Uses of Class
org.orekit.time.FieldAbsoluteDate

Packages that use FieldAbsoluteDate

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.bodies	This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.data	This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.
org.orekit.estimation.measurements	The measurements package defines everything that is related to orbit determination measurements.
org.orekit.forces	This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.drag	This package provides all drag-related forces.
org.orekit.forces.empirical	This package provides empirical forces.
org.orekit.forces.gravity	This package provides all gravity-related forces.
org.orekit.forces.maneuvers.propulsion	This package provides propulsion models intended to be used with class Maneuver.
org.orekit.forces.maneuvers.trigger	This package provides maneuver triggers' models intended to be used with class Maneuver.
org.orekit.forces.radiation	This package provides all radiation pressure related forces.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.models.earth	This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.
org.orekit.models.earth.atmosphere	This package provides the atmosphere model interface and several implementations.
org.orekit.models.earth.ionosphere	This package provides models that simulate the impact of the ionosphere.
org.orekit.models.earth.troposphere	This package provides models that simulate the impact of the troposphere.
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation	Propagation
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.events.handlers	This package provides an interface and classes dealing with events occurrence only.
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.sampling	This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces	This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.utilities	This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.time	This independent package provides classes to handle epochs, time scales, and to compare instants together.
org.orekit.utils	This package provides useful objects.

Uses of FieldAbsoluteDate in org.orekit.attitudes

Methods in org.orekit.attitudes that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldAttitude.getDate() Get the date of attitude parameters.

Methods in org.orekit.attitudes with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> FieldAttitude<T>	YawCompensation.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	LofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	AttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	InertialProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	FixedRate.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	AttitudesSequence.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	GroundPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	SpinStabilized.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	LofOffsetPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	TabulatedLofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	YawSteering.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	AggregateBoundedAttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	TabulatedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	CelestialBodyPointed.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	YawCompensation.getBaseState(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the base system state at given date, without compensation.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	YawSteering.getBaseState(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the base system state at given date, without compensation.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	YawCompensation.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	NadirPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.
abstract <T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	GroundPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	LofOffsetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	YawSteering.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	TargetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	BodyCenterPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> T	YawCompensation.getYawAngle(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the yaw compensation angle at date.
FieldAttitude<T>	FieldAttitude.interpolate(FieldAbsoluteDate<T> interpolationDate, Stream<FieldAttitude<T>> sample) Get an interpolated instance.

Constructors in org.orekit.attitudes with parameters of type FieldAbsoluteDate

Constructor and Description
FieldAttitude(FieldAbsoluteDate<T> date, Frame referenceFrame, FieldAngularCoordinates<T> orientation) Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T> date, Frame referenceFrame, FieldRotation<T> attitude, FieldVector3D<T> spin, FieldVector3D<T> acceleration) Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T> date, Frame referenceFrame, Rotation attitude, Vector3D spin, Vector3D acceleration, Field<T> field) Creates a new instance.

Uses of FieldAbsoluteDate in org.orekit.bodies

Methods in org.orekit.bodies with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> FieldVector3D<T>	OneAxisEllipsoid.getCartesianIntersectionPoint(FieldLine<T> line, FieldVector3D<T> close, Frame frame, FieldAbsoluteDate<T> date) Get the intersection point of a line with the surface of the body.
<T extends CalculusFieldElement<T>> FieldGeodeticPoint<T>	BodyShape.getIntersectionPoint(FieldLine<T> line, FieldVector3D<T> close, Frame frame, FieldAbsoluteDate<T> date) Get the intersection point of a line with the surface of the body.
<T extends CalculusFieldElement<T>> FieldGeodeticPoint<T>	OneAxisEllipsoid.getIntersectionPoint(FieldLine<T> line, FieldVector3D<T> close, Frame frame, FieldAbsoluteDate<T> date) Get the intersection point of a line with the surface of the body.
default <T extends CalculusFieldElement<T>> FieldVector3D<T>	IAUPole.getNode(FieldAbsoluteDate<T> date) Get the body Q Node direction in ICRF frame.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	IAUPole.getPole(FieldAbsoluteDate<T> date) Get the body North pole direction in ICRF frame.
<T extends CalculusFieldElement<T>> T	IAUPole.getPrimeMeridianAngle(FieldAbsoluteDate<T> date) Get the prime meridian angle.
<T extends CalculusFieldElement<T>> FieldPVCoordinates<T>	JPLEphemeridesLoader.RawPVProvider.getRawPV(FieldAbsoluteDate<T> date) Get the position-velocity at date.
<T extends CalculusFieldElement<T>> FieldGeodeticPoint<T>	BodyShape.transform(FieldVector3D<T> point, Frame frame, FieldAbsoluteDate<T> date) Transform a Cartesian point to a surface-relative point.
<T extends CalculusFieldElement<T>> FieldGeodeticPoint<T>	OneAxisEllipsoid.transform(FieldVector3D<T> point, Frame frame, FieldAbsoluteDate<T> date) Transform a Cartesian point to a surface-relative point.

Uses of FieldAbsoluteDate in org.orekit.data

Methods in org.orekit.data that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldDelaunayArguments.getDate() Get the date.

Methods in org.orekit.data with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> FieldBodiesElements<T>	FundamentalNutationArguments.evaluateAll(FieldAbsoluteDate<T> date) Evaluate all fundamental arguments for the current date (Delaunay plus planetary).

Constructors in org.orekit.data with parameters of type FieldAbsoluteDate

Constructor and Description
FieldBodiesElements(FieldAbsoluteDate<T> date, T tc, T gamma, T gammaDot, T l, T lDot, T lPrime, T lPrimeDot, T f, T fDot, T d, T dDot, T omega, T omegaDot, T lMe, T lMeDot, T lVe, T lVeDot, T lE, T lEDot, T lMa, T lMaDot, T lJu, T lJuDot, T lSa, T lSaDot, T lUr, T lUrDot, T lNe, T lNeDot, T pa, T paDot) Simple constructor.
FieldDelaunayArguments(FieldAbsoluteDate<T> date, T tc, T gamma, T gammaDot, T l, T lDot, T lPrime, T lPrimeDot, T f, T fDot, T d, T dDot, T omega, T omegaDot) Simple constructor.

Uses of FieldAbsoluteDate in org.orekit.estimation.measurements

Methods in org.orekit.estimation.measurements with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
FieldTransform<Gradient>	GroundStation.getOffsetToInertial(Frame inertial, FieldAbsoluteDate<Gradient> offsetCompensatedDate, int freeParameters, Map<String,Integer> indices) Get the transform between offset frame and inertial frame with derivatives.
FieldTransform<Gradient>	EstimatedEarthFrameProvider.getTransform(FieldAbsoluteDate<Gradient> date, int freeParameters, Map<String,Integer> indices) Get the transform with derivatives.
<T extends CalculusFieldElement<T>> FieldTransform<T>	EstimatedEarthFrameProvider.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
static <T extends CalculusFieldElement<T>> T	AbstractMeasurement.signalTimeOfFlight(TimeStampedFieldPVCoordinates<T> adjustableEmitterPV, FieldVector3D<T> receiverPosition, FieldAbsoluteDate<T> signalArrivalDate) Compute propagation delay on a link leg (typically downlink or uplink).

Uses of FieldAbsoluteDate in org.orekit.forces

Methods in org.orekit.forces with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> FieldVector3D<T>	BoxAndSolarArraySpacecraft.dragAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, T density, FieldVector3D<T> relativeVelocity, T[] parameters) Compute the acceleration due to drag.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	BoxAndSolarArraySpacecraft.getNormal(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation) Get solar array normal in spacecraft frame.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	BoxAndSolarArraySpacecraft.radiationPressureAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, FieldVector3D<T> flux, T[] parameters) Compute the acceleration due to radiation pressure.

Uses of FieldAbsoluteDate in org.orekit.forces.drag

Methods in org.orekit.forces.drag with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> FieldVector3D<T>	IsotropicDrag.dragAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, T density, FieldVector3D<T> relativeVelocity, T[] parameters) Compute the acceleration due to drag.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	DragSensitive.dragAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, T density, FieldVector3D<T> relativeVelocity, T[] parameters) Compute the acceleration due to drag.
<T extends CalculusFieldElement<T>> T[]	TimeSpanDragForce.extractParameters(T[] parameters, FieldAbsoluteDate<T> date) Extract the proper parameter drivers' values from the array in input of the acceleration method.

Uses of FieldAbsoluteDate in org.orekit.forces.empirical

Methods in org.orekit.forces.empirical with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> T[]	TimeSpanParametricAcceleration.extractParameters(T[] parameters, FieldAbsoluteDate<T> date) Extract the proper parameter drivers' values from the array in input of the acceleration method.

Uses of FieldAbsoluteDate in org.orekit.forces.gravity

Methods in org.orekit.forces.gravity with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> T[]	HolmesFeatherstoneAttractionModel.gradient(FieldAbsoluteDate<T> date, FieldVector3D<T> position, T mu) Compute the gradient of the non-central part of the gravity field.

Uses of FieldAbsoluteDate in org.orekit.forces.maneuvers.propulsion

Methods in org.orekit.forces.maneuvers.propulsion with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> FieldAttitude<T>	ThrustDirectionAndAttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.

Uses of FieldAbsoluteDate in org.orekit.forces.maneuvers.trigger

Methods in org.orekit.forces.maneuvers.trigger with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> boolean	DateBasedManeuverTriggers.isFiring(FieldAbsoluteDate<T> date, T[] parameters)
<T extends CalculusFieldElement<T>> boolean	EventBasedManeuverTriggers.isFiring(FieldAbsoluteDate<T> date, T[] parameters) Find out if the maneuver is firing or not.
<T extends CalculusFieldElement<T>> boolean	ManeuverTriggers.isFiring(FieldAbsoluteDate<T> date, T[] parameters) Find out if the maneuver is firing or not.

Uses of FieldAbsoluteDate in org.orekit.forces.radiation

Methods in org.orekit.forces.radiation with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> T	SolarRadiationPressure.getLightingRatio(FieldVector3D<T> position, Frame frame, FieldAbsoluteDate<T> date) Get the lighting ratio ([0-1]).
<T extends CalculusFieldElement<T>> T	SolarRadiationPressure.getTotalLightingRatio(FieldVector3D<T> position, Frame frame, FieldAbsoluteDate<T> date) Get the total lighting ratio ([0-1]).
<T extends CalculusFieldElement<T>> FieldVector3D<T>	RadiationSensitive.radiationPressureAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, FieldVector3D<T> flux, T[] parameters) Compute the acceleration due to radiation pressure.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	IsotropicRadiationSingleCoefficient.radiationPressureAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, FieldVector3D<T> flux, T[] parameters) Compute the acceleration due to radiation pressure.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	IsotropicRadiationCNES95Convention.radiationPressureAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, FieldVector3D<T> flux, T[] parameters) Compute the acceleration due to radiation pressure.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	IsotropicRadiationClassicalConvention.radiationPressureAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, FieldVector3D<T> flux, T[] parameters) Compute the acceleration due to radiation pressure.

Uses of FieldAbsoluteDate in org.orekit.frames

Methods in org.orekit.frames that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldTransform.getFieldDate() Get the date.

Methods in org.orekit.frames with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> T	TopocentricFrame.getAzimuth(FieldVector3D<T> extPoint, Frame frame, FieldAbsoluteDate<T> date) Get the azimuth of a point with regards to the topocentric frame center point.
<T extends CalculusFieldElement<T>> T	TopocentricFrame.getElevation(FieldVector3D<T> extPoint, Frame frame, FieldAbsoluteDate<T> date) Get the elevation of a point with regards to the local point.
<T extends CalculusFieldElement<T>> T[]	EOPHistory.getEquinoxNutationCorrection(FieldAbsoluteDate<T> date) Get the correction to the nutation parameters for equinox-based paradigm.
<T extends CalculusFieldElement<T>> T	EOPHistory.getLOD(FieldAbsoluteDate<T> date) Get the LoD (Length of Day) value.
static <T extends CalculusFieldElement<T>> FieldTransform<T>	FramesFactory.getNonInterpolatingTransform(Frame from, Frame to, FieldAbsoluteDate<T> date) Get the transform between two frames, suppressing all interpolation.
<T extends CalculusFieldElement<T>> T[]	EOPHistory.getNonRotatinOriginNutationCorrection(FieldAbsoluteDate<T> date) Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
<T extends CalculusFieldElement<T>> FieldPoleCorrection<T>	EOPHistory.getPoleCorrection(FieldAbsoluteDate<T> date) Get the pole IERS Reference Pole correction.
<T extends CalculusFieldElement<T>> T	TopocentricFrame.getRange(FieldVector3D<T> extPoint, Frame frame, FieldAbsoluteDate<T> date) Get the range of a point with regards to the topocentric frame center point.
<T extends CalculusFieldElement<T>> T	TopocentricFrame.getRangeRate(FieldPVCoordinates<T> extPV, Frame frame, FieldAbsoluteDate<T> date) Get the range rate of a point with regards to the topocentric frame center point.
<T extends CalculusFieldElement<T>> FieldTransform<T>	InterpolatingTransformProvider.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
<T extends CalculusFieldElement<T>> FieldTransform<T>	FixedTransformProvider.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
<T extends CalculusFieldElement<T>> FieldTransform<T>	L1TransformProvider.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
<T extends CalculusFieldElement<T>> FieldTransform<T>	GTODProvider.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
<T extends CalculusFieldElement<T>> FieldTransform<T>	TransformProvider.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
<T extends CalculusFieldElement<T>> FieldTransform<T>	ShiftingTransformProvider.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
<T extends CalculusFieldElement<T>> FieldTransform<T>	EclipticProvider.getTransform(FieldAbsoluteDate<T> date)
<T extends CalculusFieldElement<T>> FieldTransform<T>	ITRFVersion.Converter.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
<T extends CalculusFieldElement<T>> FieldTransform<T>	HelmertTransformation.getTransform(FieldAbsoluteDate<T> date) Get the FieldTransform corresponding to specified date.
<T extends CalculusFieldElement<T>> FieldTransform<T>	Frame.getTransformTo(Frame destination, FieldAbsoluteDate<T> date) Get the transform from the instance to another frame.
<T extends CalculusFieldElement<T>> T	EOPHistory.getUT1MinusUTC(FieldAbsoluteDate<T> date) Get the UT1-UTC value.
static <T extends CalculusFieldElement<T>> FieldTransform<T>	FieldTransform.interpolate(FieldAbsoluteDate<T> date, CartesianDerivativesFilter cFilter, AngularDerivativesFilter aFilter, Collection<FieldTransform<T>> sample) Interpolate a transform from a sample set of existing transforms.
static <T extends CalculusFieldElement<T>> FieldTransform<T>	FieldTransform.interpolate(FieldAbsoluteDate<T> date, CartesianDerivativesFilter cFilter, AngularDerivativesFilter aFilter, Stream<FieldTransform<T>> sample) Interpolate a transform from a sample set of existing transforms.
static <T extends CalculusFieldElement<T>> FieldTransform<T>	FieldTransform.interpolate(FieldAbsoluteDate<T> interpolationDate, Collection<FieldTransform<T>> sample) Interpolate a transform from a sample set of existing transforms.
<T extends CalculusFieldElement<T>> FieldTransform<T>	LOFType.transformFromInertial(FieldAbsoluteDate<T> date, FieldPVCoordinates<T> pv) Get the transform from an inertial frame defining position-velocity and the local orbital frame.

Constructors in org.orekit.frames with parameters of type FieldAbsoluteDate

Constructor and Description
FieldTransform(FieldAbsoluteDate<T> date, FieldAngularCoordinates<T> angular) Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T> date, FieldPVCoordinates<T> cartesian) Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T> date, FieldRotation<T> rotation) Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T> date, FieldRotation<T> rotation, FieldVector3D<T> rotationRate) Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T> date, FieldRotation<T> rotation, FieldVector3D<T> rotationRate, FieldVector3D<T> rotationAcceleration) Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T> date, FieldTransform<T> first, FieldTransform<T> second) Build a transform by combining two existing ones.
FieldTransform(FieldAbsoluteDate<T> date, FieldVector3D<T> translation) Build a translation transform.
FieldTransform(FieldAbsoluteDate<T> date, FieldVector3D<T> translation, FieldVector3D<T> velocity) Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T> date, FieldVector3D<T> translation, FieldVector3D<T> velocity, FieldVector3D<T> acceleration) Build a translation transform, with its first and second time derivatives.

Uses of FieldAbsoluteDate in org.orekit.models.earth

Methods in org.orekit.models.earth with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> FieldGeodeticPoint<T>	Geoid.getIntersectionPoint(FieldLine<T> lineInFrame, FieldVector3D<T> closeInFrame, Frame frame, FieldAbsoluteDate<T> date) Get the intersection point of a line with the surface of the body.
<T extends CalculusFieldElement<T>> FieldGeodeticPoint<T>	Geoid.transform(FieldVector3D<T> point, Frame frame, FieldAbsoluteDate<T> date) Transform a Cartesian point to a surface-relative point.

Uses of FieldAbsoluteDate in org.orekit.models.earth.atmosphere

Methods in org.orekit.models.earth.atmosphere with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> T	DTM2000.getDensity(FieldAbsoluteDate<T> date, FieldVector3D<T> position, Frame frame) Get the local density.
<T extends CalculusFieldElement<T>> T	NRLMSISE00.getDensity(FieldAbsoluteDate<T> date, FieldVector3D<T> position, Frame frame) Get the local density.
<T extends CalculusFieldElement<T>> T	Atmosphere.getDensity(FieldAbsoluteDate<T> date, FieldVector3D<T> position, Frame frame) Get the local density.
<T extends CalculusFieldElement<T>> T	HarrisPriester.getDensity(FieldAbsoluteDate<T> date, FieldVector3D<T> position, Frame frame) Get the local density at some position.
<T extends CalculusFieldElement<T>> T	SimpleExponentialAtmosphere.getDensity(FieldAbsoluteDate<T> date, FieldVector3D<T> position, Frame frame)
<T extends CalculusFieldElement<T>> T	JB2008.getDensity(FieldAbsoluteDate<T> date, FieldVector3D<T> position, Frame frame) Get the local density.
default <T extends CalculusFieldElement<T>> FieldVector3D<T>	Atmosphere.getVelocity(FieldAbsoluteDate<T> date, FieldVector3D<T> position, Frame frame) Get the inertial velocity of atmosphere molecules.

Uses of FieldAbsoluteDate in org.orekit.models.earth.ionosphere

Methods in org.orekit.models.earth.ionosphere with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> T	GlobalIonosphereMapModel.getTEC(FieldAbsoluteDate<T> date, GeodeticPoint recPoint) Computes the Total Electron Content (TEC) at a given date by performing a temporal interpolation with the two closest date in the IONEX file.
<T extends CalculusFieldElement<T>> T	KlobucharIonoModel.pathDelay(FieldAbsoluteDate<T> date, FieldGeodeticPoint<T> geo, T elevation, T azimuth, double frequency, T[] parameters) Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	GlobalIonosphereMapModel.pathDelay(FieldAbsoluteDate<T> date, GeodeticPoint geo, T elevation, double frequency) Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	NeQuickModel.stec(FieldAbsoluteDate<T> date, FieldGeodeticPoint<T> recP, FieldGeodeticPoint<T> satP) This method allows the computation of the Stant Total Electron Content (STEC).

Uses of FieldAbsoluteDate in org.orekit.models.earth.troposphere

Methods in org.orekit.models.earth.troposphere with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
<T extends CalculusFieldElement<T>> T[]	ViennaOneModel.computeZenithDelay(FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) This method allows the computation of the zenith hydrostatic and zenith wet delay.
<T extends CalculusFieldElement<T>> T[]	MendesPavlisModel.computeZenithDelay(FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) This method allows the computation of the zenith hydrostatic and zenith wet delay.
<T extends CalculusFieldElement<T>> T[]	ViennaThreeModel.computeZenithDelay(FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) This method allows the computation of the zenith hydrostatic and zenith wet delay.
<T extends CalculusFieldElement<T>> T[]	TimeSpanEstimatedTroposphericModel.extractParameters(T[] parameters, FieldAbsoluteDate<T> date) Extract the proper parameter drivers' values from the array in input of the pathDelay method.
<T extends CalculusFieldElement<T>> T[]	ViennaOneModel.mappingFactors(T elevation, FieldGeodeticPoint<T> point, FieldAbsoluteDate<T> date) This method allows the computation of the hydrostatic and wet mapping functions.
<T extends CalculusFieldElement<T>> T[]	GlobalMappingFunctionModel.mappingFactors(T elevation, FieldGeodeticPoint<T> point, FieldAbsoluteDate<T> date) This method allows the computation of the hydrostatic and wet mapping functions.
<T extends CalculusFieldElement<T>> T[]	NiellMappingFunctionModel.mappingFactors(T elevation, FieldGeodeticPoint<T> point, FieldAbsoluteDate<T> date) This method allows the computation of the hydrostatic and wet mapping functions.
<T extends CalculusFieldElement<T>> T[]	MappingFunction.mappingFactors(T elevation, FieldGeodeticPoint<T> point, FieldAbsoluteDate<T> date) This method allows the computation of the hydrostatic and wet mapping functions.
<T extends CalculusFieldElement<T>> T[]	MendesPavlisModel.mappingFactors(T elevation, FieldGeodeticPoint<T> point, FieldAbsoluteDate<T> date) With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
<T extends CalculusFieldElement<T>> T[]	ViennaThreeModel.mappingFactors(T elevation, FieldGeodeticPoint<T> point, FieldAbsoluteDate<T> date) This method allows the computation of the hydrostatic and wet mapping functions.
<T extends CalculusFieldElement<T>> T	ViennaOneModel.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	DiscreteTroposphericModel.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	FixedTroposphericDelay.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	MendesPavlisModel.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	MariniMurrayModel.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	SaastamoinenModel.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	ViennaThreeModel.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	EstimatedTroposphericModel.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
<T extends CalculusFieldElement<T>> T	TimeSpanEstimatedTroposphericModel.pathDelay(T elevation, FieldGeodeticPoint<T> point, T[] parameters, FieldAbsoluteDate<T> date) Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

Uses of FieldAbsoluteDate in org.orekit.orbits

Methods in org.orekit.orbits that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldOrbit.getDate() Get the date of orbital parameters.

Methods in org.orekit.orbits with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
TimeStampedFieldPVCoordinates<T>	FieldOrbit.getPVCoordinates(FieldAbsoluteDate<T> otherDate, Frame otherFrame) Get the FieldPVCoordinates of the body in the selected frame.
FieldKeplerianOrbit<T>	FieldKeplerianOrbit.interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample) Get an interpolated instance.
FieldCircularOrbit<T>	FieldCircularOrbit.interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample) Get an interpolated instance.
FieldEquinoctialOrbit<T>	FieldEquinoctialOrbit.interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample) Get an interpolated instance.
FieldCartesianOrbit<T>	FieldCartesianOrbit.interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample) Get an interpolated instance.
abstract <T extends CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.mapArrayToOrbit(T[] array, T[] arrayDot, PositionAngle type, FieldAbsoluteDate<T> date, T mu, Frame frame) Convert state array to orbital parameters.

Constructors in org.orekit.orbits with parameters of type FieldAbsoluteDate

Constructor and Description
FieldCartesianOrbit(FieldPVCoordinates<T> pvaCoordinates, Frame frame, FieldAbsoluteDate<T> date, T mu) Constructor from Cartesian parameters.
FieldCircularOrbit(FieldPVCoordinates<T> PVCoordinates, Frame frame, FieldAbsoluteDate<T> date, T mu) Constructor from Cartesian parameters.
FieldCircularOrbit(T a, T ex, T ey, T i, T raan, T alpha, PositionAngle type, Frame frame, FieldAbsoluteDate<T> date, T mu) Creates a new instance.
FieldCircularOrbit(T a, T ex, T ey, T i, T raan, T alpha, T aDot, T exDot, T eyDot, T iDot, T raanDot, T alphaDot, PositionAngle type, Frame frame, FieldAbsoluteDate<T> date, T mu) Creates a new instance.
FieldEquinoctialOrbit(FieldPVCoordinates<T> pvCoordinates, Frame frame, FieldAbsoluteDate<T> date, T mu) Constructor from Cartesian parameters.
FieldEquinoctialOrbit(T a, T ex, T ey, T hx, T hy, T l, PositionAngle type, Frame frame, FieldAbsoluteDate<T> date, T mu) Creates a new instance.
FieldEquinoctialOrbit(T a, T ex, T ey, T hx, T hy, T l, T aDot, T exDot, T eyDot, T hxDot, T hyDot, T lDot, PositionAngle type, Frame frame, FieldAbsoluteDate<T> date, T mu) Creates a new instance.
FieldKeplerianOrbit(FieldPVCoordinates<T> FieldPVCoordinates, Frame frame, FieldAbsoluteDate<T> date, T mu) Constructor from Cartesian parameters.
FieldKeplerianOrbit(T a, T e, T i, T pa, T raan, T anomaly, PositionAngle type, Frame frame, FieldAbsoluteDate<T> date, T mu) Creates a new instance.
FieldKeplerianOrbit(T a, T e, T i, T pa, T raan, T anomaly, T aDot, T eDot, T iDot, T paDot, T raanDot, T anomalyDot, PositionAngle type, Frame frame, FieldAbsoluteDate<T> date, T mu) Creates a new instance.
FieldOrbit(Frame frame, FieldAbsoluteDate<T> date, T mu) Default constructor.

Uses of FieldAbsoluteDate in org.orekit.propagation

Methods in org.orekit.propagation that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldSpacecraftState.getDate() Get the date.
FieldAbsoluteDate<T>	FieldBoundedPropagator.getMaxDate() Get the last date of the range.
FieldAbsoluteDate<T>	FieldBoundedPropagator.getMinDate() Get the first date of the range.
protected FieldAbsoluteDate<T>	FieldAbstractPropagator.getStartDate() Get the start date.

Methods in org.orekit.propagation with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
TimeStampedFieldPVCoordinates<T>	FieldAbstractPropagator.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the FieldPVCoordinates of the body in the selected frame.
FieldSpacecraftState<T>	FieldSpacecraftState.interpolate(FieldAbsoluteDate<T> date, Stream<FieldSpacecraftState<T>> sample) Get an interpolated instance.
FieldSpacecraftState<T>	FieldPropagator.propagate(FieldAbsoluteDate<T> target) Propagate towards a target date.
FieldSpacecraftState<T>	FieldAbstractPropagator.propagate(FieldAbsoluteDate<T> target) Propagate towards a target date.
FieldSpacecraftState<T>	FieldPropagator.propagate(FieldAbsoluteDate<T> start, FieldAbsoluteDate<T> target) Propagate from a start date towards a target date.
FieldSpacecraftState<T>	FieldPropagator.propagate(FieldAbsoluteDate<T> start, FieldAbsoluteDate<T> target) Propagate from a start date towards a target date.
protected void	FieldAbstractPropagator.setStartDate(FieldAbsoluteDate<T> startDate) Set a start date.

Uses of FieldAbsoluteDate in org.orekit.propagation.analytical

Methods in org.orekit.propagation.analytical with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
protected FieldSpacecraftState<T>	FieldAbstractAnalyticalPropagator.acceptStep(org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator.FieldBasicStepInterpolator interpolator, FieldAbsoluteDate<T> target) Accept a step, triggering events and step handlers.
protected FieldSpacecraftState<T>	FieldAbstractAnalyticalPropagator.basicPropagate(FieldAbsoluteDate<T> date) Propagate an orbit without any fancy features.
protected T	FieldKeplerianPropagator.getMass(FieldAbsoluteDate<T> date) Get the mass.
protected abstract T	FieldAbstractAnalyticalPropagator.getMass(FieldAbsoluteDate<T> date) Get the mass.
protected T	FieldEcksteinHechlerPropagator.getMass(FieldAbsoluteDate<T> date) Get the mass.
FieldSpacecraftState<T>	FieldAbstractAnalyticalPropagator.propagate(FieldAbsoluteDate<T> start, FieldAbsoluteDate<T> target) Propagate from a start date towards a target date.
FieldSpacecraftState<T>	FieldAbstractAnalyticalPropagator.propagate(FieldAbsoluteDate<T> start, FieldAbsoluteDate<T> target) Propagate from a start date towards a target date.
protected FieldOrbit<T>	FieldKeplerianPropagator.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.
protected abstract FieldOrbit<T>	FieldAbstractAnalyticalPropagator.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.
FieldCartesianOrbit<T>	FieldEcksteinHechlerPropagator.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.

Uses of FieldAbsoluteDate in org.orekit.propagation.analytical.tle

Methods in org.orekit.propagation.analytical.tle that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldTLE.getDate() Get the TLE current date.

Methods in org.orekit.propagation.analytical.tle with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
protected T	FieldTLEPropagator.getMass(FieldAbsoluteDate<T> date) Get the mass.
FieldPVCoordinates<T>	FieldTLEPropagator.getPVCoordinates(FieldAbsoluteDate<T> date, T[] parameters) Get the extrapolated position and velocity from an initial TLE.
FieldOrbit<T>	FieldTLEPropagator.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.

Constructors in org.orekit.propagation.analytical.tle with parameters of type FieldAbsoluteDate

Constructor and Description
FieldTLE(int satelliteNumber, char classification, int launchYear, int launchNumber, String launchPiece, int ephemerisType, int elementNumber, FieldAbsoluteDate<T> epoch, T meanMotion, T meanMotionFirstDerivative, T meanMotionSecondDerivative, T e, T i, T pa, T raan, T meanAnomaly, int revolutionNumberAtEpoch, double bStar) Simple constructor from already parsed elements.
FieldTLE(int satelliteNumber, char classification, int launchYear, int launchNumber, String launchPiece, int ephemerisType, int elementNumber, FieldAbsoluteDate<T> epoch, T meanMotion, T meanMotionFirstDerivative, T meanMotionSecondDerivative, T e, T i, T pa, T raan, T meanAnomaly, int revolutionNumberAtEpoch, double bStar, TimeScale utc) Simple constructor from already parsed elements using the given time scale as UTC.

Uses of FieldAbsoluteDate in org.orekit.propagation.events

Methods in org.orekit.propagation.events that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldDateDetector.getDate() Get the current event date according to the propagator.
FieldAbsoluteDate<T>	FieldEventState.getEventDate() Get the occurrence time of the event triggered in the current step.
FieldAbsoluteDate<T>	FieldEventState.EventOccurrence.getStopDate() Get the new time for a stop action.

Methods in org.orekit.propagation.events with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
void	FieldDateDetector.addEventDate(FieldAbsoluteDate<T> target) Add an event date.
void	FieldEventState.init(FieldSpacecraftState<T> s0, FieldAbsoluteDate<T> t) Initialize event handler at the start of a propagation.
void	FieldAbstractDetector.init(FieldSpacecraftState<T> s0, FieldAbsoluteDate<T> t) Initialize event handler at the start of a propagation.
default void	FieldEventDetector.init(FieldSpacecraftState<T> s0, FieldAbsoluteDate<T> t) Initialize event handler at the start of a propagation.

Constructors in org.orekit.propagation.events with parameters of type FieldAbsoluteDate

Constructor and Description
FieldDateDetector(FieldAbsoluteDate<T> target) Build a new instance.

Uses of FieldAbsoluteDate in org.orekit.propagation.events.handlers

Methods in org.orekit.propagation.events.handlers with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
default void	FieldEventHandler.init(FieldSpacecraftState<T> initialState, FieldAbsoluteDate<T> target) Initialize event handler at the start of a propagation.

Uses of FieldAbsoluteDate in org.orekit.propagation.integration

Methods in org.orekit.propagation.integration that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldIntegratedEphemeris.getMaxDate() Get the last date of the range.
FieldAbsoluteDate<T>	FieldIntegratedEphemeris.getMinDate() Get the first date of the range.
FieldAbsoluteDate<T>	FieldStateMapper.getReferenceDate() Get reference date.
FieldAbsoluteDate<T>	FieldStateMapper.mapDoubleToDate(T t) Map the raw double time offset to a date.
FieldAbsoluteDate<T>	FieldStateMapper.mapDoubleToDate(T t, FieldAbsoluteDate<T> date) Map the raw double time offset to a date.

Methods in org.orekit.propagation.integration with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
protected FieldSpacecraftState<T>	FieldIntegratedEphemeris.basicPropagate(FieldAbsoluteDate<T> date) Propagate an orbit without any fancy features.
protected void	FieldAbstractIntegratedPropagator.beforeIntegration(FieldSpacecraftState<T> initialState, FieldAbsoluteDate<T> tEnd) Method called just before integration.
protected abstract FieldStateMapper<T>	FieldAbstractIntegratedPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
protected T	FieldIntegratedEphemeris.getMass(FieldAbsoluteDate<T> date) Get the mass.
TimeStampedFieldPVCoordinates<T>	FieldIntegratedEphemeris.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the FieldPVCoordinates of the body in the selected frame.
void	FieldAbstractIntegratedPropagator.MainStateEquations.init(FieldSpacecraftState<T> initialState, FieldAbsoluteDate<T> target) Initialize the equations at the start of propagation.
default void	FieldAdditionalEquations.init(FieldSpacecraftState<T> initialState, FieldAbsoluteDate<T> target) Initialize the equations at the start of propagation.
abstract FieldSpacecraftState<T>	FieldStateMapper.mapArrayToState(FieldAbsoluteDate<T> date, T[] y, T[] yDot, PropagationType type) Map the raw double components to a spacecraft state.
T	FieldStateMapper.mapDateToDouble(FieldAbsoluteDate<T> date) Map a date to a raw double time offset.
FieldAbsoluteDate<T>	FieldStateMapper.mapDoubleToDate(T t, FieldAbsoluteDate<T> date) Map the raw double time offset to a date.
FieldSpacecraftState<T>	FieldAbstractIntegratedPropagator.propagate(FieldAbsoluteDate<T> target) Propagate towards a target date.
FieldSpacecraftState<T>	FieldAbstractIntegratedPropagator.propagate(FieldAbsoluteDate<T> tStart, FieldAbsoluteDate<T> tEnd) Propagate from a start date towards a target date.
FieldSpacecraftState<T>	FieldAbstractIntegratedPropagator.propagate(FieldAbsoluteDate<T> tStart, FieldAbsoluteDate<T> tEnd) Propagate from a start date towards a target date.
protected FieldOrbit<T>	FieldIntegratedEphemeris.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.

Constructors in org.orekit.propagation.integration with parameters of type FieldAbsoluteDate

Constructor and Description
FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate, FieldAbsoluteDate<T> minDate, FieldAbsoluteDate<T> maxDate, FieldStateMapper<T> mapper, PropagationType type, FieldDenseOutputModel<T> model, Map<String,T[]> unmanaged, List<FieldAdditionalStateProvider<T>> providers, String[] equations) Creates a new instance of IntegratedEphemeris.
FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate, FieldAbsoluteDate<T> minDate, FieldAbsoluteDate<T> maxDate, FieldStateMapper<T> mapper, PropagationType type, FieldDenseOutputModel<T> model, Map<String,T[]> unmanaged, List<FieldAdditionalStateProvider<T>> providers, String[] equations) Creates a new instance of IntegratedEphemeris.
FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate, FieldAbsoluteDate<T> minDate, FieldAbsoluteDate<T> maxDate, FieldStateMapper<T> mapper, PropagationType type, FieldDenseOutputModel<T> model, Map<String,T[]> unmanaged, List<FieldAdditionalStateProvider<T>> providers, String[] equations) Creates a new instance of IntegratedEphemeris.
FieldStateMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Simple constructor.

Uses of FieldAbsoluteDate in org.orekit.propagation.numerical

Methods in org.orekit.propagation.numerical with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
protected FieldStateMapper<T>	FieldNumericalPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
TimeStampedFieldPVCoordinates<T>	FieldNumericalPropagator.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the FieldPVCoordinates of the body in the selected frame.

Uses of FieldAbsoluteDate in org.orekit.propagation.sampling

Methods in org.orekit.propagation.sampling with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
FieldSpacecraftState<T>	FieldOrekitStepInterpolator.getInterpolatedState(FieldAbsoluteDate<T> date) Get the state at interpolated date.
void	FieldStepHandlerMultiplexer.init(FieldSpacecraftState<T> s0, FieldAbsoluteDate<T> t) Initialize step handler at the start of a propagation.
default void	FieldOrekitStepHandler.init(FieldSpacecraftState<T> s0, FieldAbsoluteDate<T> t) Initialize step handler at the start of a propagation.
void	FieldOrekitStepNormalizer.init(FieldSpacecraftState<T> s0, FieldAbsoluteDate<T> t) Initialize step handler at the start of a propagation.
default void	FieldOrekitFixedStepHandler.init(FieldSpacecraftState<T> s0, FieldAbsoluteDate<T> t, T step) Initialize step handler at the start of a propagation.

Uses of FieldAbsoluteDate in org.orekit.propagation.semianalytical.dsst

Methods in org.orekit.propagation.semianalytical.dsst with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
protected void	FieldDSSTPropagator.beforeIntegration(FieldSpacecraftState<T> initialState, FieldAbsoluteDate<T> tEnd) Method called just before integration.
protected FieldStateMapper<T>	FieldDSSTPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType ignoredOrbitType, PositionAngle ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.

Uses of FieldAbsoluteDate in org.orekit.propagation.semianalytical.dsst.forces

Methods in org.orekit.propagation.semianalytical.dsst.forces with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
Map<String,T[]>	AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients.getCoefficients(FieldAbsoluteDate<T> date, Set<String> selected) Computes the coefficients involved in the contributions.
Map<String,T[]>	FieldShortPeriodTerms.getCoefficients(FieldAbsoluteDate<T> date, Set<String> selected) Computes the coefficients involved in the contributions.

Uses of FieldAbsoluteDate in org.orekit.propagation.semianalytical.dsst.utilities

Methods in org.orekit.propagation.semianalytical.dsst.utilities that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<T>	FieldAuxiliaryElements.getDate() Get the date of the orbit.

Methods in org.orekit.propagation.semianalytical.dsst.utilities with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
void	FieldShortPeriodicsInterpolatedCoefficient.addGridPoint(FieldAbsoluteDate<T> date, T[] value) Add a point to the interpolation grid.
T[]	FieldShortPeriodicsInterpolatedCoefficient.value(FieldAbsoluteDate<T> date) Compute the value of the coefficient.

Uses of FieldAbsoluteDate in org.orekit.time

Methods in org.orekit.time that return FieldAbsoluteDate

Modifier and Type	Method and Description
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createBesselianEpoch(T besselianEpoch) Build an instance corresponding to a Besselian Epoch (BE).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createBesselianEpoch(T besselianEpoch, TimeScales timeScales) Build an instance corresponding to a Besselian Epoch (BE).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createGPSDate(int weekNumber, T milliInWeek) Build an instance corresponding to a GPS date.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createGPSDate(int weekNumber, T milliInWeek, TimeScale gps) Build an instance corresponding to a GPS date.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createJDDate(int jd, T secondsSinceNoon, TimeScale timeScale) Build an instance corresponding to a Julian Day date.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createJulianEpoch(T julianEpoch) Build an instance corresponding to a Julian Epoch (JE).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createJulianEpoch(T julianEpoch, TimeScales timeScales) Build an instance corresponding to a Julian Epoch (JE).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createMJDDate(int mjd, T secondsInDay, TimeScale timeScale) Build an instance corresponding to a Modified Julian Day date.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getArbitraryEpoch(Field<T> field) Get an arbitrary date.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getCCSDSEpoch(Field<T> field) Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4):
FieldAbsoluteDate<T>	FieldAbsoluteDate.getDate() Get the date.
FieldAbsoluteDate<T>	FieldTimeStamped.getDate() Get the date.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getFiftiesEpoch(Field<T> field) Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getFutureInfinity(Field<T> field) Dummy date at infinity in the future direction.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getGalileoEpoch(Field<T> field) Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getGPSEpoch(Field<T> field) Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getJ2000Epoch(Field<T> field) J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getJavaEpoch(Field<T> field) Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getJulianEpoch(Field<T> field) Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getModifiedJulianEpoch(Field<T> field) Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getPastInfinity(Field<T> field) Dummy date at infinity in the past direction.
FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSCalendarSegmentedTimeCode(byte preambleField, byte[] timeField) Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSCalendarSegmentedTimeCode(byte preambleField, byte[] timeField, TimeScale utc) Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSDaySegmentedTimeCode(Field<T> field, byte preambleField, byte[] timeField, DateComponents agencyDefinedEpoch) Build an instance from a CCSDS Day Segmented Time Code (CDS).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSDaySegmentedTimeCode(Field<T> field, byte preambleField, byte[] timeField, DateComponents agencyDefinedEpoch, TimeScale utc) Build an instance from a CCSDS Day Segmented Time Code (CDS).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSUnsegmentedTimeCode(Field<T> field, byte preambleField1, byte preambleField2, byte[] timeField, FieldAbsoluteDate<T> agencyDefinedEpoch) Build an instance from a CCSDS Unsegmented Time Code (CUC).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSUnsegmentedTimeCode(Field<T> field, byte preambleField1, byte preambleField2, byte[] timeField, FieldAbsoluteDate<T> agencyDefinedEpoch, FieldAbsoluteDate<T> ccsdsEpoch) Build an instance from a CCSDS Unsegmented Time Code (CUC).
FieldAbsoluteDate<T>	FieldAbsoluteDate.shiftedBy(double dt) Get a time-shifted date.
FieldAbsoluteDate<T>	FieldAbsoluteDate.shiftedBy(T dt) Get a time-shifted date.

Methods in org.orekit.time with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
int	FieldAbsoluteDate.compareTo(FieldAbsoluteDate<T> date) Compare the instance with another date.
T	FieldAbsoluteDate.durationFrom(FieldAbsoluteDate<T> instant) Compute the physically elapsed duration between two instants.
<T extends CalculusFieldElement<T>> T	GLONASSScale.getLeap(FieldAbsoluteDate<T> date) Get the value of the previous leap.
default <T extends CalculusFieldElement<T>> T	TimeScale.getLeap(FieldAbsoluteDate<T> date) Get the value of the previous leap.
<T extends CalculusFieldElement<T>> T	UTCScale.getLeap(FieldAbsoluteDate<T> date) Get the value of the previous leap.
<T extends CalculusFieldElement<T>> T	UTCTAIOffset.getOffset(FieldAbsoluteDate<T> date) Get the TAI - UTC offset in seconds.
<T extends CalculusFieldElement<T>> boolean	GLONASSScale.insideLeap(FieldAbsoluteDate<T> date) Check if date is within a leap second introduction in this time scale.
default <T extends CalculusFieldElement<T>> boolean	TimeScale.insideLeap(FieldAbsoluteDate<T> date) Check if date is within a leap second introduction in this time scale.
<T extends CalculusFieldElement<T>> boolean	UTCScale.insideLeap(FieldAbsoluteDate<T> date) Check if date is within a leap second introduction in this time scale.
default T	FieldTimeInterpolable.interpolate(FieldAbsoluteDate<KK> date, Collection<T> sample) Get an interpolated instance.
T	FieldTimeInterpolable.interpolate(FieldAbsoluteDate<KK> date, Stream<T> sample) Get an interpolated instance.
<T extends CalculusFieldElement<T>> int	GLONASSScale.minuteDuration(FieldAbsoluteDate<T> date) Check length of the current minute in this time scale.
default <T extends CalculusFieldElement<T>> int	TimeScale.minuteDuration(FieldAbsoluteDate<T> date) Check length of the current minute in this time scale.
<T extends CalculusFieldElement<T>> int	UTCScale.minuteDuration(FieldAbsoluteDate<T> date) Check length of the current minute in this time scale.
T	FieldAbsoluteDate.offsetFrom(FieldAbsoluteDate<T> instant, TimeScale timeScale) Compute the apparent clock offset between two instant in the perspective of a specific time scale.
<T extends CalculusFieldElement<T>> T	GLONASSScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	GPSScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	TimeScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	TDBScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	GalileoScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	GMSTScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	QZSSScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	IRNSSScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	UTCScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	SatelliteClockScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	UT1Scale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	TTScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	TCGScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	TCBScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	BDTScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
<T extends CalculusFieldElement<T>> T	TAIScale.offsetFromTAI(FieldAbsoluteDate<T> date) Get the offset to convert locations from TAIScale to instance.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSUnsegmentedTimeCode(Field<T> field, byte preambleField1, byte preambleField2, byte[] timeField, FieldAbsoluteDate<T> agencyDefinedEpoch) Build an instance from a CCSDS Unsegmented Time Code (CUC).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSUnsegmentedTimeCode(Field<T> field, byte preambleField1, byte preambleField2, byte[] timeField, FieldAbsoluteDate<T> agencyDefinedEpoch, FieldAbsoluteDate<T> ccsdsEpoch) Build an instance from a CCSDS Unsegmented Time Code (CUC).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSUnsegmentedTimeCode(Field<T> field, byte preambleField1, byte preambleField2, byte[] timeField, FieldAbsoluteDate<T> agencyDefinedEpoch, FieldAbsoluteDate<T> ccsdsEpoch) Build an instance from a CCSDS Unsegmented Time Code (CUC).
<T extends CalculusFieldElement<T>> T	TimeScalarFunction.value(FieldAbsoluteDate<T> date) Compute a function of time.
<T extends CalculusFieldElement<T>> T[]	TimeVectorFunction.value(FieldAbsoluteDate<T> date) Compute a function of time.

Constructors in org.orekit.time with parameters of type FieldAbsoluteDate

Constructor and Description
FieldAbsoluteDate(FieldAbsoluteDate<T> since, double elapsedDuration) Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T> reference, double apparentOffset, TimeScale timeScale) Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
FieldAbsoluteDate(FieldAbsoluteDate<T> since, T elapsedDuration) Build an instance from an elapsed duration since to another instant.

Uses of FieldAbsoluteDate in org.orekit.utils

Methods in org.orekit.utils that return FieldAbsoluteDate

Modifier and Type	Method and Description
FieldAbsoluteDate<D>	FieldTimeSpanMap.Transition.getAbsoluteDate() Get the transition field absolute date.
FieldAbsoluteDate<T>	TimeStampedFieldPVCoordinates.getDate() Get the date.
FieldAbsoluteDate<T>	TimeStampedFieldAngularCoordinates.getDate() Get the date.

Methods in org.orekit.utils with parameters of type FieldAbsoluteDate

Modifier and Type	Method and Description
void	FieldTimeSpanMap.addValidAfter(T entry, FieldAbsoluteDate<D> earliestValidityDate) Add an entry valid after a limit date.
void	FieldTimeSpanMap.addValidBefore(T entry, FieldAbsoluteDate<D> latestValidityDate) Add an entry valid before a limit date.
<T extends CalculusFieldElement<T>> T	IERSConventions.evaluateTC(FieldAbsoluteDate<T> date) Evaluate the date offset between the current date and the reference date.
<T extends CalculusFieldElement<T>> T	IERSConventions.evaluateTC(FieldAbsoluteDate<T> date, TimeScales timeScales) Evaluate the date offset between the current date and the reference date.
T	FieldTimeSpanMap.get(FieldAbsoluteDate<D> date) Get the entry valid at a specified date.
TimeStampedFieldPVCoordinates<T>	FieldPVCoordinatesProvider.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the FieldPVCoordinates of the body in the selected frame.
TimeStampedFieldPVCoordinates<T>	FieldAbsolutePVCoordinates.getPVCoordinates(FieldAbsoluteDate<T> otherDate, Frame outputFrame)
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	ExtendedPVCoordinatesProvider.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the FieldPVCoordinates of the body in the selected frame.
static <T extends CalculusFieldElement<T>> TimeStampedFieldAngularCoordinates<T>	TimeStampedFieldAngularCoordinates.interpolate(FieldAbsoluteDate<T> date, AngularDerivativesFilter filter, Collection<TimeStampedFieldAngularCoordinates<T>> sample) Interpolate angular coordinates.
static <T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	TimeStampedFieldPVCoordinates.interpolate(FieldAbsoluteDate<T> date, CartesianDerivativesFilter filter, Collection<TimeStampedFieldPVCoordinates<T>> sample) Interpolate position-velocity.
static <T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	TimeStampedFieldPVCoordinates.interpolate(FieldAbsoluteDate<T> date, CartesianDerivativesFilter filter, Stream<TimeStampedFieldPVCoordinates<T>> sample) Interpolate position-velocity.
FieldAbsolutePVCoordinates<T>	FieldAbsolutePVCoordinates.interpolate(FieldAbsoluteDate<T> date, Stream<FieldAbsolutePVCoordinates<T>> sample)
static <T extends CalculusFieldElement<T>> FieldAbsolutePVCoordinates<T>	FieldAbsolutePVCoordinates.interpolate(Frame frame, FieldAbsoluteDate<T> date, CartesianDerivativesFilter filter, Stream<FieldAbsolutePVCoordinates<T>> sample) Interpolate position-velocity.

Constructors in org.orekit.utils with parameters of type FieldAbsoluteDate

Constructor and Description
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T> date, FieldAbsolutePVCoordinates<T> start, FieldAbsolutePVCoordinates<T> end) Subtractive constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T> date, T a, FieldAbsolutePVCoordinates<T> AbsPva) Multiplicative constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T> date, T a1, FieldAbsolutePVCoordinates<T> absPv1, T a2, FieldAbsolutePVCoordinates<T> absPv2) Linear constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T> date, T a1, FieldAbsolutePVCoordinates<T> absPv1, T a2, FieldAbsolutePVCoordinates<T> absPv2, T a3, FieldAbsolutePVCoordinates<T> absPv3) Linear constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T> date, T a1, FieldAbsolutePVCoordinates<T> absPv1, T a2, FieldAbsolutePVCoordinates<T> absPv2, T a3, FieldAbsolutePVCoordinates<T> absPv3, T a4, FieldAbsolutePVCoordinates<T> absPv4) Linear constructor
FieldAbsolutePVCoordinates(Frame frame, FieldAbsoluteDate<T> date, FieldPVCoordinates<T> pva) Build from frame, date and FieldPVA coordinates.
FieldAbsolutePVCoordinates(Frame frame, FieldAbsoluteDate<T> date, FieldVector3D<T> position, FieldVector3D<T> velocity) Build from position and velocity.
FieldAbsolutePVCoordinates(Frame frame, FieldAbsoluteDate<T> date, FieldVector3D<T> position, FieldVector3D<T> velocity, FieldVector3D<T> acceleration) Build from position, velocity, acceleration.
FieldAbsolutePVCoordinates(Frame frame, FieldAbsoluteDate<T> date, FieldVector3D<U> p) Builds a FieldAbsolutePVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T> date, FieldPVCoordinates<T> u1, FieldPVCoordinates<T> u2, FieldPVCoordinates<T> v1, FieldPVCoordinates<T> v2, double tolerance) Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T> date, FieldRotation<T> rotation, FieldVector3D<T> rotationRate, FieldVector3D<T> rotationAcceleration) Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T> date, FieldRotation<U> r) Builds a TimeStampedFieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, double a, FieldPVCoordinates<T> pv) Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, double a1, FieldPVCoordinates<T> pv1, double a2, FieldPVCoordinates<T> pv2) Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, double a1, FieldPVCoordinates<T> pv1, double a2, FieldPVCoordinates<T> pv2, double a3, FieldPVCoordinates<T> pv3) Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, double a1, FieldPVCoordinates<T> pv1, double a2, FieldPVCoordinates<T> pv2, double a3, FieldPVCoordinates<T> pv3, double a4, FieldPVCoordinates<T> pv4) Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, FieldPVCoordinates<T> pv) Basic constructor.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, FieldPVCoordinates<T> start, FieldPVCoordinates<T> end) Subtractive constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, FieldVector3D<T> position, FieldVector3D<T> velocity, FieldVector3D<T> acceleration) Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, FieldVector3D<U> p) Builds a TimeStampedFieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a, FieldPVCoordinates<T> pv) Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, FieldPVCoordinates<T> pv1, T a2, FieldPVCoordinates<T> pv2) Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, FieldPVCoordinates<T> pv1, T a2, FieldPVCoordinates<T> pv2, T a3, FieldPVCoordinates<T> pv3) Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, FieldPVCoordinates<T> pv1, T a2, FieldPVCoordinates<T> pv2, T a3, FieldPVCoordinates<T> pv3, T a4, FieldPVCoordinates<T> pv4) Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a, PVCoordinates pv) Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2) Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2, T a3, PVCoordinates pv3) Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2, T a3, PVCoordinates pv3, T a4, PVCoordinates pv4) Linear constructor