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

⨍ Functions 4,135◇ Types & classes 724

↓ 3 callersFunctionunsignedCharToPrintable

src/simgear/xml/xmlparse.c:8681

↓ 3 callersMethoduntie

src/input_output/FGPropertyManager.h:414

↓ 3 callersFunctionwrap_last_line

(txt: str, indent: str)

python/Doxy2PyDocStrings.py:33

↓ 2 callersMethodAddAttribute

src/input_output/FGXMLElement.cpp:706

↓ 2 callersMethodAxisReport

src/initialization/FGTrimAxis.cpp:295

↓ 2 callersMethodCalcFuelNeed

src/models/propulsion/FGPiston.cpp:536

↓ 2 callersFunctionCalculateDensityAltitude

Calculates the density altitude given any temperature or pressure bias. Calculated density for the specified geometric altitude given any temperature

src/models/FGAtmosphere.h:254

↓ 2 callersFunctionCelsiusToKelvin

Converts from degrees Celsius to degrees Kelvin * @param celsius The temperature in degrees Celsius. * @return The temperature in Kelvin. */

src/FGJSBBase.h:235

↓ 2 callersMethodCheckRateValue

(self, fdm, rate_value)

tests/TestActuator.py:68

↓ 2 callersMethodCopyOutputsFromJSBSim

%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

matlab/JSBSimInterface.cpp:297

↓ 2 callersMethodDisable

Disables the input generation for all input instances.

src/models/FGInput.cpp:217

↓ 2 callersMethodDoTrim

src/FGFDMExec.cpp:1330

↓ 2 callersMethodDumpState

src/models/FGPropagate.cpp:708

↓ 2 callersFunctionEnable

Enables the output generation for all output instances.

src/models/FGOutput.h:180

↓ 2 callersMethodEnable

Enables the input generation for all input instances.

src/models/FGInput.cpp:209

↓ 2 callersMethodFGLinearization

src/initialization/FGLinearization.cpp:26

↓ 2 callersFunctionFGParameterValue

src/math/FGParameterValue.h:78

↓ 2 callersFunctionFMAX

examples/FlightGear.cxx:81

↓ 2 callersFunctionFlush

Ends the current log record and commits any buffered output.

src/input_output/FGLog.h:138

↓ 2 callersMethodFormat

src/input_output/FGLog.cpp:108

↓ 2 callersFunctionGenDistance

* The distance or arc length to point 3. * * @param[in] arcmode boolean flag determining the meaning of returned * value. * @ret

src/GeographicLib/GeodesicLine.hpp:684

↓ 2 callersFunctionGetAGLevel

Compute the altitude above ground. The altitude depends on location l. @param l location @param contact Contact point location below

src/input_output/FGGroundCallback.h:93

↓ 2 callersMethodGetAeroFunctionStrings

src/models/FGAerodynamics.cpp:535

↓ 2 callersMethodGetAeroFunctionValues

src/models/FGAerodynamics.cpp:567

↓ 2 callersFunctionGetClimbRateFpsIC

Gets the initial climb rate. @return Initial rate of climb in feet/second */

src/initialization/FGInitialCondition.h:520

↓ 2 callersMethodGetComponent

Retrieves a specific component.

src/models/FGFCSChannel.h:99

↓ 2 callersMethodGetComponentStrings

src/models/FGFCS.cpp:649

↓ 2 callersMethodGetComponentValues

src/models/FGFCS.cpp:672

↓ 2 callersMethodGetCranking

src/models/propulsion/FGEngine.h:153

↓ 2 callersFunctionGetDensity

@name Density access functions. @{ Returns the density in slugs/ft^3. This function may only be used if Run() is called first. */

src/models/FGAtmosphere.h:167

↓ 2 callersMethodGetEGT

src/models/propulsion/FGPiston.h:241

↓ 2 callersMethodGetElement

src/math/FGFunction.cpp:65

↓ 2 callersMethodGetGroundReactionStrings

src/models/FGGroundReactions.cpp:160

↓ 2 callersMethodGetGroundReactionValues

src/models/FGGroundReactions.cpp:200

↓ 2 callersFunctionGetID

utils/simplot/main.cpp:325

↓ 2 callersMethodGetIgnition

src/models/propulsion/FGTurbine.h:203

↓ 2 callersMethodGetIxx

Retrieves the propeller moment of inertia

src/models/propulsion/FGPropeller.h:241

↓ 2 callersFunctionGetLineNumber

Returns the line number at which the element has been defined. @return the line number */

src/input_output/FGXMLElement.h:230

↓ 2 callersFunctionGetLocationY

src/models/propulsion/FGTank.h:307

↓ 2 callersFunctionGetLocationZ

src/models/propulsion/FGTank.h:308

↓ 2 callersMethodGetMagnetos

src/models/propulsion/FGPiston.h:242

↓ 2 callersMethodGetN2

src/models/propulsion/FGTurbine.h:209

↓ 2 callersFunctionGetName

src/math/FGTable.h:416

↓ 2 callersMethodGetName

src/models/propulsion/FGTurbine.h:331

↓ 2 callersMethodGetNumComponents

Returns the number of components in the channel.

src/models/FGFCSChannel.h:97

↓ 2 callersFunctionGetNumEngines

Retrieves the number of engines defined for the aircraft.

src/models/FGPropulsion.h:126

↓ 2 callersMethodGetNumSourceTanks

src/models/propulsion/FGEngine.h:192

↓ 2 callersMethodGetOutput

src/models/flight_control/FGFCSComponent.h:94

↓ 2 callersMethodGetOutputName

src/models/flight_control/FGSwitch.h:165

↓ 2 callersMethodGetPhiRad

Gets Euler angle phi @return phi [rad] */

src/initialization/FGTrimAnalysis.h:606

↓ 2 callersMethodGetPitch

Retrieves the pitch of the propeller in degrees.

src/models/propulsion/FGPropeller.h:232

↓ 2 callersFunctionGetPointmassInertia

Computes the inertia contribution of a pointmass. Computes and returns the inertia matrix of a pointmass of mass slugs at the given vector

src/models/FGMassBalance.h:161

↓ 2 callersFunctionGetPrintableName

src/input_output/FGPropertyManager.cpp:96

↓ 2 callersMethodGetPropulsionStrings

src/models/FGPropulsion.cpp:493

↓ 2 callersMethodGetPropulsionValues

src/models/FGPropulsion.cpp:522

↓ 2 callersFunctionGetRelativeName

src/input_output/FGPropertyManager.cpp:133

↓ 2 callersMethodGetSolid

Gets the surface is a solid flag value

src/models/FGSurface.h:107

↓ 2 callersMethodGetSourceTank

src/models/propulsion/FGEngine.cpp:103

↓ 2 callersMethodGetStateName

src/initialization/FGTrimAxis.h:113

↓ 2 callersMethodGetTerrainElevation

src/models/FGPropagate.cpp:607

↓ 2 callersMethodGetTurbDirection

src/models/atmosphere/FGWinds.h:264

↓ 2 callersMethodGetTurbMagnitude

src/models/atmosphere/FGWinds.h:263

↓ 2 callersMethodGetTurbPQR

src/models/atmosphere/FGWinds.h:262

↓ 2 callersMethodGetVariables

tests/TestInitialConditions.py:243

↓ 2 callersMethodGetVolume

Get the current volume of the ballonet @return volume in ft<sup>3</sup>. */

src/models/FGGasCell.h:332

↓ 2 callersMethodGetWindDirDegIC

src/initialization/FGInitialCondition.cpp:923

↓ 2 callersFunctionHasAttribute

Determines if an element has the supplied attribute. @param key specifies the attribute key to retrieve the value of. @return true or fals

src/input_output/FGXMLElement.h:155

↓ 2 callersMethodHasTest

src/models/flight_control/FGDistributor.h:187

↓ 2 callersMethodInitializeDerivatives

src/models/FGPropagate.cpp:190

↓ 2 callersFunctionIntegrationSuspended

Returns the simulation suspension state. @return true if suspended, false if executing */

src/FGFDMExec.h:567

↓ 2 callersMethodIsInitFile

src/JSBSim.cpp:178

↓ 2 callersFunctionKelvinToCelsius

Converts from degrees Kelvin to degrees Celsius * @param celsius The temperature in degrees Kelvin. * @return The temperature in Celsius. */

src/FGJSBBase.h:242

↓ 2 callersMethodLoadScript

(self, tree, script_path, prop_output_to_CSV=[])

tests/TestInitialConditions.py:123

↓ 2 callersFunctionLoadWinSockDLL

src/input_output/FGfdmSocket.cpp:80

↓ 2 callersFunctionLookupAxisName

src/math/FGTable.cpp:141

↓ 2 callersFunctionMagnitude

Length of the vector. Compute and return the euclidean norm of this vector. */

src/math/FGQuaternion.h:460

↓ 2 callersFunctionMakeArbitraryPlot

utils/simplot/prep_plot.cpp:553

↓ 2 callersMethodPhiOrPsiAndGimbalLock

(self, var, vars)

tests/TestInitialConditions.py:347

↓ 2 callersFunctionReadInertiaMatrix

src/models/FGMassBalance.cpp:101

↓ 2 callersMethodReceive

src/input_output/FGfdmSocket.cpp:273

↓ 2 callersMethodRun

src/initialization/FGTrimAnalysisControl.cpp:438

↓ 2 callersMethodSRand

src/FGFDMExec.cpp:1361

↓ 2 callersMethodSetActiveEngine

src/models/FGPropulsion.cpp:743

↓ 2 callersFunctionSetAnglesToBody

src/models/propulsion/FGForce.h:287

↓ 2 callersMethodSetAugmentation

src/models/propulsion/FGTurbine.h:224

↓ 2 callersMethodSetCondition

src/models/propulsion/FGTurboProp.h:134

↓ 2 callersMethodSetContents

src/models/propulsion/FGTank.cpp:322

↓ 2 callersMethodSetDaLPos

src/models/FGFCS.cpp:186

↓ 2 callersMethodSetDaRPos

src/models/FGFCS.cpp:205

↓ 2 callersMethodSetDePos

src/models/FGFCS.cpp:224

↓ 2 callersMethodSetDelimiter

Set the delimiter. @param delim delimiter of the output values (most likely a comma or a tab) */

src/input_output/FGOutputTextFile.h:75

↓ 2 callersMethodSetDfPos

src/models/FGFCS.cpp:262

↓ 2 callersMethodSetDrPos

src/models/FGFCS.cpp:243

↓ 2 callersMethodSetFeatherCmd

src/models/FGFCS.cpp:453

↓ 2 callersMethodSetGeneratorPower

src/models/propulsion/FGTurboProp.h:133

↓ 2 callersMethodSetIgnition

src/models/propulsion/FGTurbine.h:223

↓ 2 callersMethodSetInitialState

src/models/FGAuxiliary.cpp:129

↓ 2 callersMethodSetLength

src/models/FGMassBalance.h:292

↓ 2 callersFunctionSetLocation

Normal point of application, JSBsim structural coords (inches, x +back, y +right, z +up)

src/models/propulsion/FGForce.h:241

↓ 2 callersMethodSetLongitudeRadIC

src/initialization/FGInitialCondition.cpp:905

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