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.
|
| 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 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 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 |
| |
| FGFDMExec * | FDMExec |
| |
| std::string | Name |
| |
| std::shared_ptr< FGPropertyManager > | PropertyManager |
| |
| unsigned int | rate |
| |
| FGPropertyReader | LocalProperties |
| |
| std::vector< std::shared_ptr< FGFunction > > | PostFunctions |
| |
| std::vector< std::shared_ptr< FGFunction > > | PreFunctions |
| |
| 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 | fttom = 0.3048 |
| |
| static constexpr double | ktstofps = 1852./(3600*fttom) |
| |
| static constexpr double | fpstokts = 1.0 / ktstofps |
| |
| static constexpr double | inchtoft = 1.0/12.0 |
| |
| 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__ |
| |
Inheritance diagram for FGAircraft:
1.9.8 
