVector3 & | GetForces (void) const |
|
double | GetForces (int idx) const |
|
const FGColumnVector3 & | GetXYZrp (void) const |
| Gets the the aero reference point (RP) coordinates.
|
|
const FGColumnVector3 & | GetXYZvrp (void) const |
|
const FGColumnVector3 & | GetXYZep (void) const |
|
double | GetXYZrp (int idx) const |
|
double | GetXYZvrp (int idx) const |
|
double | GetXYZep (int idx) const |
|
void | SetAircraftName (const std::string &name) |
|
void | SetXYZrp (int idx, double value) |
|
void | SetWingArea (double S) |
|
| FGModel (FGFDMExec *) |
| Constructor.
|
|
| ~FGModel () override |
| Destructor.
|
|
bool | InitModel (void) override |
|
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) |
|
virtual SGPath | FindFullPathName (const SGPath &path) const |
|
const std::string & | GetName (void) |
|
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.
|
|
|
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 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 | Upload (Element *el, bool preLoad) |
| Uploads this model in memory.
|
|
static std::string | CreateIndexedPropertyName (const std::string &Property, int index) |
|
unsigned int | exe_ctr |
|
unsigned int | rate |
|
std::string | Name |
|
FGFDMExec * | FDMExec |
|
FGPropertyManager * | PropertyManager |
|
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 |
|
Encapsulates an Aircraft and its systems.
Owns all the parts (other classes) which make up this aircraft. This includes the Engines, Tanks, Propellers, Nozzles, Aerodynamic and Mass properties, landing gear, etc. These constituent parts may actually run as separate JSBSim models themselves, but the responsibility for initializing them and for retrieving their force and moment contributions falls to FGAircraft.
The <metrics> section of the aircraft configuration file is read here, and the metrical information is held by this class.
Configuration File Format for <metrics> Section:
<metrics>
<wingarea unit="{FT2 | M2}"> {number} </wingarea>
<wingspan unit="{FT | M}"> {number} </wingspan>
<chord unit="{FT | M}"> {number} </chord>
<htailarea unit="{FT2 | M2}"> {number} </htailarea>
<htailarm unit="{FT | M}"> {number} </htailarm>
<vtailarea unit="{FT2 | M}"> {number} </vtailarea>
<vtailarm unit="{FT | M}"> {number} </vtailarm>
<wing_incidence unit="{RAD | DEG}"> {number} </wing_incidence>
<location name="{AERORP | EYEPOINT | VRP}" unit="{IN | M}">
<x> {number} </x>
<y> {number} </y>
<z> {number} </z>
</location>
{other location blocks}
</metrics>
@author Jon S. Berndt
@see Cooke, Zyda, Pratt, and McGhee, "NPSNET: Flight Simulation Dynamic Modeling
Using Quaternions", Presence, Vol. 1, No. 4, pp. 404-420 Naval Postgraduate
School, January 1994
@see D. M. Henderson, "Euler Angles, Quaternions, and Transformation Matrices",
JSC 12960, July 1977
@see Richard E. McFarland, "A Standard Kinematic Model for Flight Simulation at
NASA-Ames", NASA CR-2497, January 1975
@see Barnes W. McCormick, "Aerodynamics, Aeronautics, and Flight Mechanics",
Wiley & Sons, 1979 ISBN 0-471-03032-5
@see Bernard Etkin, "Dynamics of Flight, Stability and Control", Wiley & Sons,
1982 ISBN 0-471-08936-2
Definition at line 102 of file FGAircraft.h.