MCPcopy Create free account

hub / github.com/JSBSim-Team/jsbsim / functions

Functions4,135 in github.com/JSBSim-Team/jsbsim

↓ 1 callersFunctionstripTrailingNewlines_inplace
src/simgear/misc/strutils.cxx:269
↓ 1 callersFunctionsumex
Eq. A24c */
src/models/atmosphere/MSIS/nrlmsise-00.c:589
↓ 1 callersFunctiontest_gtd7
src/models/atmosphere/MSIS/nrlmsise-00_test.c:34
↓ 1 callersFunctiontselec
src/models/atmosphere/MSIS/nrlmsise-00.c:82
↓ 1 callersMethodupdate
src/math/FGNelderMead.cpp:56
↓ 1 callersMethodupdate
Run an iteration of the EOM (equations of motion)
examples/FlightGear.cxx:509
↓ 1 callersFunctionwriteRandomBytes_arc4random
src/simgear/xml/xmlparse.c:1111
↓ 1 callersFunctionwriteRandomBytes_dev_urandom
Extract entropy from /dev/urandom */
src/simgear/xml/xmlparse.c:1078
↓ 1 callersFunctionwriteRandomBytes_getrandom_nonblock
Obtain entropy on Linux 3.17+ */
src/simgear/xml/xmlparse.c:1043
↓ 1 callersFunctionwriteRandomBytes_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 callersMethodwrite_fgfs
utils/aeromatic++/Aircraft.cpp:1087
↓ 1 callersMethodyaw
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
MethodA1m1f
The scale factor A1-1 = mean value of (d/dsigma)I1 - 1
src/GeographicLib/Geodesic.cpp:950
MethodA2m1f
The scale factor A2-1 = mean value of (d/dsigma)I2 - 1
src/GeographicLib/Geodesic.cpp:1195
MethodA3coeff
The scale factor A3 = mean value of (d/dsigma)I3
src/GeographicLib/Geodesic.cpp:1334
MethodAccelX
src/math/FGStateSpace.h:342
MethodAccelY
src/math/FGStateSpace.h:356
MethodAccelZ
src/math/FGStateSpace.h:370
FunctionAddChildElement
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
MethodAddControl
src/initialization/FGTrimAnalysis.cpp:692
MethodAddPointMass
src/models/FGMassBalance.cpp:267
MethodAddState
src/initialization/FGTrim.cpp:139
FunctionAddTemplateFunc
src/FGFDMExec.h:627
MethodAeromatic
utils/aeromatic++/Aircraft.cpp:102
MethodAircraft
utils/aeromatic++/Aircraft.cpp:40
MethodAllocate
src/FGFDMExec.cpp:204
MethodAlpha
src/math/FGStateSpace.h:384
MethodAlt
src/math/FGStateSpace.h:445
MethodAngRound
src/GeographicLib/Math.cpp:117
MethodAppend
* @brief Append the specified string to the internal buffer. * * @param s The string to append. */
src/input_output/FGfdmSocket.h:131
MethodApplyEnginesCommands
UnrealEngine/Plugins/JSBSimFlightDynamicsModel/Source/JSBSimFlightDynamicsModel/Private/JSBSimMovementComponent.cpp:995
FunctionArc
* @return \e a13, the arc length to point 3 (degrees). **********************************************************************/
src/GeographicLib/GeodesicLine.hpp:695
FunctionArcDirect
\name Direct geodesic problem specified in terms of arc length. **********************************************************************/ @{ * Solv
src/GeographicLib/Geodesic.hpp:491
MethodArcDirectLine
src/GeographicLib/Geodesic.cpp:154
FunctionArcPosition
* 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
MethodArrestorHook
utils/aeromatic++/Systems/Systems.h:171
MethodAstroid
src/GeographicLib/Geodesic.cpp:597
FunctionAzimuth
* @return \e azi1 the azimuth (degrees) of the geodesic line at point 1. **********************************************************************/
src/GeographicLib/GeodesicLine.hpp:606
MethodBadUnits
src/models/FGAuxiliary.cpp:476
MethodBeginDestroy
UnrealEngine/Plugins/JSBSimFlightDynamicsModel/Source/JSBSimFlightDynamicsModel/Private/JSBSimMovementComponent.cpp:405
MethodBeginPlay
UnrealEngine/Plugins/JSBSimFlightDynamicsModel/Source/JSBSimFlightDynamicsModel/Private/JSBSimMovementComponent.cpp:413
MethodBeta
src/math/FGStateSpace.h:463
MethodBias
src/models/flight_control/FGActuator.cpp:198
MethodBias
src/models/flight_control/FGSensor.cpp:207
MethodBindModel
src/models/propulsion/FGTransmission.cpp:136
MethodBiplane
utils/aeromatic++/AeroBiplane.cpp:33
MethodBufferLogger
src/input_output/FGLog.cpp:62
MethodBuildPropertyCatalog
src/FGFDMExec.cpp:1083
MethodBuildStabilityTransformMatrices
src/models/FGAerodynamics.cpp:644
MethodC1f
The coefficients C1[l] in the Fourier expansion of B1
src/GeographicLib/Geodesic.cpp:983
MethodC1pf
The coefficients C1p[l] in the Fourier expansion of B1p
src/GeographicLib/Geodesic.cpp:1089
MethodC2f
The coefficients C2[l] in the Fourier expansion of B2
src/GeographicLib/Geodesic.cpp:1228
MethodC3coeff
The coefficients C3[l] in the Fourier expansion of B3
src/GeographicLib/Geodesic.cpp:1436
MethodC4coeff
src/GeographicLib/Geodesic.cpp:1641
MethodCNumericLocale
src/input_output/string_utilities.cpp:65
MethodCOG
src/math/FGStateSpace.h:901
MethodCableControls
utils/aeromatic++/Systems/Controls.h:41
MethodCalcFuelNeed
src/models/propulsion/FGTurbine.cpp:384
MethodCalcFuelNeed
src/models/propulsion/FGElectric.cpp:110
MethodCalcFuelNeed
src/models/propulsion/FGBrushLessDCMotor.h:91
MethodCalcFuelNeed
src/models/propulsion/FGTurboProp.cpp:425
MethodCalcFuelNeed
src/models/propulsion/FGRocket.cpp:222
MethodCalcFuelNeed
src/models/propulsion/FGEngine.cpp:93
MethodCalcOxidizerNeed
src/models/propulsion/FGEngine.h:181
MethodCalcRotorState
src/models/propulsion/FGRotor.cpp:604
MethodCalculate
src/models/FGAtmosphere.cpp:146
MethodCalculate
src/models/atmosphere/FGMars.cpp:70
MethodCalculate
src/models/atmosphere/FGMSIS.cpp:125
MethodCalculate
src/models/atmosphere/FGStandardAtmosphere.cpp:182
MethodCalculate
src/models/propulsion/FGTurbine.cpp:109
MethodCalculate
src/models/propulsion/FGRotor.cpp:675
MethodCalculate
src/models/propulsion/FGTank.cpp:345
MethodCalculate
src/models/propulsion/FGThruster.h:87
MethodCalculate
src/models/propulsion/FGPiston.cpp:480
MethodCalculate
src/models/propulsion/FGElectric.cpp:86
MethodCalculate
src/models/propulsion/FGNozzle.cpp:78
MethodCalculate
basically P = Q*w and Q_Engine + (-Q_Rotor) = J * dw/dt, J = Moment
src/models/propulsion/FGTransmission.cpp:73
MethodCalculate
src/models/propulsion/FGTurboProp.cpp:182
MethodCalculate
src/models/propulsion/FGPropeller.cpp:212
MethodCalculate
src/models/propulsion/FGRocket.cpp:156
MethodCalculate
src/models/propulsion/FGBrushLessDCMotor.cpp:124
MethodCalculateDensityAltitude
src/models/atmosphere/FGStandardAtmosphere.cpp:532
MethodCalculateDynamicFilters
src/models/flight_control/FGFilter.cpp:112
MethodCalculateFrictionForces
src/models/FGAccelerations.cpp:233
MethodCalculateInertialVelocity
src/models/FGPropagate.cpp:319
MethodCalculateInertias
src/models/propulsion/FGTank.cpp:379
MethodCalculateLapseRates
src/models/atmosphere/FGStandardAtmosphere.cpp:460
MethodCalculatePQRdot
src/models/FGAccelerations.cpp:139
MethodCalculatePhiWFromTargetNlfTurn
src/initialization/FGTrimAnalysis.cpp:774
MethodCalculatePressureAltitude
src/models/atmosphere/FGStandardAtmosphere.cpp:563
MethodCalculatePressureBreakpoints
src/models/atmosphere/FGStandardAtmosphere.cpp:477
MethodCalculateQuatdot
src/models/FGPropagate.cpp:306
MethodCalculateSLSoundSpeedAndDensity
src/models/atmosphere/FGStandardAtmosphere.cpp:238
MethodCalculateStdDensityBreakpoints
src/models/atmosphere/FGStandardAtmosphere.cpp:523
MethodCalculateTransformMatrix
src/models/flight_control/FGSensorOrientation.h:105
MethodCalculateUVW
src/models/FGPropagate.cpp:329
← previousnext →1,101–1,200 of 4,135, ranked by callers