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enum | { eL = 1
, eM
, eN
} |
| Moments L, M, N. More...
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|
enum | { eP = 1
, eQ
, eR
} |
| Rates P, Q, R. More...
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enum | { eU = 1
, eV
, eW
} |
| Velocities U, V, W. More...
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enum | { eX = 1
, eY
, eZ
} |
| Positions X, Y, Z. More...
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enum | { ePhi = 1
, eTht
, ePsi
} |
| Euler angles Phi, Theta, Psi. More...
|
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enum | { eDrag = 1
, eSide
, eLift
} |
| Stability axis forces, Drag, Side force, Lift. More...
|
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enum | { eRoll = 1
, ePitch
, eYaw
} |
| Local frame orientation Roll, Pitch, Yaw. More...
|
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enum | { eNorth = 1
, eEast
, eDown
} |
| Local frame position North, East, Down. More...
|
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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.
|
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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.
|
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static constexpr double | RankineToCelsius (double rankine) |
| Converts from degrees Rankine to degrees Celsius.
|
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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.
|
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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.
|
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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 |
|
static std::string | CreateIndexedPropertyName (const std::string &Property, int index) |
|
static Message | localMsg |
|
static std::queue< Message > | Messages |
|
static unsigned int | messageId = 0 |
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static constexpr double | radtodeg = 180. / 3.14159265358979323846 |
|
static constexpr double | degtorad = 3.14159265358979323846 / 180. |
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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 |
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static constexpr double | inchtoft = 1.0/12.0 |
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static constexpr double | fttom = 0.3048 |
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static constexpr double | m3toft3 = 1.0/(fttom*fttom*fttom) |
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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.
|
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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 |
|
Base class for JSBSim Flight Control System Components.
The Flight Control System (FCS) for JSBSim consists of the FCS container class (see FGFCS), the FGFCSComponent base class, and the component classes from which can be constructed a string, or channel. See:
- Author
- Jon S. Berndt
- See also
- Documentation for the FGFCS class, and for the configuration file class
Definition at line 84 of file FGFCSComponent.h.