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github.com/JSBSim-Team/jsbsim
/ functions
Functions
4,135 in github.com/JSBSim-Team/jsbsim
⨍
Functions
4,135
◇
Types & classes
724
↓ 1 callers
Function
stripTrailingNewlines_inplace
src/simgear/misc/strutils.cxx:269
↓ 1 callers
Function
sumex
Eq. A24c */
src/models/atmosphere/MSIS/nrlmsise-00.c:589
↓ 1 callers
Function
test_gtd7
src/models/atmosphere/MSIS/nrlmsise-00_test.c:34
↓ 1 callers
Function
tselec
src/models/atmosphere/MSIS/nrlmsise-00.c:82
↓ 1 callers
Method
update
src/math/FGNelderMead.cpp:56
↓ 1 callers
Method
update
Run an iteration of the EOM (equations of motion)
examples/FlightGear.cxx:509
↓ 1 callers
Function
writeRandomBytes_arc4random
src/simgear/xml/xmlparse.c:1111
↓ 1 callers
Function
writeRandomBytes_dev_urandom
Extract entropy from /dev/urandom */
src/simgear/xml/xmlparse.c:1078
↓ 1 callers
Function
writeRandomBytes_getrandom_nonblock
Obtain entropy on Linux 3.17+ */
src/simgear/xml/xmlparse.c:1043
↓ 1 callers
Function
writeRandomBytes_rand_s
Obtain entropy on Windows using the rand_s() function which * generates cryptographically secure random numbers. Internally it * uses RtlGenRandom
src/simgear/xml/xmlparse.c:1144
↓ 1 callers
Method
write_fgfs
utils/aeromatic++/Aircraft.cpp:1087
↓ 1 callers
Method
yaw
utils/aeromatic++/Systems/Controls.cpp:830
Method
set_pitch
utils/aeromatic++/AeroFighterJet.cpp:131
Function
(charRefNumber)
src/simgear/xml/xmltok_impl.c:1602
Function
(nameLength)
src/simgear/xml/xmltok_impl.c:1733
Function
(skipS)
src/simgear/xml/xmltok_impl.c:1763
Method
A1m1f
The scale factor A1-1 = mean value of (d/dsigma)I1 - 1
src/GeographicLib/Geodesic.cpp:950
Method
A2m1f
The scale factor A2-1 = mean value of (d/dsigma)I2 - 1
src/GeographicLib/Geodesic.cpp:1195
Method
A3coeff
The scale factor A3 = mean value of (d/dsigma)I3
src/GeographicLib/Geodesic.cpp:1334
Method
AccelX
src/math/FGStateSpace.h:342
Method
AccelY
src/math/FGStateSpace.h:356
Method
AccelZ
src/math/FGStateSpace.h:370
Function
AddChildElement
Adds a child element to the list of children stored for this element. * @param el Child element to add. */
src/input_output/FGXMLElement.h:345
Method
AddControl
src/initialization/FGTrimAnalysis.cpp:692
Method
AddPointMass
src/models/FGMassBalance.cpp:267
Method
AddState
src/initialization/FGTrim.cpp:139
Function
AddTemplateFunc
src/FGFDMExec.h:627
Method
Aeromatic
utils/aeromatic++/Aircraft.cpp:102
Method
Aircraft
utils/aeromatic++/Aircraft.cpp:40
Method
Allocate
src/FGFDMExec.cpp:204
Method
Alpha
src/math/FGStateSpace.h:384
Method
Alt
src/math/FGStateSpace.h:445
Method
AngRound
src/GeographicLib/Math.cpp:117
Method
Append
* @brief Append the specified string to the internal buffer. * * @param s The string to append. */
src/input_output/FGfdmSocket.h:131
Method
ApplyEnginesCommands
UnrealEngine/Plugins/JSBSimFlightDynamicsModel/Source/JSBSimFlightDynamicsModel/Private/JSBSimMovementComponent.cpp:995
Function
Arc
* @return \e a13, the arc length to point 3 (degrees). **********************************************************************/
src/GeographicLib/GeodesicLine.hpp:695
Function
ArcDirect
\name Direct geodesic problem specified in terms of arc length. **********************************************************************/ @{ * Solv
src/GeographicLib/Geodesic.hpp:491
Method
ArcDirectLine
src/GeographicLib/Geodesic.cpp:154
Function
ArcPosition
* Compute the position of point 2 which is an arc length \e a12 (degrees) * from point 1. * * @param[in] a12 arc length from point 1 to
src/GeographicLib/GeodesicLine.hpp:394
Method
ArrestorHook
utils/aeromatic++/Systems/Systems.h:171
Method
Astroid
src/GeographicLib/Geodesic.cpp:597
Function
Azimuth
* @return \e azi1 the azimuth (degrees) of the geodesic line at point 1. **********************************************************************/
src/GeographicLib/GeodesicLine.hpp:606
Method
BadUnits
src/models/FGAuxiliary.cpp:476
Method
BeginDestroy
UnrealEngine/Plugins/JSBSimFlightDynamicsModel/Source/JSBSimFlightDynamicsModel/Private/JSBSimMovementComponent.cpp:405
Method
BeginPlay
UnrealEngine/Plugins/JSBSimFlightDynamicsModel/Source/JSBSimFlightDynamicsModel/Private/JSBSimMovementComponent.cpp:413
Method
Beta
src/math/FGStateSpace.h:463
Method
Bias
src/models/flight_control/FGActuator.cpp:198
Method
Bias
src/models/flight_control/FGSensor.cpp:207
Method
BindModel
src/models/propulsion/FGTransmission.cpp:136
Method
Biplane
utils/aeromatic++/AeroBiplane.cpp:33
Method
BufferLogger
src/input_output/FGLog.cpp:62
Method
BuildPropertyCatalog
src/FGFDMExec.cpp:1083
Method
BuildStabilityTransformMatrices
src/models/FGAerodynamics.cpp:644
Method
C1f
The coefficients C1[l] in the Fourier expansion of B1
src/GeographicLib/Geodesic.cpp:983
Method
C1pf
The coefficients C1p[l] in the Fourier expansion of B1p
src/GeographicLib/Geodesic.cpp:1089
Method
C2f
The coefficients C2[l] in the Fourier expansion of B2
src/GeographicLib/Geodesic.cpp:1228
Method
C3coeff
The coefficients C3[l] in the Fourier expansion of B3
src/GeographicLib/Geodesic.cpp:1436
Method
C4coeff
src/GeographicLib/Geodesic.cpp:1641
Method
CNumericLocale
src/input_output/string_utilities.cpp:65
Method
COG
src/math/FGStateSpace.h:901
Method
CableControls
utils/aeromatic++/Systems/Controls.h:41
Method
CalcFuelNeed
src/models/propulsion/FGTurbine.cpp:384
Method
CalcFuelNeed
src/models/propulsion/FGElectric.cpp:110
Method
CalcFuelNeed
src/models/propulsion/FGBrushLessDCMotor.h:91
Method
CalcFuelNeed
src/models/propulsion/FGTurboProp.cpp:425
Method
CalcFuelNeed
src/models/propulsion/FGRocket.cpp:222
Method
CalcFuelNeed
src/models/propulsion/FGEngine.cpp:93
Method
CalcOxidizerNeed
src/models/propulsion/FGEngine.h:181
Method
CalcRotorState
src/models/propulsion/FGRotor.cpp:604
Method
Calculate
src/models/FGAtmosphere.cpp:146
Method
Calculate
src/models/atmosphere/FGMars.cpp:70
Method
Calculate
src/models/atmosphere/FGMSIS.cpp:125
Method
Calculate
src/models/atmosphere/FGStandardAtmosphere.cpp:182
Method
Calculate
src/models/propulsion/FGTurbine.cpp:109
Method
Calculate
src/models/propulsion/FGRotor.cpp:675
Method
Calculate
src/models/propulsion/FGTank.cpp:345
Method
Calculate
src/models/propulsion/FGThruster.h:87
Method
Calculate
src/models/propulsion/FGPiston.cpp:480
Method
Calculate
src/models/propulsion/FGElectric.cpp:86
Method
Calculate
src/models/propulsion/FGNozzle.cpp:78
Method
Calculate
basically P = Q*w and Q_Engine + (-Q_Rotor) = J * dw/dt, J = Moment
src/models/propulsion/FGTransmission.cpp:73
Method
Calculate
src/models/propulsion/FGTurboProp.cpp:182
Method
Calculate
src/models/propulsion/FGPropeller.cpp:212
Method
Calculate
src/models/propulsion/FGRocket.cpp:156
Method
Calculate
src/models/propulsion/FGBrushLessDCMotor.cpp:124
Method
CalculateDensityAltitude
src/models/atmosphere/FGStandardAtmosphere.cpp:532
Method
CalculateDynamicFilters
src/models/flight_control/FGFilter.cpp:112
Method
CalculateFrictionForces
src/models/FGAccelerations.cpp:233
Method
CalculateInertialVelocity
src/models/FGPropagate.cpp:319
Method
CalculateInertias
src/models/propulsion/FGTank.cpp:379
Method
CalculateLapseRates
src/models/atmosphere/FGStandardAtmosphere.cpp:460
Method
CalculatePQRdot
src/models/FGAccelerations.cpp:139
Method
CalculatePhiWFromTargetNlfTurn
src/initialization/FGTrimAnalysis.cpp:774
Method
CalculatePressureAltitude
src/models/atmosphere/FGStandardAtmosphere.cpp:563
Method
CalculatePressureBreakpoints
src/models/atmosphere/FGStandardAtmosphere.cpp:477
Method
CalculateQuatdot
src/models/FGPropagate.cpp:306
Method
CalculateSLSoundSpeedAndDensity
src/models/atmosphere/FGStandardAtmosphere.cpp:238
Method
CalculateStdDensityBreakpoints
src/models/atmosphere/FGStandardAtmosphere.cpp:523
Method
CalculateTransformMatrix
src/models/flight_control/FGSensorOrientation.h:105
Method
CalculateUVW
src/models/FGPropagate.cpp:329
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