Uses of Class
agi.foundation.geometry.Axes

Packages that use Axes

Package	Description
agi.foundation.aircraftpropagation	Contains types for propagating an aircraft through various maneuvers subject to flight phase performance models and wind effects.
agi.foundation.ccsds	Contains types for interoperating with data formats supported by The Consultative Committee for Space Data Systems (CCSDS).
agi.foundation.celestial	Contains types used in modeling characteristics of celestial objects and celestial phenomena.
agi.foundation.cesium	Contains types used for defining graphical properties of definitional objects to be written out as CZML.
agi.foundation.communications	Contains types for representing electromagnetic signals and propagating them along communication links.
agi.foundation.communications.antennas	Contains types for representing antennas, defining gain patterns, and processing electromagnetic signals.
agi.foundation.coordinates	Contains types for quantifying and converting between various coordinate representations.
agi.foundation.geometry	Contains types for expressing the motion of fundamental geometric objects such as points, axes, and reference frames; the manner in which they are related; and transformations between representations.
agi.foundation.graphics	Provides commonly used and instantiated graphics types related to 3D scene management, terrain and imagery, and more.
agi.foundation.navigation.advanced	Contains types used in GPS communications modeling.
agi.foundation.numericalmethods	Contains general numerical algorithms.
agi.foundation.platforms	Contains types used in modeling various mechanical platforms such as satellites, facilities, aircraft, etc.
agi.foundation.propagators	Contains types used in producing the state of an object from a known element set.
agi.foundation.segmentpropagation	Contains types for modeling a trajectory in segments, where the type of propagation varies for each segment.
agi.foundation.stk	Contains types for interoperating with the STK desktop application and related data.
agi.foundation.tracking	Contains types for acquiring, analyzing and archiving dynamic data, such as those found in real-time feeds or simulation environments.

Uses of Axes in agi.foundation.aircraftpropagation

Methods in agi.foundation.aircraftpropagation that return Axes

Modifier and Type	Method and Description
Axes	SimpleFixedWingCoordinatedFlight.getBodyAxes() Gets an Axes aligned with the body of the aircraft.

Uses of Axes in agi.foundation.ccsds

Methods in agi.foundation.ccsds that return types with arguments of type Axes

Modifier and Type	Method and Description
DateMotionCollection1<Axes>	CcsdsOrbitEphemerisMessageSegment.getCovarianceAxes() Gets or sets a collection containing the axes of the covariance data.

Method parameters in agi.foundation.ccsds with type arguments of type Axes

Modifier and Type	Method and Description
void	CcsdsOrbitEphemerisMessageSegment.setCovarianceAxes(DateMotionCollection1<Axes> value) Gets or sets a collection containing the axes of the covariance data.

Uses of Axes in agi.foundation.celestial

Subclasses of Axes in agi.foundation.celestial

Modifier and Type	Class and Description
class	CentralBodyInertialAxes This class provides the Axes based on the STK definition of a CentralBody's Inertial Axes.
class	IauOrientationAxes The Axes representing the orientation of a CentralBody as represented by the data from the IAU/IAG Working Group reports on rotational elements expressed in the InertialFrame (get / set)Axes (get / set) of the SolarSystemBarycenter.

Methods in agi.foundation.celestial that return Axes

Modifier and Type	Method and Description
Axes	ReactionWheelTorque.getBodyAxes() Gets the body axes of the spacecraft using the reaction wheel.
Axes	OffAxisTorque.getBodyAxes() Gets the body axes of the thrusting vehicle.
Axes	NPlateSolarRadiationForce.getBodyAxes() Gets the axes defining the orientation of the spacecraft body.
Axes	NPlateAtmosphericDragForce.getBodyAxes() Gets the axes defining the orientation of the spacecraft body.
Axes	MagneticCoilTorque.getBodyAxes() Gets the body axes of the spacecraft.
Axes	GravityGradientTorque.getBodyAxes() Gets the body axes of the gravity-gradient satellite.
abstract Axes	TorqueEvaluator.getDefinedIn() Gets the Axes in which this torque is defined.
abstract Axes	ForceEvaluator.getDefinedIn() Gets the Axes in which this force is defined.
Axes	SimpleSolarRadiationForce.getDefinedInAxes() Gets the axes in which this force is defined.
Axes	NPlateSolarRadiationForce.getDefinedInAxes() Gets the axes in which this force is defined.
Axes	NPlateAtmosphericDragForce.getDefinedInAxes() Gets the Axes in which this force is defined.
Axes	ConstantTorque.getDefinedInAxes() Gets the axes that the torque is represented in.
Axes	ConstantForce.getDefinedInAxes() Gets the axes that the force is represented in.
Axes	AtmosphericDragForce.getDefinedInAxes() Gets the Axes in which this force is defined.
Axes	ContinuousThrustForceModel.getIntegrationAxes() Gets the axes that this force model will be integrated in.
Axes	CentralBody.getOrientationAxes() Gets the axes that describes the orientation of the object.
Axes	SolarRadiationBodyPlate.getPointingAxes() Gets the axes that are used to define the pointing of this plate.
Axes	DragBodyPlate.getPointingAxes() Gets the axes that are used to define the pointing of this plate.

Methods in agi.foundation.celestial with parameters of type Axes

Modifier and Type	Method and Description
protected boolean	IauOrientationAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	CentralBodyInertialAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
static Vector	ContinuousThrustForceModel.createIspThrustVector(Scalar isp, Scalar massFlowRate, Axes burnAxes, Cartesian thrustDirection) Creates a thrust Vector where the thrust is computed from the isp, and massFlowRate pointing in the thrustDirection in the specified burnAxes.
static MagneticCoilTorque	MagneticCoilTorque.createMagneticCoilTorqueUsingIgrfCofModel(String filename, Point bodyCenterOfMass, double numberOfLoops, Scalar current, Vector directedArea, Axes bodyAxes) Creates a new magnetic coil torque that uses an InternationalGeomagneticReferenceFieldVector to describe the magnetic field and a Point to describe the position of the spacecraft.
static MagneticCoilTorque	MagneticCoilTorque.createMagneticCoilTorqueUsingIgrfTxtModel(String filename, Point bodyCenterOfMass, double numberOfLoops, Scalar current, Vector directedArea, Axes bodyAxes) Creates a new magnetic coil torque that uses an InternationalGeomagneticReferenceFieldVector to describe the magnetic field and a Point to describe the position of the spacecraft.
static MagneticCoilTorque	MagneticCoilTorque.createMagneticCoilTorqueUsingWmmModel(String filename, Point bodyCenterOfMass, double numberOfLoops, Scalar current, Vector directedArea, Axes bodyAxes) Creates a new magnetic coil torque that uses a WorldMagneticModelVector to describe the magnetic field and a Point to describe the position of the spacecraft.
static Vector	ContinuousThrustForceModel.createVeThrustVector(Scalar exhaustSpeed, Scalar massFlowRate, Axes burnAxes, Vector thrustDirection) Creates a thrust Vector where the thrust is computed from the exhaustSpeed, and massFlowRate pointing in the thrustDirection in the specified burnAxes.
Scalar	SolarRadiationPlate.getSwitchingScalar(Axes bodyAxes, Vector toSunVector) Gets a scalar that is used to determine whether this plate is facing a direction within 90 degrees of the incident sunlight direction at a given time.
Scalar	DragTwoDofSolarPanelPlate.getSwitchingScalar(Axes bodyAxes, Vector toSunVector, Vector velocity) Gets a scalar that is used to determine whether this plate is facing a direction within 90 degrees of the incident atmosphere direction at a given time.
abstract Scalar	DragPlate.getSwitchingScalar(Axes bodyAxes, Vector toSunVector, Vector velocity) Gets a scalar that is used to determine whether this plate is facing a direction within 90 degrees of the incident atmosphere direction at a given time.
Scalar	DragOneDofSolarPanelPlate.getSwitchingScalar(Axes bodyAxes, Vector toSunVector, Vector velocity) Gets a scalar that is used to determine whether this plate is facing a direction within 90 degrees of the incident atmosphere direction at a given time.
Scalar	DragBodyPlate.getSwitchingScalar(Axes bodyAxes, Vector toSunVector, Vector velocity) Gets a scalar that is used to determine whether this plate is facing a direction within 90 degrees of the incident atmosphere direction at a given time.
Vector	SolarRadiationTwoDofSolarPanelPlate.getUnitNormalVector(Axes bodyAxes, Vector toSunVector) Gets the unit normal vector of the plate that describes its pointing and is used to determine how much of the plate's ReferenceArea (get / set) is directed toward the Sun (for SolarRadiationPlates) or toward the incoming atmosphere (for DragPlates).
Vector	SolarRadiationOneDofSolarPanelPlate.getUnitNormalVector(Axes bodyAxes, Vector toSunVector) Gets the unit normal vector of the plate that describes its pointing and is used to determine how much of the plate's ReferenceArea (get / set) is directed toward the Sun (for SolarRadiationPlates) or toward the incoming atmosphere (for DragPlates).
Vector	SolarRadiationBodyPlate.getUnitNormalVector(Axes bodyAxes, Vector toSunVector) Gets the unit normal vector of the plate that describes its pointing and is used to determine how much of the plate's ReferenceArea (get / set) is directed toward the Sun (for SolarRadiationPlates) or toward the incoming atmosphere (for DragPlates).
abstract Vector	IndividualPlateModel.getUnitNormalVector(Axes bodyAxes, Vector toSunVector) Gets the unit normal vector of the plate that describes its pointing and is used to determine how much of the plate's ReferenceArea (get / set) is directed toward the Sun (for SolarRadiationPlates) or toward the incoming atmosphere (for DragPlates).
Vector	DragTwoDofSolarPanelPlate.getUnitNormalVector(Axes bodyAxes, Vector toSunVector) Gets the unit normal vector of the plate that describes its pointing and is used to determine how much of the plate's ReferenceArea (get / set) is directed toward the Sun (for SolarRadiationPlates) or toward the incoming atmosphere (for DragPlates).
Vector	DragOneDofSolarPanelPlate.getUnitNormalVector(Axes bodyAxes, Vector toSunVector) Gets the unit normal vector of the plate that describes its pointing and is used to determine how much of the plate's ReferenceArea (get / set) is directed toward the Sun (for SolarRadiationPlates) or toward the incoming atmosphere (for DragPlates).
Vector	DragBodyPlate.getUnitNormalVector(Axes bodyAxes, Vector toSunVector) Gets the unit normal vector of the plate that describes its pointing and is used to determine how much of the plate's ReferenceArea (get / set) is directed toward the Sun (for SolarRadiationPlates) or toward the incoming atmosphere (for DragPlates).
void	ReactionWheelTorque.setBodyAxes(Axes value) Sets the body axes of the spacecraft using the reaction wheel.
void	OffAxisTorque.setBodyAxes(Axes value) Sets the body axes of the thrusting vehicle.
void	NPlateSolarRadiationForce.setBodyAxes(Axes value) Sets the axes defining the orientation of the spacecraft body.
void	NPlateAtmosphericDragForce.setBodyAxes(Axes value) Sets the axes defining the orientation of the spacecraft body.
void	MagneticCoilTorque.setBodyAxes(Axes value) Sets the body axes of the spacecraft.
void	GravityGradientTorque.setBodyAxes(Axes value) Sets the body axes of the gravity-gradient satellite.
void	ConstantTorque.setDefinedInAxes(Axes value) Sets the axes that the torque is represented in.
void	ConstantForce.setDefinedInAxes(Axes value) Sets the axes that the force is represented in.
void	ContinuousThrustForceModel.setIntegrationAxes(Axes value) Sets the axes that this force model will be integrated in.
void	SolarRadiationBodyPlate.setPointingAxes(Axes value) Sets the axes that are used to define the pointing of this plate.
void	DragBodyPlate.setPointingAxes(Axes value) Sets the axes that are used to define the pointing of this plate.

Constructors in agi.foundation.celestial with parameters of type Axes

Constructor and Description
ConstantForce(Axes definedInAxes, Cartesian force) Initializes a new instance of the class.
ConstantTorque(Axes definedInAxes, Cartesian torque) Initializes a new instance of the class.
ContinuousThrustForceModel(Vector thrustVector, Axes integrationAxes) Initialize a new instance.
ContinuousThrustForceModel(Vector thrustVector, Axes integrationAxes, boolean ignorePartials) Initialize a new instance.
DragBodyPlate(String plateName, String groupName, double referenceArea, UnitCartesian unitNormalCartesian, double dragCoefficient, Axes pointingAxes) Initializes a new instance.
GravityGradientTorque(Point bodyCenterOfMass, CentralBody centralBody, double gravitationalParameter, Matrix3By3Symmetric inertiaMatrix, Axes bodyAxes) Initializes the gravity-gradient torque model.
GravityGradientTorque(Point bodyCenterOfMass, Matrix3By3Symmetric inertiaMatrix, Axes bodyAxes) Initializes the gravity-gradient torque model.
MagneticCoilTorque(Vector magneticFieldVector, double numberOfLoops, Scalar current, Cartesian directedArea, Axes bodyAxes) Initializes the magnetic coil torque model.
MagneticCoilTorque(Vector magneticFieldVector, double numberOfLoops, Scalar current, Vector directedArea, Axes bodyAxes) Initializes the magnetic coil torque model.
NPlateAtmosphericDragForce(NPlateModel nPlateModel, Axes bodyAxes, ScalarAtmosphericDensity density, CentralBody illuminatingBody) Initializes a ForceModel describing the atmospheric drag force on an object.
NPlateSolarRadiationForce(NPlateModel nPlateModel, Axes bodyAxes, Point targetPoint) Initializes a ForceModel describing the solar radiation pressure force on an object.
NPlateSolarRadiationForce(NPlateModel nPlateModel, Axes bodyAxes, ScalarOccultation occultationFactor) Initializes a ForceModel describing the solar radiation pressure force on an object.
OffAxisTorque(Scalar thrustMagnitude, UnitCartesian thrustAxis, Cartesian offset, Axes bodyAxes) Initializes a model of the torque generated by a thruster that is not aligned with the center of mass of a vehicle.
OffAxisTorque(Vector thrustVector, Cartesian offset, Axes bodyAxes) Initializes a model of the torque generated by a thruster that is not aligned with the center of mass of a vehicle.
ReactionWheelTorque(Scalar spinMagnitude, UnitCartesian spinAxis, double spinAxisInertia, Axes bodyAxes) Initializes the reaction wheel torque model.
SolarRadiationBodyPlate(String plateName, String groupName, double referenceArea, UnitCartesian unitNormalCartesian, double specularReflectivity, double diffuseReflectivity, Axes pointingAxes) Initializes a new instance.

Uses of Axes in agi.foundation.cesium

Methods in agi.foundation.cesium that return Axes

Modifier and Type	Method and Description
Axes	AxesCesiumProperty.getAxes() Gets the axes.

Methods in agi.foundation.cesium with parameters of type Axes

Modifier and Type	Method and Description
void	AxesCesiumProperty.setAxes(Axes value) Sets the axes.
static AxesCesiumProperty	AxesCesiumProperty.toAxesCesiumProperty(Axes value) Converts a Axes to a AxesCesiumProperty.

Constructors in agi.foundation.cesium with parameters of type Axes

Constructor and Description
AxesCesiumProperty(Axes axes) Initializes a new instance with the provided Axes.

Uses of Axes in agi.foundation.communications

Methods in agi.foundation.communications that return Axes

Modifier and Type	Method and Description
Axes	PointScattererExtension.getSignalTransmissionAxes() Gets the Axes associated with signal transmission.

Methods in agi.foundation.communications with parameters of type Axes

Modifier and Type	Method and Description
abstract SignalPolarizationEvaluator	PolarizationSource.getPolarizationEvaluator(EvaluatorGroup group, Vector linkGeometry, Axes polarizationAxes) Gets an evaluator for evaluating polarization based on link geometry and polarization axes.
SignalPolarizationEvaluator	OrthogonalPolarizationSource.getPolarizationEvaluator(EvaluatorGroup group, Vector linkGeometry, Axes polarizationAxes) Gets an evaluator for evaluating polarization based on link geometry and polarization axes.
SignalPolarizationEvaluator	Ieee1979PolarizationSource.getPolarizationEvaluator(EvaluatorGroup group, Vector linkGeometry, Axes polarizationAxes) Gets an evaluator for evaluating polarization based on link geometry and polarization axes.
SignalPolarizationEvaluator	FrequencyDependentElectricFieldPolarizationSource.getPolarizationEvaluator(EvaluatorGroup group, Vector linkGeometry, Axes polarizationAxes) Gets an evaluator for evaluating polarization based on link geometry and polarization axes.
SignalPolarizationEvaluator	ConstantPolarizationSource.getPolarizationEvaluator(EvaluatorGroup group, Vector linkGeometry, Axes polarizationAxes) Gets an evaluator for evaluating polarization based on link geometry and polarization axes.

Constructors in agi.foundation.communications with parameters of type Axes

Constructor and Description
ComplexAnalogTransmitter(String name, Point locationPoint, Axes orientationAxes, RadioFrequencyGainPattern antennaGainPattern, Signal signalToTransmit) Creates a new instance, specifying all parameters.
ComplexAnalogTransmitter(String name, Point locationPoint, Axes orientationAxes, RadioFrequencyGainPattern antennaGainPattern, Signal signalToTransmit, PolarizationSource polarizationSource) Creates a new instance, specifying all parameters.
ComplexDigitalTransmitter(String name, Point locationPoint, Axes orientationAxes, DigitalModulation modulation, RadioFrequencyGainPattern antennaGainPattern, double carrierFrequency, double power, double dataRate, SignalDataCollection signalData) Creates a new instance from the specified parameters.
ComplexDigitalTransmitter(String name, Point locationPoint, Axes orientationAxes, DigitalModulation modulation, RadioFrequencyGainPattern antennaGainPattern, double carrierFrequency, double power, double dataRate, SignalDataCollection signalData, PolarizationSource polarizationSource) Creates a new instance from the specified parameters.
ComplexReceiver(String name, Point location, Axes orientation, Amplifier amplifier, RadioFrequencyGainPattern gainPattern) Creates a new instance specifying all parameters.
ComplexReceiver(String name, Point location, Axes orientation, Amplifier amplifier, RadioFrequencyGainPattern gainPattern, PolarizationSource polarizationSource) Creates a new instance specifying all parameters.
OpticalReceiver(String name, Point location, Axes orientation, Photodetector photodetector, OpticalGainPattern gainPattern) Creates a new instance specifying all parameters.
OpticalReceiver(String name, Point location, Axes orientation, Photodetector photodetector, OpticalGainPattern gainPattern, PolarizationSource polarizationSource) Creates a new instance specifying all parameters.
OpticalTransmitter(String name, Point locationPoint, Axes orientation, DigitalModulation modulation, OpticalGainPattern antennaGainPattern, double wavelength, double power, double dataRate, SignalDataCollection signalData) Creates a new instance specifying all parameters.
OpticalTransmitter(String name, Point locationPoint, Axes orientation, DigitalModulation modulation, OpticalGainPattern antennaGainPattern, double wavelength, double power, double dataRate, SignalDataCollection signalData, PolarizationSource polarizationSource) Creates a new instance specifying all parameters.
SimpleAnalogTransmitter(String name, Point location, Axes orientationAxes, double carrierFrequency, double effectiveIsotropicRadiatedPower, double bandwidth) Creates a new instance, specifying all parameters.
SimpleAnalogTransmitter(String name, Point location, Axes orientationAxes, double carrierFrequency, double effectiveIsotropicRadiatedPower, double bandwidth, PolarizationSource polarizationSource) Creates a new instance, specifying all parameters.
SimpleDigitalTransmitter(String name, Point locationPoint, Axes orientationAxes, double carrierFrequency, double effectiveIsotropicRadiatedPower, double dataRate) Creates a new instance from the specified parameters.
SimpleDigitalTransmitter(String name, Point locationPoint, Axes orientationAxes, double carrierFrequency, double effectiveIsotropicRadiatedPower, double dataRate, PolarizationSource polarizationSource) Creates a new instance from the specified parameters.
SimpleReceiver(String name, Point locationPoint, Axes orientationAxes, double gain, double noiseFactor, double targetFrequency, double filterBandwidth) Creates a new instance specifying all parameters.
SimpleReceiver(String name, Point locationPoint, Axes orientationAxes, double gain, double noiseFactor, double targetFrequency, double filterBandwidth, PolarizationSource polarizationSource) Creates a new instance specifying all parameters.
Transceiver(String name, Point inputAntennaLocationPoint, Axes inputAntennaOrientationAxes, RadioFrequencyGainPattern inputAntennaGainPattern, Point outputAntennaLocationPoint, Axes outputAntennaOrientationAxes, RadioFrequencyGainPattern outputAntennaGainPattern, DigitalModulation modulation, double gain, double noiseFactor, double carrierFrequency, SignalFilter filter) Creates a new instance specifying all properties.
Transceiver(String name, Point inputAntennaLocationPoint, Axes inputAntennaOrientationAxes, RadioFrequencyGainPattern inputAntennaGainPattern, PolarizationSource inputPolarizationSource, Point outputAntennaLocationPoint, Axes outputAntennaOrientationAxes, RadioFrequencyGainPattern outputAntennaGainPattern, PolarizationSource outputPolarizationSource, DigitalModulation modulation, double gain, double noiseFactor, double carrierFrequency, SignalFilter filter) Creates a new instance specifying all properties.
Transponder(String name, Point inputAntennaLocationPoint, Axes inputAntennaOrientationAxes, RadioFrequencyGainPattern inputAntennaGainPattern, Point outputAntennaLocationPoint, Axes outputAntennaOrientationAxes, RadioFrequencyGainPattern outputAntennaGainPattern, double gain, double noiseFactor, SignalFilter filter) Creates a new instance specifying all properties.
Transponder(String name, Point inputAntennaLocationPoint, Axes inputAntennaOrientationAxes, RadioFrequencyGainPattern inputAntennaGainPattern, PolarizationSource inputPolarizationSource, Point outputAntennaLocationPoint, Axes outputAntennaOrientationAxes, RadioFrequencyGainPattern outputAntennaGainPattern, PolarizationSource outputPolarizationSource, double gain, double noiseFactor, SignalFilter filter) Creates a new instance specifying all properties.

Uses of Axes in agi.foundation.communications.antennas

Methods in agi.foundation.communications.antennas that return Axes

Modifier and Type	Method and Description
Axes	ISignalTransmissionService.getSignalTransmissionAxes() Gets the Axes associated with signal transmission.
Axes	BaseTransmittingAntennaExtension.getSignalTransmissionAxes() Gets the Axes associated with signal transmission.

Methods in agi.foundation.communications.antennas with parameters of type Axes

Modifier and Type	Method and Description
Evaluator<Double>	IsotropicGainPattern.getAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, Signal sampleSignal) Get an evaluator for the gain that would be applied to the given sample signal.
Evaluator<Double>	IAntennaGainService.getAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, Signal sampleSignal) Get an evaluator for the gain that would be applied to the given sample signal.
Evaluator<Double>	BaseGainPattern.getAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, Signal sampleSignal) Get an evaluator for the gain that would be applied to the given sample signal based on the given geometry.
Evaluator<Double>	BaseGainPattern.getAntennaGainEvaluator(Vector linkDirection, Axes antennaAxes, Signal sampleSignal) Get an evaluator for the gain that would be applied to the given sample signal based on the given geometry.
SignalEvaluator	GpsSatelliteAntennaPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	FrpaGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	UniformRectangularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	UniformCircularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	SquareHornGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	SincExponentRectangularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	SincExponentCircularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	RectangularBeamGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	PhasedArrayGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of input signals based on link geometry and the gain pattern.
SignalEvaluator	PencilBeamGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ParabolicGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRS731Version1GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRS672Version4GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRS580Version6GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRS465Version6GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRS465Version5GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRS1528R13GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRS1528R12GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRF1245Version3GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRF1245Version1GainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRBO1213Version1CrossPolarGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	ItuRBO1213Version1CoPolarGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	IsotropicGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Gets the evaluator for the specified inputSignal since no gain is applied.
SignalEvaluator	IAntennaGainService.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of input signals based on link geometry and the gain pattern.
SignalEvaluator	HemisphericalGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	HelicalGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	GaussianOpticalGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	GaussianGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	FrequencyDependentElectricFieldGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	DipoleGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CustomGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CosineSquaredRectangularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CosineSquaredPedestalRectangularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CosineSquaredPedestalCircularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CosineSquaredCircularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CosineRectangularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CosinePedestalRectangularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CosinePedestalCircularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	CosineCircularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	BesselEnvelopeCircularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
SignalEvaluator	BesselCircularApertureGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of signals based on link geometry and this gain pattern.
abstract SignalEvaluator	BaseGainPattern.getApplyAntennaGainEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes, ISignalSource inputSignal, SignalPropagationGraph graph) Get an evaluator which can modify a set of input signals based on link geometry and the gain pattern.
abstract BeamformerWeightsEvaluator	PhasedArrayBeamformer.getBeamWeightsEvaluator(EvaluatorGroup group, ISignalSource inputSignal, Vector linkDirection, Axes antennaAxes, List<PhasedArrayElement> elementPattern) Gets a BeamformerWeightsEvaluator which when evaluated produces a ComplexMatrix of element weights.
BeamformerWeightsEvaluator	MinimumVarianceDistortionlessResponseBeamformer.getBeamWeightsEvaluator(EvaluatorGroup group, ISignalSource inputSignal, Vector linkDirection, Axes antennaAxes, List<PhasedArrayElement> elementPattern) Gets a BeamformerWeightsEvaluator which when evaluated produces a ComplexMatrix of element weights.
DirectionsEvaluator	StaticDirectionsProvider.getDirectionsEvaluator(EvaluatorGroup group, ISignalSource inputSignal, Vector linkDirection, Axes antennaAxes) Gets an evaluator for evaluating directions based on an input signal, link direction vector, and antenna axes.
DirectionsEvaluator	LinkDirectionsProvider.getDirectionsEvaluator(EvaluatorGroup group, ISignalSource inputSignal, Vector linkDirection, Axes antennaAxes) Gets an evaluator for evaluating directions based on an input signal, link direction vector, and antenna axes.
abstract DirectionsEvaluator	DirectionsProvider.getDirectionsEvaluator(EvaluatorGroup group, ISignalSource inputSignal, Vector linkDirection, Axes antennaAxes) Gets an evaluator for evaluating directions based on an input signal, link direction vector, and antenna axes.
abstract ScalarEvaluator	PhasedArrayElementFactor.getEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes) Gets a ScalarEvaluator for evaluating the element factor based on the link direction vector and the antenna axes.
ScalarEvaluator	CosineExponentElementFactor.getEvaluator(EvaluatorGroup group, Vector linkDirection, Axes antennaAxes) Gets a ScalarEvaluator which computes an element factor using the equation 4 * PI * elementArea * direction.Z^(cosineExponent), where direction.Z is the z component of the unit vector in the link direction and cosineExponent and elementArea are given by the CosineExponent (get / set) and ElementArea (get / set) properties, respectively.

Uses of Axes in agi.foundation.coordinates

Methods in agi.foundation.coordinates that return Axes

Modifier and Type	Method and Description
Axes	AxesAdapter.getCurrentAxes() Gets the Axes that the ElementIdentification (get / set) in the state will be in once the state is adapted.
Axes	AxesAdapter.getPreviousAxes() Gets the Axes that the ElementIdentification (get / set) in the previous state is defined in.

Methods in agi.foundation.coordinates with parameters of type Axes

Modifier and Type	Method and Description
void	AxesAdapter.setCurrentAxes(Axes value) Sets the Axes that the ElementIdentification (get / set) in the state will be in once the state is adapted.
void	AxesAdapter.setPreviousAxes(Axes value) Sets the Axes that the ElementIdentification (get / set) in the previous state is defined in.

Constructors in agi.foundation.coordinates with parameters of type Axes

Constructor and Description
AxesAdapter(String elementIdentification, Axes currentAxes) Initializes a new instance.

Uses of Axes in agi.foundation.geometry

Subclasses of Axes in agi.foundation.geometry

Modifier and Type	Class and Description
class	AxesAlignedConstrained A set of axes with the one axis aligned with the Principal (get / set) direction vector and another axis constrained to minimize the angular separation from the Reference (get / set) vector.
class	AxesAlongTerrain An Axes defined by the surface normal to the terrain surface.
class	AxesBPlane The axes that a VectorBPlane are computed in.
class	AxesEastNorthUp The set of axes defined by the local East, North, and Up directions at a point with respect to the shape of a central body as the point moves over time.
class	AxesFixedAtJulianDate A set of Axes which is defined by the instantaneous orientation of another set of axes at a specified JulianDate.
class	AxesFixedOffset An axes whose orientation does not change with respect to the axes in which it is defined.
class	AxesFromArchive<TEntity extends IEntityIdentifier & IEntityLastUpdate> An Axes whose orientation is defined by archived tracking data.
class	AxesFromBankAngle An Axes defining a first order representation for an aircraft in steady flight with the bank angles specified by changes in the horizontal acceleration vector.
class	AxesInAxes An axes which is effectively equivalent to another axes but is defined in a third axes.
class	AxesInPointsAxes An axes observed in the axes in which a point is defined.
class	AxesInterpolator A set of Axes that is defined with respect to a set of reference axes by an interpolator which can evaluate the Axes over time.
class	AxesInVectorsAxes An axes observed in the axes in which a vector is defined.
class	AxesLinearRate An axes whose orientation changes with respect to the axes in which it is defined by rotating at a linearly increasing or decreasing rate about a defined spin axis.
class	AxesLocalVerticalLocalHorizontal The Local Vertical, Local Horizontal (LVLH) axes which follow the motion of a given point over time.
class	AxesNorthEastDown The set of axes defined by the local North, East, and Down directions at a point with respect to the shape of a central body as the point moves over time.
class	AxesPropagationParameter Represents an Axes which in turns represents the attitude and angular velocity in an integration state.
class	AxesTargetingLink An Axes which orients itself so that its Z-axis is aligned along a link, pointing from one platform to another, and its X-axis is constrained toward a reference vector.
class	AxesVehicleVelocityLocalHorizontal The Vehicle Velocity, Local Horizontal (VVLH) axes which follow the motion of a given point over time.
class	AxesVelocityOrbitNormal These Axes will have its X axis be aligned with the velocity vector of the given point and the Y axis will be constrained to the orbit normal vector.
class	CompositeAxes A Axes that is defined by a collection of intervals, where the data associated with each interval is a another Axes representing the orientation for that interval.
class	EntityAxes<TEntity extends IEntityOrientation> An Axes that obtains its value from a tracking entity implementing IEntityOrientation.
class	ServiceProviderAxes An Axes that can be used to refer to the current OrientationAxes (get) of an IServiceProvider, whatever it is at the time that this axes is evaluated.

Methods in agi.foundation.geometry that return Axes

Modifier and Type	Method and Description
Axes	InternationalTerrestrialReferenceFrameTransformer.convertAxes(Axes fromAxes, Axes axes) Converts an Axes such that the ITRF transformation is applied when it is evaluated.
static Axes	InternationalTerrestrialReferenceFrameTransformer.convertAxes(EarthCentralBody earth, Axes axes, String toFrame) Converts an Axes such that an ITRF transformation is applied when it is evaluated.
static Axes	InternationalTerrestrialReferenceFrameTransformer.convertAxes(EarthCentralBody earth, Axes axes, String toFrame, ArrayList<InternationalTerrestrialReferenceFrameTransformer> itrfList) Converts an Axes such that an ITRF transformation is applied when it is evaluated.
Axes	VectorDerivative.getAxes() Gets the axes.
Axes	ReferenceFrame.getAxes() Gets the axes of the reference frame.
static Axes	AxesHelper.getAxes(IServiceProvider provider) Gets the Axes from the IOrientationAxesService provided by an object.
static Axes	AxesHelper.getAxes(IServiceProvider provider, String exceptionMessage) Gets the Axes from the IOrientationAxesService provided by an object.
Axes	AxesInVectorsAxes.getAxesToObserve() Gets the axes to observe.
Axes	AxesInPointsAxes.getAxesToObserve() Gets the axes to observe.
Axes	AxesInAxes.getAxesToObserve() Gets the axes to observe in another axes.
abstract Axes	Covariance3By3Evaluator.getDefinedIn() Gets the Axes that the covariance information is defined in.
Axes	VectorInterpolator.getDefinedInAxes() Gets the axes in which the interpolated vector is defined.
Axes	VectorFixed.getDefinedInAxes() Gets the axes in which the Vector is defined.
Axes	ParameterizedVector.getDefinedInAxes() Gets the axes in which the vector is defined.
Axes	ParameterizedOnStateVector.getDefinedInAxes() Gets the axes in which the vector is defined.
Axes	AxesFixedAtJulianDate.getFixedAxes() Gets the Axes that will be evaluated at the FixedAt (get / set) date.
Axes	VectorFixedAtJulianDate.getFixedWithRespectTo() Gets the (optional) Axes in which the FixedVector (get / set) will be fixed.
Axes	AxesFixedAtJulianDate.getFixedWithRespectTo() Gets the (optional) Axes in which the FixedAxes (get / set) will be fixed.
Axes	VectorInAxes.getInAxes() Gets the axes in which to observe the vector.
Axes	AxesInAxes.getInAxes() Gets the axes in which to find the axes.
Axes	VectorPropagationParameter.getIntegrationAxes() Gets the Axes used to define the state during integration.
Axes	VectorSum.getObservedAxes() Gets the Axes in which the resultant vector sum will be observed.
Axes	IOrientationAxesService.getOrientationAxes() Gets the axes that describes the orientation of the object.
abstract Axes	DynamicCovariance3By3.getOrientationAxes() Gets the time-varying axes of the covariance ellipsoid.
Axes	ConstantCovariance3By3.getOrientationAxes() Gets the time-varying axes of the covariance ellipsoid.
Axes	VectorAngularVelocity.getReferenceAxes() Gets the reference axes.
Axes	VectorAngularAcceleration.getReferenceAxes() Gets the reference axes.
Axes	ScalarVectorElement.getReferenceAxes() Gets the Axes to observe the ReferenceVector (get / set).
Axes	AxesLinearRate.getReferenceAxes() Gets the axes from which this axes is offset.
Axes	AxesInterpolator.getReferenceAxes() Gets the reference axes in which this axes is defined.
Axes	AxesFixedOffset.getReferenceAxes() Gets the axes from which this axes is offset.
static Axes	Axes.getRoot() Gets the root axes, which is not defined in terms of any other axes.
Axes	VectorAngularVelocity.getRotatingAxes() Gets the rotating axes.
Axes	VectorAngularAcceleration.getRotatingAxes() Gets the rotating axes.
static Axes	GeometryTransformer.Advanced.unwrap(Axes axes) Unwraps an AxesInAxes, AxesInVectorsAxes, or AxesInPointsAxes, returning the simple underlying Axes.

Methods in agi.foundation.geometry that return types with arguments of type Axes

Modifier and Type	Method and Description
protected static TimeIntervalCollection1<Axes>	VectorEvaluator.createConstantDefinedIn(Axes definedIn) Creates a TimeIntervalCollection indicating that the Axes that this Vector is defined in is the same for all possible times.
protected static TimeIntervalCollection1<Axes>	AxesEvaluator.createConstantDefinedIn(Axes definedIn) Creates a TimeIntervalCollection indicating that the Axes that this Axes is defined in is the same for all possible times.
abstract TimeIntervalCollection1<Axes>	VectorEvaluator.getDefinedInIntervals() Gets a TimeIntervalCollection where the Data (get) property of each interval is the Axes in which this Vector is defined over the interval.
abstract TimeIntervalCollection1<Axes>	AxesEvaluator.getDefinedInIntervals() Gets a TimeIntervalCollection where the Data (get) property of each interval is the Axes in which this Axes is defined over the interval.
TimeIntervalCollection1<Axes>	CompositeAxes.getIntervals() Gets the collection of intervals where the data for a given interval represents the Axes for that time.

Methods in agi.foundation.geometry with parameters of type Axes

Modifier and Type	Method and Description
protected boolean	EntityAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesFromArchive.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesFromBankAngle.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesAlongTerrain.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesVelocityOrbitNormal.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesVehicleVelocityLocalHorizontal.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesPropagationParameter.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesNorthEastDown.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesLocalVerticalLocalHorizontal.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesEastNorthUp.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesBPlane.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	ServiceProviderAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	CompositeAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesTargetingLink.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesLinearRate.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesInVectorsAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesInterpolator.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesInPointsAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesInAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesFixedOffset.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesFixedAtJulianDate.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected boolean	AxesAlignedConstrained.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
protected abstract boolean	Axes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
Axes	InternationalTerrestrialReferenceFrameTransformer.convertAxes(Axes fromAxes, Axes axes) Converts an Axes such that the ITRF transformation is applied when it is evaluated.
static Axes	InternationalTerrestrialReferenceFrameTransformer.convertAxes(EarthCentralBody earth, Axes axes, String toFrame) Converts an Axes such that an ITRF transformation is applied when it is evaluated.
static Axes	InternationalTerrestrialReferenceFrameTransformer.convertAxes(EarthCentralBody earth, Axes axes, String toFrame, ArrayList<InternationalTerrestrialReferenceFrameTransformer> itrfList) Converts an Axes such that an ITRF transformation is applied when it is evaluated.
protected static TimeIntervalCollection1<Axes>	VectorEvaluator.createConstantDefinedIn(Axes definedIn) Creates a TimeIntervalCollection indicating that the Axes that this Vector is defined in is the same for all possible times.
protected static TimeIntervalCollection1<Axes>	AxesEvaluator.createConstantDefinedIn(Axes definedIn) Creates a TimeIntervalCollection indicating that the Axes that this Axes is defined in is the same for all possible times.
Vector	AxesPropagationParameter.createVectorAngularVelocity(Axes axes) Constructs a vector which represents the angular velocity of this axes with respect to another axes.
Vector	Vector.createVectorDerivative(int order, Axes axes) Constructs a vector which represents a derivative of this vector.
static AxesEvaluator	GeometryTransformer.getAxesTransformation(Axes from, Axes to) Gets an evaluator that can be used to find the transformation from one axes to another.
static AxesEvaluator	GeometryTransformer.getAxesTransformation(Axes from, Axes to, EvaluatorGroup group) Gets an evaluator that can be used to find the transformation from one axes to another.
Covariance3By3Evaluator	DynamicCovariance3By3.getEvaluator(Axes definedIn) Constructs an evaluator that calculates the size and orientation of the position covariance over time.
abstract Covariance3By3Evaluator	DynamicCovariance3By3.getEvaluator(Axes definedIn, EvaluatorGroup group) Constructs an evaluator that calculates the size and orientation of the position covariance over time.
Covariance3By3Evaluator	ConstantCovariance3By3.getEvaluator(Axes definedIn, EvaluatorGroup group) Constructs an evaluator that calculates the size and orientation of the position covariance over time.
Scalar	Vector.getScalarElement(CartesianElement element, Axes referenceAxes) Gets a Scalar representing the X, Y, Z, or Magnitude of this vector.
Scalar	Vector.getScalarElement(CartesianElement element, Axes referenceAxes, int order) Gets a Scalar representing the X, Y, Z, or Magnitude of this vector, or any derivative of those elements.
static AxesEvaluator	GeometryTransformer.Advanced.getTransformationFromPointsAxes(Point fromPoint, Axes to) Gets an evaluator that can be used to find the transformation from the axes in which a point is defined to a given axes.
static AxesEvaluator	GeometryTransformer.Advanced.getTransformationFromPointsAxes(Point fromPoint, Axes to, EvaluatorGroup group) Gets an evaluator that can be used to find the transformation from the axes in which a point is defined to a given axes.
static AxesEvaluator	GeometryTransformer.Advanced.getTransformationFromVectorsAxes(Vector fromVector, Axes to) Gets an evaluator that can be used to find the transformation from the axes in which a vector is defined to a given axes.
static AxesEvaluator	GeometryTransformer.Advanced.getTransformationFromVectorsAxes(Vector fromVector, Axes to, EvaluatorGroup group) Gets an evaluator that can be used to find the transformation from the axes in which a vector is defined to a given axes.
static VectorFixed	VectorFixed.getUnitXVector(Axes definedInAxes) Gets a VectorFixed whose Components (get / set) are the UnitX (get) direction of the axes.
static VectorFixed	VectorFixed.getUnitYVector(Axes definedInAxes) Gets a VectorFixed whose Components (get / set) are the UnitY (get) direction of the axes.
static VectorFixed	VectorFixed.getUnitZVector(Axes definedInAxes) Gets a VectorFixed whose Components (get / set) are the UnitZ (get) direction of the axes.
static VectorEvaluator	GeometryTransformer.observeVector(Vector vector, Axes inAxes) Gets an evaluator that can be used to find the Motion<Cartesian> of this vector in a given axes at a given JulianDate.
static VectorEvaluator	GeometryTransformer.observeVector(Vector vector, Axes inAxes, EvaluatorGroup group) Gets an evaluator that can be used to find the Motion<Cartesian> of this vector in a given axes at a given JulianDate.
void	VectorDerivative.setAxes(Axes value) Sets the axes.
void	ReferenceFrame.setAxes(Axes value) Sets the axes of the reference frame.
void	AxesInVectorsAxes.setAxesToObserve(Axes value) Sets the axes to observe.
void	AxesInPointsAxes.setAxesToObserve(Axes value) Sets the axes to observe.
void	AxesInAxes.setAxesToObserve(Axes value) Sets the axes to observe in another axes.
void	VectorInterpolator.setDefinedInAxes(Axes value) Sets the axes in which the interpolated vector is defined.
void	VectorFixed.setDefinedInAxes(Axes value) Sets the axes in which the Vector is defined.
void	ParameterizedVector.setDefinedInAxes(Axes value) Sets the axes in which the vector is defined.
void	ParameterizedOnStateVector.setDefinedInAxes(Axes value) Sets the axes in which the vector is defined.
void	AxesFixedAtJulianDate.setFixedAxes(Axes value) Sets the Axes that will be evaluated at the FixedAt (get / set) date.
void	VectorFixedAtJulianDate.setFixedWithRespectTo(Axes value) Sets the (optional) Axes in which the FixedVector (get / set) will be fixed.
void	AxesFixedAtJulianDate.setFixedWithRespectTo(Axes value) Sets the (optional) Axes in which the FixedAxes (get / set) will be fixed.
void	VectorInAxes.setInAxes(Axes value) Sets the axes in which to observe the vector.
void	AxesInAxes.setInAxes(Axes value) Sets the axes in which to find the axes.
void	VectorPropagationParameter.setIntegrationAxes(Axes value) Sets the Axes used to define the state during integration.
void	VectorSum.setObservedAxes(Axes value) Sets the Axes in which the resultant vector sum will be observed.
void	ISetOrientationAxesService.setOrientationAxes(Axes value) Sets the axes that describes the orientation of the object.
void	ConstantCovariance3By3.setOrientationAxes(Axes orientationAxes) Sets the OrientationAxes (get).
void	VectorAngularVelocity.setReferenceAxes(Axes value) Sets the reference axes.
void	VectorAngularAcceleration.setReferenceAxes(Axes value) Sets the reference axes.
void	ScalarVectorElement.setReferenceAxes(Axes value) Sets the Axes to observe the ReferenceVector (get / set).
void	AxesLinearRate.setReferenceAxes(Axes value) Sets the axes from which this axes is offset.
void	AxesInterpolator.setReferenceAxes(Axes value) Sets the reference axes in which this axes is defined.
void	AxesFixedOffset.setReferenceAxes(Axes value) Sets the axes from which this axes is offset.
void	VectorAngularVelocity.setRotatingAxes(Axes value) Sets the rotating axes.
void	VectorAngularAcceleration.setRotatingAxes(Axes value) Sets the rotating axes.
static Axes	GeometryTransformer.Advanced.unwrap(Axes axes) Unwraps an AxesInAxes, AxesInVectorsAxes, or AxesInPointsAxes, returning the simple underlying Axes.

Constructors in agi.foundation.geometry with parameters of type Axes

Constructor and Description
Axes(Axes existingInstance, CopyContext context) Initializes a new instance as a copy of an existing instance.
AxesFixedAtJulianDate(Axes fixedAxes, Axes fixedWithRespectTo, ValueDefinition<JulianDate> fixedAt) Initializes a new instance.
AxesFixedAtJulianDate(Axes fixedAxes, ValueDefinition<JulianDate> fixedAt) Initializes a new instance.
AxesFixedOffset(Axes referenceAxes, UnitQuaternion offset) Initializes a new instance with the specified parameters.
AxesInAxes(Axes axesToObserve, Axes inAxes) Initializes a new instance.
AxesInPointsAxes(Axes axesToObserve, Point point) Initializes a new instance.
AxesInterpolator(Axes referenceAxes, InterpolationAlgorithm interpolationAlgorithm, int degree, DateMotionCollection2<UnitQuaternion,Cartesian> data) Initializes a new instance of the AxesInterpolator class from the provided parameters.
AxesInterpolator(Axes referenceAxes, InterpolationAlgorithm interpolationAlgorithm, int degree, DateMotionCollection2<UnitQuaternion,Cartesian> data, List<JulianDate> segmentBoundaryTimes) Initializes a new instance of the AxesInterpolator class from the provided parameters.
AxesInterpolator(Axes referenceAxes, InterpolationAlgorithmType algorithmType, int degree, DateMotionCollection2<UnitQuaternion,Cartesian> data) Initializes a new instance of the AxesInterpolator class from the provided parameters.
AxesInterpolator(Axes referenceAxes, InterpolationAlgorithmType algorithmType, int degree, DateMotionCollection2<UnitQuaternion,Cartesian> data, List<JulianDate> segmentBoundaryTimes) Initializes a new instance of the AxesInterpolator class from the provided parameters.
AxesInterpolator(Axes referenceAxes, RotationalMotionInterpolator interpolator) Initializes a new instance from the provided parameters.
AxesInVectorsAxes(Axes axesToObserve, Vector vector) Initializes a new instance.
AxesLinearRate(Axes referenceAxes, JulianDate epoch, UnitQuaternion initialRotation, UnitCartesian spinAxis, double initialRotationalVelocity, double rotationalAcceleration) Initializes a new instance with the specified parameters.
ConstantCovariance3By3(Cartesian standardDeviations, Axes orientationAxes) Creates a new instance from the specified constant size and the orientation axes.
ParameterizedOnStateVector(TimeBasedStateParameter parameter, Axes definedInAxes, String elementIdentification) Initializes a new instance.
ParameterizedVector(Axes definedInAxes) Initializes a new instance.
ParameterizedVector(CartesianParameter parameter, Axes definedInAxes) Initializes a new instance.
ReferenceFrame(Point origin, Axes axes) Initializes a new instance with the specified origin and axes.
ScalarVectorElement(Vector vector, CartesianElement element, Axes referenceAxes) Initializes a new instance.
VectorAngularAcceleration(Axes rotatingAxes, Axes referenceAxes) Initializes a new instance of the VectorAngularAcceleration class using the provided axes.
VectorAngularVelocity(Axes rotatingAxes, Axes referenceAxes) Initializes a new instance of the VectorAngularVelocity class using the provided axes.
VectorDerivative(Vector vector, int order, Axes axes) Initializes a new instance of the VectorVelocity class to represent the velocity of a given point in a given reference frame.
VectorFixed(Axes definedInAxes, Cartesian components) Initializes a new instance of the VectorFixed class using the provided vector components with respect to the provided Axes.
VectorFixedAtJulianDate(Vector fixedVector, Axes fixedWithRespectTo, ValueDefinition<JulianDate> fixedAt) Initializes a new instance.
VectorInAxes(Vector vectorToObserve, Axes inAxes) Initializes a new instance.
VectorInterpolator(Axes definedInAxes, InterpolationAlgorithm interpolationAlgorithm, int degree, DateMotionCollection1<Cartesian> data) Initializes a new instance of the VectorInterpolator class from the provided parameters.
VectorInterpolator(Axes definedInAxes, InterpolationAlgorithm interpolationAlgorithm, int degree, DateMotionCollection1<Cartesian> data, List<JulianDate> segmentBoundaryTimes) Initializes a new instance of the VectorInterpolator class from the provided parameters.
VectorInterpolator(Axes definedInAxes, InterpolationAlgorithmType algorithmType, int degree, DateMotionCollection1<Cartesian> data) Initializes a new instance of the VectorInterpolator class from the provided parameters.
VectorInterpolator(Axes definedInAxes, InterpolationAlgorithmType algorithmType, int degree, DateMotionCollection1<Cartesian> data, List<JulianDate> segmentBoundaryTimes) Initializes a new instance of the VectorInterpolator class from the provided parameters.
VectorInterpolator(Axes definedInAxes, TranslationalMotionInterpolator interpolator) Initializes a new instance of the VectorInterpolator class from the provided parameters.
VectorNormalized(Axes axes, Cartesian direction) Construct a new unit vector based on a direction and an axes.
VectorNormalized(Axes axes, UnitCartesian direction) Construct a new unit vector based on a direction and an axes.
VectorPropagationParameter(Axes axes) Initializes a new instance with the given axes of integration.

Constructor parameters in agi.foundation.geometry with type arguments of type Axes

Constructor and Description
CompositeAxes(TimeIntervalCollection1<Axes> intervals) Initializes a new instance with the provided intervals.

Uses of Axes in agi.foundation.graphics

Methods in agi.foundation.graphics that return Axes

Modifier and Type	Method and Description
Axes	Camera.getAxes() Gets camera's axes of rotation.

Methods in agi.foundation.graphics with parameters of type Axes

Modifier and Type	Method and Description
void	Camera.setAxes(Axes value) Sets camera's axes of rotation.
void	Camera.view(Axes axes, Point cameraPosition, Point referencePoint) Views from a point to a point.
void	Camera.view(Axes axes, Point cameraPosition, Point referencePoint, UnitCartesian upAxis) Views from a point to a point.
void	Camera.viewCentralBody(CentralBody centralBody, Axes axes) Zoom to a central body and use the specified axes for rotation.
void	Camera.viewDirection(Axes axes, Point cameraPosition, Vector direction) Views from a point to a direction.
void	Camera.viewDirection(Axes axes, Point cameraPosition, Vector direction, UnitCartesian upAxis) Views from a point to a direction.
void	Camera.viewOffset(Axes axes, Point referencePoint, Cartesian offset) Sets the camera's reference point - the point the camera is looking at.
void	Camera.viewOffset(Axes axes, Point referencePoint, Cartesian offset, UnitCartesian upAxis) Sets the camera's reference point - the point the camera is looking at.
void	Camera.viewOffsetDirection(Axes axes, Point referencePoint, Vector direction) Sets the camera's reference point - the point the camera is looking at.
void	Camera.viewOffsetDirection(Axes axes, Point referencePoint, Vector direction, UnitCartesian upAxis) Sets the camera's reference point - the point the camera is looking at.

Constructors in agi.foundation.graphics with parameters of type Axes

Constructor and Description
AxesPrimitive(ReferenceFrame sys, Axes axes, GraphicsFont font) Initializes an axes primitive with the specified ISystem sys as its source.

Uses of Axes in agi.foundation.navigation.advanced

Constructors in agi.foundation.navigation.advanced with parameters of type Axes

Constructor and Description
GpsCommunicationsFrontEnd(PlatformCollection gpsConstellation, GpsSignalConfiguration signalConfiguration, Point location, Axes orientation) Creates a front end for a GpsReceiver that can be used to model communications between GPS satellites and the GpsReceiver, using a predefined receiver signal configuration.
GpsCommunicationsFrontEnd(PlatformCollection gpsConstellation, NavigationSignalCollection signalsToTrack, List<SignalPropagationModel> signalPropagationModels, Point location, Axes orientation) Creates a front end for a GpsReceiver that can be used to model communications between GPS satellites and the GpsReceiver.

Uses of Axes in agi.foundation.numericalmethods

Methods in agi.foundation.numericalmethods that return Axes

Modifier and Type	Method and Description
Axes	Covariance6By6TwoBodyBlender.getCovarianceAxes() Gets the native axes of the CovarianceData (get / set).
Axes	Covariance3By3SizeAndOrientationInterpolator.getDefinedInAxes() Gets the Axes that the CovarianceData (get / set) is defined in.
Axes	Covariance3By3SizeAndOrientationInterpolator.getOrientationAxes() Gets the time-varying axes of the covariance ellipsoid.

Methods in agi.foundation.numericalmethods with parameters of type Axes

Modifier and Type	Method and Description
Covariance3By3Evaluator	Covariance3By3SizeAndOrientationInterpolator.getEvaluator(Axes definedIn, EvaluatorGroup group) Constructs an evaluator that calculates the size and orientation of the position covariance over time.
void	Covariance6By6TwoBodyBlender.setCovarianceAxes(Axes value) Sets the native axes of the CovarianceData (get / set).
void	Covariance3By3SizeAndOrientationInterpolator.setDefinedInAxes(Axes value) Sets the Axes that the CovarianceData (get / set) is defined in.

Constructors in agi.foundation.numericalmethods with parameters of type Axes

Constructor and Description
Covariance6By6TwoBodyBlender(DateMotionCollection1<Cartesian> orbitStates, DateMotionCollection1<Matrix> covarianceData, ReferenceFrame orbitStatesFrame, Axes covarianceAxes, ReferenceFrame inertialPropagationFrame, double gravitationalParameter) Initializes a new instance.
Covariance6By6TwoBodyBlender(DateMotionCollection1<Cartesian> orbitStates, IDateMotionCollection1<Matrix6By6Symmetric> covarianceData, ReferenceFrame orbitStatesFrame, Axes covarianceAxes, ReferenceFrame inertialPropagationFrame, double gravitationalParameter) Initializes a new instance.

Uses of Axes in agi.foundation.platforms

Subclasses of Axes in agi.foundation.platforms

Modifier and Type	Class and Description
class	PlatformOrientationAxes An Axes that can be used to refer to the current OrientationAxes (get / set) of a Platform, whatever it is at the time that this axes is evaluated.

Methods in agi.foundation.platforms that return Axes

Modifier and Type	Method and Description
Axes	AxesGraphicsParameter.getAxes() Gets the Axes (get / set) to use.
Axes	VectorGraphicsParameter.getInAxes() Gets the Axes to observe in.
Axes	AxesGraphicsParameter.getInAxes() Gets the Axes (get / set) to observe in.
Axes	Platform.getOrientationAxes() Gets the time-varying orientation of this platform.
Axes	OrientationAxesExtension.getOrientationAxes() Gets the axes that describe the orientation of the object.

Methods in agi.foundation.platforms with parameters of type Axes

Modifier and Type	Method and Description
protected boolean	PlatformOrientationAxes.checkForSameDefinition(Axes other) Checks to determine if another instance has the same definition as this instance and returns true if it does.
void	AxesGraphicsParameter.setAxes(Axes value) Sets the Axes (get / set) to use.
void	VectorGraphicsParameter.setInAxes(Axes value) Sets the Axes to observe in.
void	AxesGraphicsParameter.setInAxes(Axes value) Sets the Axes (get / set) to observe in.
void	Platform.setOrientationAxes(Axes value) Sets the time-varying orientation of this platform.
void	OrientationAxesExtension.setOrientationAxes(Axes value) Sets the axes that describe the orientation of the object.

Constructors in agi.foundation.platforms with parameters of type Axes

Constructor and Description
AxesGraphicsParameter(Axes axes, Axes inAxes) Initializes a new instance with the specified axes.
OrientationAxesExtension(Axes orientationAxes) Initializes the extension with the given axes.
Platform(String name, Point locationPoint, Axes orientationAxes) Initializes a new instance with a specified name, time-varying position, and time-varying orientation.
VectorGraphicsParameter(Vector vector, Axes inAxes) Initializes a new instance with the specified vector.

Uses of Axes in agi.foundation.propagators

Methods in agi.foundation.propagators that return Axes

Modifier and Type	Method and Description
Axes	AuxiliaryStateVector.getDefinedInAxes() Gets the Axes that this vector is defined in.
Axes	PropagationEulerianAxes.getIntegrationAxes() Gets a Axes which is parameterized on the attitude and angular velocity in the state during integration.
Axes	PropagationVector.getPropagationAxes() Gets the Axes in which the propagation occurs.

Methods in agi.foundation.propagators with parameters of type Axes

Modifier and Type	Method and Description
void	AuxiliaryStateVector.setDefinedInAxes(Axes value) Sets the Axes that this vector is defined in.
void	PropagationVector.setPropagationAxes(Axes value) Sets the Axes in which the propagation occurs.

Uses of Axes in agi.foundation.segmentpropagation

Methods in agi.foundation.segmentpropagation that return Axes

Modifier and Type	Method and Description
Axes	ImpulsiveManeuverInformation.getOrientation() Gets the orientation of the engines that will apply the DeltaV (get / set).

Methods in agi.foundation.segmentpropagation with parameters of type Axes

Modifier and Type	Method and Description
void	ImpulsiveManeuverInformation.setOrientation(Axes value) Sets the orientation of the engines that will apply the DeltaV (get / set).

Constructors in agi.foundation.segmentpropagation with parameters of type Axes

Constructor and Description
ImpulsiveManeuverInformation(String propagationElementIdentification, Cartesian deltaV, Axes orientationAxes) Initializes a new instance.
ImpulsiveManeuverInformation(String propagationElementIdentification, Cartesian deltaV, Axes orientationAxes, String fuelMassIdentification, String dryMassIdentification, Scalar exhaustVelocity, InvalidFuelStateBehavior whatToDo) Initializes a new instance.

Uses of Axes in agi.foundation.stk

Methods in agi.foundation.stk that return Axes

Modifier and Type	Method and Description
Axes	StkAttitudeFile.createAxes() Creates an Axes whose time-varying orientation is computed by interpolating over the attitude data held by this instance.
abstract Axes	StkAttitudeFile.Attitude.createAxes() Creates an Axes whose time-varying orientation is computed by interpolating over the attitude data held by this instance.
Axes	StkAttitudeFile.AttitudeTimeQuaternions.createAxes() Creates an Axes whose time-varying orientation is computed by interpolating over the attitude data held by this instance.
Axes	StkEphemerisFile.Covariance.getCoordinateAxes() Gets the axes in which this covariance data is observed.
Axes	StkAttitudeFile.AttitudeTimeQuaternions.getCoordinateAxes() Gets the axes in which the data is defined.

Methods in agi.foundation.stk with parameters of type Axes

Modifier and Type	Method and Description
void	StkAttitudeFile.configureFromAxes(Axes axes, JulianDate start, JulianDate stop, Duration step, int order) Configures this instance with values computed by sampling an Axes over an interval with a fixed step.
void	StkAttitudeFile.AttitudeTimeQuaternions.setCoordinateAxes(Axes value) Sets the axes in which the data is defined.

Uses of Axes in agi.foundation.tracking

Methods in agi.foundation.tracking that return Axes

Modifier and Type	Method and Description
Axes	IEntityOrientationDescriptor.getOrientationAxes() Gets the axes in which Orientation (get) is defined.