A B C D E F G H I J K L M N O P Q R S T U V W X Y Z 

A

a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final semi major axis.
a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
a.
A - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
A = sqrt(μ * a).
a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered semi major axis.
AbsoluteDate - Class in org.orekit.time
This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate
Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an elapsed duration since to another instant.
AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for absorption coefficient.
AbstractAnalyticalPropagator - Class in org.orekit.propagation.analytical
Common handling of Propagator methods for analytical propagators.
AbstractAnalyticalPropagator(AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Build a new instance.
AbstractDetector<T extends EventDetector> - Class in org.orekit.propagation.events
Common parts shared by several orbital events finders.
AbstractDetector(double, double, int, EventHandler<T>) - Constructor for class org.orekit.propagation.events.AbstractDetector
Build a new instance.
AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces
Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.
AbstractGaussianContribution(double, ForceModel) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Build a new instance.
AbstractIntegratedPropagator - Class in org.orekit.propagation.integration
Common handling of Propagator methods for both numerical and semi-analytical propagators.
AbstractIntegratedPropagator(AbstractIntegrator, boolean) - Constructor for class org.orekit.propagation.integration.AbstractIntegratedPropagator
Build a new instance.
AbstractIntegratedPropagator.MainStateEquations - Interface in org.orekit.propagation.integration
Differential equations for the main state (orbit, attitude and mass).
AbstractPropagator - Class in org.orekit.propagation
Common handling of Propagator methods for analytical propagators.
AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator
Build a new instance.
AbstractPropagatorConverter - Class in org.orekit.propagation.conversion
Common handling of PropagatorConverter methods for propagators conversions.
AbstractPropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorConverter
Build a new instance.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in interface org.orekit.forces.ForceModel
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in interface org.orekit.forces.ForceModel
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.Relativity
 
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.Relativity
 
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.propagation.numerical.Jacobianizer
Compute acceleration and derivatives with respect to state.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.propagation.numerical.Jacobianizer
Compute acceleration and derivatives with respect to parameter.
acceptStep(AbsoluteDate, double) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsBashforthIntegrator.
AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a new instance.
AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsMoultonIntegrator.
AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a new instance.
AdapterPropagator - Class in org.orekit.propagation.analytical
Orbit propagator that adapts an underlying propagator, adding differential effects.
AdapterPropagator(Propagator) - Constructor for class org.orekit.propagation.analytical.AdapterPropagator
Build a propagator from an underlying reference propagator.
AdapterPropagator.DifferentialEffect - Interface in org.orekit.propagation.analytical
Interface for orbit differential effects.
add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Add a step handler.
add(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Add the argument matrix with the current matrix.
addAcceleration(Vector3D, Frame) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of an acceleration expressed in some inertial frame.
addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add a set of user-specified equations to be integrated along with the orbit propagation.
addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state.
addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add a loader for celestial bodies.
addChild(OrphanFrame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame
Add a child.
addChild(OrphanFrame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame
Add a child.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.drag.DragForce
Compute the contribution of the drag to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.OceanTides
Compute the contribution of the force model to the perturbing acceleration.
addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Add the contribution of the wave to Stokes coefficients.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.Relativity
 
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.SolidTides
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute the contribution of the force model to the perturbing acceleration.
addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for celestial bodies.
addDefaultEOP1980HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add the default READERS for ocean tides.
addDefaultPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add the default readers for gravity fields.
addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager
Add the default providers configuration.
addDefaultUTCTAILoader() - Static method in class org.orekit.time.TimeScalesFactory
Add the default loader for UTC-TAI offsets history files.
addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Add a differential effect.
addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Static method in class org.orekit.frames.FramesFactory
Add a loader for Earth Orientation Parameters history.
addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector
Add an event date.
addEventDetector(T) - Method in class org.orekit.propagation.AbstractPropagator
Add an event detector.
addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add an event detector.
addEventDetector(T) - Method in interface org.orekit.propagation.Propagator
Add an event detector.
addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Add a force model to the global perturbation model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Add a force model to the global perturbation model.
addGridPoint(AbsoluteDate, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
AdditionalEquations - Interface in org.orekit.propagation.integration
This interface allows users to add their own differential equations to a numerical propagator.
AdditionalStateProvider - Interface in org.orekit.propagation
This interface represents providers for additional state data beyond SpacecraftState.
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.Orbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the Kepler evolution.
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add a reader for ocean tides.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Add an offset from the instance.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Add an offset from the instance.
addPoint(AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic
Add a fitting point.
addPotentialCoefficientsReader(PotentialCoefficientsReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add a reader for gravity fields.
addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Add a data provider to the supported list.
addSatellite(String) - Method in class org.orekit.files.sp3.SP3File
Add a new satellite with a given identifier to the list of stored satellites.
addSatelliteCoordinate(String, SatelliteTimeCoordinate) - Method in class org.orekit.files.sp3.SP3File
Adds a new P/V coordinate for a given satellite.
addSwitchingCondition(AttitudeProvider, T, boolean, boolean, AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence
Add a switching condition between two attitude providers.
addUTCTAILoader(UTCTAILoader) - Static method in class org.orekit.time.TimeScalesFactory
Add a loader for UTC-TAI offsets history files.
addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Add parsed coefficients.
addXYZAcceleration(double, double, double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of an acceleration expressed in the inertial frame (it is important to make sure this acceleration is defined in the same frame as the orbit) .
afterIntegration() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just after integration.
AlignmentDetector - Class in org.orekit.propagation.events
Finder for satellite/body alignment events.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AltitudeDetector - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AngularCoordinates - Class in org.orekit.utils
Simple container for rotation/rotation rate/rotation acceleration triplets.
AngularCoordinates() - Constructor for class org.orekit.utils.AngularCoordinates
Simple constructor.
AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate pair.
AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate/rotation acceleration triplet.
AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
AngularCoordinates(FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a AngularCoordinates from a FieldRotation<DerivativeStructure>.
AngularDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedAngularCoordinates and TimeStampedFieldAngularCoordinates interpolation.
apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on a spacecraft state.
apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect
Apply the effect to a spacecraft state.
apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Apply the effect to a spacecraft state.
applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic
Approximate an already fitted model to polynomial only terms.
ApsideDetector - Class in org.orekit.propagation.events
Finder for apside crossing events.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants
Conversion factor from arc seconds to radians: 2*PI/(360*60*60).
AstronomicalAmplitudeReader - Class in org.orekit.forces.gravity.potential
Parser for tides astronomical amplitude Hf.
AstronomicalAmplitudeReader(String, int, int, int, double) - Constructor for class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Simple constructor.
Atmosphere - Interface in org.orekit.forces.drag
Interface for atmospheric models.
AtmosphericRefractionModel - Interface in org.orekit.models
Defines an refraction model that can be used to correct for the apparent position of an object due to atmospheric effects.
ATOMIC_NITROGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for atomic nitrogen.
ATOMIC_OXYGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for atomic oxygen.
attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame
Attach the instance (and all its children down to leafs) to the main tree.
attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame
Attach the instance (and all its children down to leafs) to the main tree.
Attitude - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
AttitudeProvider - Interface in org.orekit.attitudes
This interface represents an attitude provider model set.
AttitudeProviderModifier - Interface in org.orekit.attitudes
This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudesSequence - Class in org.orekit.attitudes
This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence
Constructor for an initially empty sequence.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction
Suffix for parameter name for attraction coefficient enabling jacobian processing.
AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities
Container class for common parameters used by all DSST forces.
AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Simple constructor.

B

B - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
B = sqrt(1 - h² - k²).
B_STAR - Static variable in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Parameter name for B* coefficient.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
 
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Propagate an orbit without any fancy features.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just before integration.
BESSELIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Besselian year: 365.242198781 Constants.JULIAN_DAY.
beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
sqrt (1 - e2).
beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
1 - e2.
BodiesElements - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements
Simple constructor.
BodyCenterPointing - Class in org.orekit.attitudes
This class handles body center pointing attitude provider.
BodyCenterPointing(Frame) - Constructor for class org.orekit.attitudes.BodyCenterPointing
Creates new instance.
BodyShape - Interface in org.orekit.bodies
Interface representing the rigid surface shape of a natural body.
BoundedPropagator - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces
experimental class representing the features of a classical satellite with a convex body shape and rotating flat solar arrays.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lightning of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lightning of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft.Facet - Class in org.orekit.forces
Class representing a single facet of a convex spacecraft body.
BoxAndSolarArraySpacecraft.Facet(Vector3D, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Simple constructor.
buildIdentityMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the identity matrix of order 2.
buildIdentityMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the identity matrix of order 4.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in interface org.orekit.propagation.conversion.FirstOrderIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder
Build a first order integrator.
buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a propagator.
buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a propagator.
buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a propagator.
buildPropagator(AbsoluteDate, double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Build a propagator.
buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a propagator.
buildRow(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Build a coefficients row.
buildTriangularArray(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Build a coefficients triangular array.
buildZeroMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the empty matrix of order 2.
buildZeroMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the empty matrix of order 4.
BULLETINA_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinA files (IAU1980 and IAU2000 compatibles).
BULLETINB_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinB files (IAU1980 compatibles).
BULLETINB_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinB files (IAU2000 compatibles).

C

C - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
C = 1 + p² + q².
c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C1 from SPTRCK #3.
c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C2 from SPTRCK #3.
c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C4 from SPTRCK #3.
CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential
CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Simple constructor.
calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.
calculatePathDelay(double, double) - Method in class org.orekit.models.earth.FixedTroposphericDelay
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
calculatePathDelay(double, double) - Method in class org.orekit.models.earth.SaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
calculatePathDelay(double, double) - Method in interface org.orekit.models.earth.TroposphericDelayModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
calculateSignalDelay(double, double) - Method in class org.orekit.models.earth.FixedTroposphericDelay
Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.
calculateSignalDelay(double, double) - Method in class org.orekit.models.earth.SaastamoinenModel
Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.
calculateSignalDelay(double, double) - Method in interface org.orekit.models.earth.TroposphericDelayModel
Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.
canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if coefficients can be added.
CartesianDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.
CartesianOrbit - Class in org.orekit.orbits
This class holds cartesian orbital parameters.
CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from any kind of orbital parameters.
CCSDS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
CCSDS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01.
CCSDSFrame - Enum in org.orekit.files.ccsds
Frames used in CCSDS Orbit Data Messages.
CelestialBody - Interface in org.orekit.bodies
Interface for celestial bodies like Sun, Moon or solar system planets.
CelestialBodyFactory - Class in org.orekit.bodies
Factory class for bodies of the solar system.
CelestialBodyLoader - Interface in org.orekit.bodies
Interface for loading celestial bodies.
CelestialBodyPointed - Class in org.orekit.attitudes
This class handles a celestial body pointed attitude provider.
CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed
Creates new instance.
CenterName - Enum in org.orekit.files.ccsds
Orbit central bodies for which a Celestial body can be created.
CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.forces.gravity.NewtonianAttraction
Name of the single parameter of this model: the central attraction coefficient.
checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory
Check Earth orientation parameters continuity.
ChronologicalComparator - Class in org.orekit.time
Comparator for TimeStamped instance.
ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator
Simple constructor.
CircularFieldOfViewDetector - Class in org.orekit.propagation.events
Finder for target entry/exit events with respect to a satellite sensor Field Of View.
CircularFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, double) - Constructor for class org.orekit.propagation.events.CircularFieldOfViewDetector
Build a new instance.
CircularOrbit - Class in org.orekit.orbits
This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(double, double, double, double, double, double, PositionAngle, TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from cartesian parameters.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from cartesian parameters.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from any kind of orbital parameters.
CjSjCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Sj(k, h) and the Cj(k, h) series and their partial derivatives with respect to k and h.
CjSjCoefficient(double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Cj(k, h) and Sj(k, h) constructor.
ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for ClassicalRungeKuttaIntegrator.
ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder
Build a new instance.
ClasspathCrawler - Class in org.orekit.data
Provider for data files stored as resources in the classpath.
ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear the specified celestial body from the internal cache.
clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear all loaded celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for one celestial body.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for all celestial bodies.
clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory
Clear loaders for Earth Orientation Parameters history.
clearEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Remove all events detectors.
clearEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Remove all events detectors.
clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Clear the recorded values from the interpolation grid.
clearLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
Clear the set of data file names that have been loaded.
clearLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
Clear the logged events.
clearOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Clear ocean tides readers.
clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Clear gravity field readers.
clearProviders() - Method in class org.orekit.data.DataProvidersManager
Remove all data providers.
clearUTCTAILoaders() - Static method in class org.orekit.time.TimeScalesFactory
Clear loaders for UTC-TAI offsets history files.
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
C / (2 * A * B) .
coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
coef for SGP C3 computation.
coef1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
coef for SGP C5 computation.
CoefficientsFactory - Class in org.orekit.propagation.semianalytical.dsst.utilities
This class is designed to provide coefficient from the DSST theory.
CoefficientsFactory.MNSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities
MNS couple's key.
CoefficientsFactory.MNSKey(int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey
Simpleconstructor.
CoefficientsFactory.NSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities
Key formed by two integer values.
CoefficientsFactory.NSKey(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Simple constructor.
compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator
Compare two time-stamped instances.
compareTo(CoefficientsFactory.MNSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey
compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compare the instance with another date.
compareTo(DateComponents) - Method in class org.orekit.time.DateComponents
compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
compile(PoissonSeries<S>...) - Static method in class org.orekit.data.PoissonSeries
Join several nutation series, for fast simultaneous evaluation.
computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.propagation.integration.AdditionalEquations
Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Compute the derivatives related to the additional state parameters.
computeGsHs(double, double, double, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute recursively Gs and Hs polynomials from equation 3.1-(5).
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the values for the first four coefficients and their derivatives by means of series.
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the initial values (see Collins, 4-255, 4-256 and 4.259)
computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the limit visibility point for a satellite in a given direction.
computeMeanState(SpacecraftState, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from osculating to mean, orbit.
computeOsculatingState(SpacecraftState, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from mean to osculating orbit.
computeQns(double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Qn,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).
computeShortPeriodicsCoefficients(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the coefficients used for short periodic variations.
computeShortPeriodicsCoefficients(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Compute the coefficients used for short periodic variations.
computeShortPeriodicsCoefficients(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Compute the coefficients used for short periodic variations.
computeShortPeriodicsCoefficients(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Compute the coefficients used for short periodic variations.
computeVns(int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Vn,s coefficients from 2.8.2-(1)(2).
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Configure ocean load deformation coefficients.
Constants - Interface in org.orekit.utils
Set of useful physical constants.
ConstantThrustManeuver - Class in org.orekit.forces.maneuvers
This class implements a simple maneuver with constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
containsSatellite(String) - Method in class org.orekit.files.ccsds.ODMFile
Tests whether a satellite with the given id is contained in this orbit file.
containsSatellite(String) - Method in interface org.orekit.files.general.OrbitFile
Tests whether a satellite with the given id is contained in this orbit file.
containsSatellite(String) - Method in class org.orekit.files.sp3.SP3File
Tests whether a satellite with the given id is contained in this orbit file.
ContinueOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent
 
convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter
Convert a row.
convert(Propagator, double, int, Collection<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(List<SpacecraftState>, boolean, Collection<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Convert an osculating orbit into a mean orbit, in DSST sense.
convert(Propagator, double, int, Collection<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(List<SpacecraftState>, boolean, Collection<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
cosinus original inclination.
create(double, double, int, EventHandler<ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
create(double, double, int, EventHandler<T>) - Method in class org.orekit.propagation.events.AbstractDetector
Build a new instance.
create(double, double, int, EventHandler<AlignmentDetector>) - Method in class org.orekit.propagation.events.AlignmentDetector
Build a new instance.
create(double, double, int, EventHandler<AltitudeDetector>) - Method in class org.orekit.propagation.events.AltitudeDetector
Build a new instance.
create(double, double, int, EventHandler<ApsideDetector>) - Method in class org.orekit.propagation.events.ApsideDetector
Build a new instance.
create(double, double, int, EventHandler<CircularFieldOfViewDetector>) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Build a new instance.
create(double, double, int, EventHandler<DateDetector>) - Method in class org.orekit.propagation.events.DateDetector
Build a new instance.
create(double, double, int, EventHandler<DihedralFieldOfViewDetector>) - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Build a new instance.
create(double, double, int, EventHandler<EclipseDetector>) - Method in class org.orekit.propagation.events.EclipseDetector
Build a new instance.
create(double, double, int, EventHandler<ElevationDetector>) - Method in class org.orekit.propagation.events.ElevationDetector
Build a new instance.
create(double, double, int, EventHandler<EventFilter<T>>) - Method in class org.orekit.propagation.events.EventFilter
Build a new instance.
create(double, double, int, EventHandler<EventShifter<T>>) - Method in class org.orekit.propagation.events.EventShifter
Build a new instance.
create(double, double, int, EventHandler<GeographicZoneDetector>) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Build a new instance.
create(double, double, int, EventHandler<NodeDetector>) - Method in class org.orekit.propagation.events.NodeDetector
Build a new instance.
createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createFromModifiedRodrigues(double[][]) - Static method in class org.orekit.utils.AngularCoordinates
Convert a modified Rodrigues vector and derivatives to angular coordinates.
createFromWeekComponents(int, int, int) - Static method in class org.orekit.time.DateComponents
Build a date from week components.
createGPSDate(int, double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a GPS date.
createIllegalArgumentException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException
Create an IllegalArgumentException with localized message.
createIllegalStateException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException
Create an IllegalStateException with localized message.
createInternalError(Throwable) - Static method in exception org.orekit.errors.OrekitException
Create an RuntimeException for an internal error.
createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a mapper between raw double components and spacecraft state.
createParseException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException
Create an ParseException with localized message.
createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Create an ITRF frame by transforming another ITRF frame.
crossProduct(PVCoordinates, PVCoordinates) - Static method in class org.orekit.utils.PVCoordinates
Compute the cross-product of two instances.
CunninghamAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
CunninghamAttractionModel(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.CunninghamAttractionModel
Creates a new instance.

D

DataLoader - Interface in org.orekit.data
Interface for loading data files from data providers.
DataProvider - Interface in org.orekit.data
Interface for providing data files to file loaders.
DataProvidersManager - Class in org.orekit.data
Singleton class managing all supported data providers.
DateComponents - Class in org.orekit.time
Class representing a date broken up as year, month and day components.
DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from a year and day number.
DateComponents(int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a reference epoch.
DateDetector - Class in org.orekit.propagation.events
Finder for date events.
DateDetector(double, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector
Build a new instance.
DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector
Build a new instance.
DateTimeComponents - Class in org.orekit.time
Holder for date and time components.
DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents
Build a new instance from its components.
DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from a seconds offset with respect to another one.
DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for default type of ephemeris (SGP4/SDP4).
DEFAULT_CACHED_SLOTS_NUMBER - Static variable in class org.orekit.utils.GenericTimeStampedCache
Default number of independent cached time slots.
DEFAULT_CORRECTION_FACTOR - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default correction factor value.
DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader
Default supported files name pattern for JPL DE files.
DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader
Default supported files name pattern for IMCCE INPOP files.
DEFAULT_LAW - Static variable in interface org.orekit.propagation.Propagator
Default attitude provider.
DEFAULT_MASS - Static variable in interface org.orekit.propagation.Propagator
Default mass.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.AbstractDetector
Default cmaximum number of iterations in the event time search.
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector
Default maximum checking interval (s).
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.OceanTides
Default number of points tides field sampling.
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.SolidTides
Default number of points tides field sampling.
DEFAULT_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default local pressure at viewpoint (Pa).
DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.OceanTides
Default step for tides field sampling (seconds).
DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.SolidTides
Default step for tides field sampling (seconds).
DEFAULT_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default local temperature at viewpoint (K).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector
Default convergence threshold (s).
DelaunayArguments - Class in org.orekit.data
Delaunay arguments used for nutation or tides.
DelaunayArguments(AbsoluteDate, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments
Simple constructor.
DihedralFieldOfViewDetector - Class in org.orekit.propagation.events
Finder for body entering/exiting dihedral FOV events.
DihedralFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, Vector3D, double, Vector3D, double) - Constructor for class org.orekit.propagation.events.DihedralFieldOfViewDetector
Build a new instance.
DirectoryCrawler - Class in org.orekit.data
Provider for data files stored in a directories tree on filesystem.
DirectoryCrawler(File) - Constructor for class org.orekit.data.DirectoryCrawler
Build a data files crawler.
DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for DormandPrince54Integrator.
DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a new instance.
DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for DormandPrince853Integrator.
DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a new instance.
DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive
Parameter name for drag coefficient enabling jacobian processing.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag, with state derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute acceleration due to drag, with parameters derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag, with state derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in interface org.orekit.forces.drag.DragSensitive
Compute acceleration due to drag, with parameters derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in class org.orekit.forces.SphericalSpacecraft
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.SphericalSpacecraft
Compute the acceleration due to drag, with state derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in class org.orekit.forces.SphericalSpacecraft
Compute acceleration due to drag, with parameters derivatives.
DragForce - Class in org.orekit.forces.drag
Atmospheric drag force model.
DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce
Simple constructor.
DragSensitive - Interface in org.orekit.forces.drag
Interface for spacecraft that are sensitive to atmospheric drag forces.
DrozinerAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
DrozinerAttractionModel(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.DrozinerAttractionModel
Creates a new instance.
dsEvaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces
Atmospheric drag contribution to the DSSTPropagator.
DSSTAtmosphericDrag(Atmosphere, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor assuming spherical spacecraft.
DSSTAtmosphericDrag(Atmosphere, DragSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor with custom spacecraft.
DSSTCentralBody - Class in org.orekit.propagation.semianalytical.dsst.forces
Central body gravitational contribution to the DSSTPropagator.
DSSTCentralBody(Frame, double, UnnormalizedSphericalHarmonicsProvider, boolean) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
DSST Central body constructor.
DSSTCentralBody(Frame, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
DSST Central body constructor.
DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces
This interface represents a force modifying spacecraft motion for a DSSTPropagator.
DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst
This class propagates orbits using the DSST theory.
DSSTPropagator(AbstractIntegrator, boolean) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(AbstractIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces
Solar radiation pressure contribution to the DSSTPropagator.
DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values and spherical spacecraft.
DSSTSolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values, but custom spacecraft.
DSSTSolarRadiationPressure(double, double, double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Constructor with customizable reference values but spherical spacecraft.
DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Complete constructor.
DSSTThirdBody - Class in org.orekit.propagation.semianalytical.dsst.forces
Third body attraction perturbation to the DSSTPropagator.
DSSTThirdBody(CelestialBody) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Complete constructor.
DTM2000 - Class in org.orekit.forces.drag
This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.DTM2000
Simple constructor for independent computation.
DTM2000InputParameters - Interface in org.orekit.forces.drag
Container for solar activity data, compatible with DTM2000 Atmosphere model.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compute the physically elapsed duration between two instants.

E

e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final eccentricity.
e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity squared.
EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth-Moon barycenter.
EarthStandardAtmosphereRefraction - Class in org.orekit.models.earth
Implementation of refraction model for Earth standard atmosphere.
EarthStandardAtmosphereRefraction() - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Creates a new default instance.
EarthStandardAtmosphereRefraction(double, double) - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Creates an instance given a specific pressure and temperature.
ecc - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Eccentricity.
EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical
This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Private helper constructor.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential.
EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential provider.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Eckstein-Hechler propagator.
EcksteinHechlerPropagatorBuilder(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EcksteinHechlerPropagatorBuilder(Frame, double, double, TideSystem, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EclipseDetector - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipticProvider - Class in org.orekit.frames
An inertial frame aligned with the ecliptic.
EclipticProvider(IERSConventions) - Constructor for class org.orekit.frames.EclipticProvider
Create a transform provider from MOD to an ecliptically aligned frame.
eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity * eta.
EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.
EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.
EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.
EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.
EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.
EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EGM96 model: 6378136.3 m.
EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for EGM files.
EGMFormatReader - Class in org.orekit.forces.gravity.potential
This reader is adapted to the EGM Format.
EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor.
EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.
EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.
EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.
EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.
EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.
EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EIGEN5C model: 6378136.46 m.
EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².
ElevationDetector - Class in org.orekit.propagation.events
Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
ElevationMask - Class in org.orekit.utils
Class for modeling the ground elevation values around a given point.
ElevationMask(double[][]) - Constructor for class org.orekit.utils.ElevationMask
Creates an instance of an Elevation mask based on the passed in parameter.
Ellipse - Class in org.orekit.bodies
Model of a 2D ellipse in 3D space.
Ellipse(Vector3D, Vector3D, Vector3D, double, double, Frame) - Constructor for class org.orekit.bodies.Ellipse
Simple constructor.
Ellipsoid - Class in org.orekit.bodies
Modeling of a general three-axes ellipsoid.
Ellipsoid(Frame, double, double, double) - Constructor for class org.orekit.bodies.Ellipsoid
Simple constructor.
EME2000_ALIGNED - Static variable in class org.orekit.attitudes.InertialProvider
Dummy attitude provider, perfectly aligned with the EME2000 frame.
emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache
Get an empty immutable cache, cast to the correct type.
endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
End parsing.
ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState
Check if two instances have the same set of additional states available.
EOPC04_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOPC04 files (IAU1980 compatibles).
EOPC04_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOPC04 files (IAU2000 compatibles).
EOPEntry - Class in org.orekit.frames
This class holds an Earth Orientation Parameters entry.
EOPEntry(int, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.EOPEntry
Simple constructor.
EOPHistory - Class in org.orekit.frames
This class loads any kind of Earth Orientation Parameter data throughout a large time range.
EOPHistory(IERSConventions, Collection<EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory
Simple constructor.
EOPHistoryLoader - Interface in org.orekit.frames
Interface for loading Earth Orientation Parameters history.
Ephemeris - Class in org.orekit.propagation.analytical
This class is designed to accept and handle tabulated orbital entries.
Ephemeris(List<SpacecraftState>, int) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for ephemeris generation mode.
equals(Object) - Method in class org.orekit.bodies.GeodeticPoint
 
equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey
equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
equals(Object) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represent the same time as another instance.
equals(Object) - Method in class org.orekit.time.DateComponents
equals(Object) - Method in class org.orekit.time.DateTimeComponents
equals(Object) - Method in class org.orekit.time.TimeComponents
EquinoctialOrbit - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from cartesian parameters.
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from cartesian parameters.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from any kind of orbital parameters.
estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates
Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates
Estimate FieldRotation rate between two orientations.
estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates
Estimate velocity between two positions.
estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates
Estimate velocity between two positions.
eta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
eta from SPTRCK #3.
etasq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
eta squared.
EulerIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for EulerIntegrator.
EulerIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerIntegratorBuilder
Build a new instance.
evaluateAll(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments
Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateDerivative(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments
Evaluate all fundamental arguments for the current date (Delaunay plus planetary), including the first time derivative.
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Evaluate the impact of the proposed step on the event detector.
evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
EventDetector - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
EventFilter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper used to detect only increasing or decreasing events.
EventFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventFilter
EventHandler<T extends EventDetector> - Interface in org.orekit.propagation.events.handlers
An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.
EventHandler.Action - Enum in org.orekit.propagation.events.handlers
Enumerate for actions to be performed when an event occurs.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AbstractDetector
Handle the event.
eventOccurred(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.EventDetector
Handle the event.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler
eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing
Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing
Handle a detection event and choose what to do next.
EventShifter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper shifting events occurrences times.
EventShifter(T, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter
Build a new instance.
EventsLogger - Class in org.orekit.propagation.events
This class logs events detectors events during propagation.
EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger
Simple constructor.
EventsLogger.LoggedEvent - Class in org.orekit.propagation.events
Class for logged events entries.
EventState<T extends EventDetector> - Class in org.orekit.propagation.events
This class handles the state for one event detector during integration steps.
EventState(T) - Constructor for class org.orekit.propagation.events.EventState
Simple constructor.
extendListOfLists(List<List<Double>>, int, int, double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Extend a list of lists of coefficients if needed.

F

f - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Equinoctial frame f vector.
FactoryManagedFrame - Class in org.orekit.frames
Base class for the predefined frames that are managed by FramesFactory.
FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame
Simple constructor.
feed(Pattern, DataLoader) - Method in class org.orekit.data.ClasspathCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in interface org.orekit.data.DataProvider
Feed a data file loader by browsing the data collection.
feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager
Feed a data file loader by browsing all data providers.
feed(Pattern, DataLoader) - Method in class org.orekit.data.DirectoryCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in class org.orekit.data.NetworkCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in class org.orekit.data.ZipJarCrawler
Feed a data file loader by browsing the data collection.
FES_CHAT_EPSILON_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES C hat and epsilon tides files.
FES_CNM_SNM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES Cnm, Snm tides files.
FES_HF_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES Hf tides files.
FESCHatEpsilonReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides files following the fes2004.dat format.
FESCHatEpsilonReader(String, double, double, OceanLoadDeformationCoefficients, Map<Integer, Double>) - Constructor for class org.orekit.forces.gravity.potential.FESCHatEpsilonReader
Simple constructor.
FESCnmSnmReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides files following the fes2004_Cnm-Snm.dat format.
FESCnmSnmReader(String, double) - Constructor for class org.orekit.forces.gravity.potential.FESCnmSnmReader
Simple constructor.
FieldAngularCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils
Simple container for FieldRotation/FieldRotation rate pairs, using RealFieldElement.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a rotation/rotation rate pair.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldRotation/FieldRotation rate/FieldRotation acceleration triplet.
FieldBodiesElements<T extends RealFieldElement<T>> - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
FieldBodiesElements(AbsoluteDate, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements
Simple constructor.
FieldDelaunayArguments<T extends RealFieldElement<T>> - Class in org.orekit.data
Delaunay arguments used for nutation or tides.
FieldDelaunayArguments(AbsoluteDate, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments
Simple constructor.
FieldPVCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils
Simple container for Position/Velocity pairs, using RealFieldElement.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a PVCoordinates triplet with zero acceleration.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a PVCoordinates triplet.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor
FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Subtractive constructor
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor
FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for 1950 dates: 1950-01-01.
fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a single vector.
fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EOPHistoryLoader
Load celestial body.
FilterType - Enum in org.orekit.propagation.events
Enumerate for filtering events.
FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion
Propagator converter using finite differences to compute the jacobian.
FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Simple constructor.
FirstOrderIntegratorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build first order integrators for propagators conversion.
fit() - Method in class org.orekit.utils.SecularAndHarmonic
Fit parameters.
FixedRate - Class in org.orekit.attitudes
This class handles a simple attitude provider at constant rate around a fixed axis.
FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate
Creates a new instance.
FixedTransformProvider - Class in org.orekit.frames
Transform provider using fixed transform.
FixedTransformProvider(Transform) - Constructor for class org.orekit.frames.FixedTransformProvider
Simple constructor.
FixedTroposphericDelay - Class in org.orekit.models.earth
A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.
FixedTroposphericDelay(double[], double[], double[][]) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance.
FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the DataProvidersManager.
ForceModel - Interface in org.orekit.forces
This interface represents a force modifying spacecraft motion.
Frame - Class in org.orekit.frames
Tridimensional references frames class.
Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
FrameAncestorException - Exception in org.orekit.errors
This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.
FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException
Simple constructor.
FramesFactory - Class in org.orekit.frames
Factory for predefined reference frames.
freeze() - Method in class org.orekit.frames.Transform
Get a frozen transform.
FundamentalNutationArguments - Class in org.orekit.data
Class computing the fundamental arguments for nutation and tides.
FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the future direction.

G

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventFilter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
Compute the value of the switching function.
g - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Equinoctial frame g vector.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants
Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for Galileo System Time: 1999-08-22.
GalileoScale - Class in org.orekit.time
Galileo system time scale.
GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(double[], double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Simple constructor.
generate(T, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator
Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OMMFile
Generate a CartesianOrbit from the KeplerianOrbit.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OPMFile
Generate a CartesianOrbit from the OPM state vector data.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OMMFile
Generate a KeplerianOrbit based on the OMM mean keplerian elements.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OPMFile
Generate a KeplerianOrbit from the OPM keplerian elements if hasKeplerianElements is true, or from the state vector data otherwise.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.OMMFile
Generate spacecraft state from the KeplerianOrbit generated by generateKeplerianOrbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.OPMFile
Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateTLE() - Method in class org.orekit.files.ccsds.OMMFile
Generate TLE from OMM file.
GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
Generic thread-safe cache for time-stamped data.
GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>, Class<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache
Simple constructor.
GeodeticPoint - Class in org.orekit.bodies
Point location relative to a 2D body surface.
GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint
Build a new instance.
GeographicZoneDetector - Class in org.orekit.propagation.events
Detector for entry/exit of a zone defined by geographic boundaries.
GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a new detector.
GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a detector.
GeoMagneticElements - Class in org.orekit.models.earth
Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements
Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth
Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField
Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth
Factory for different GeoMagneticField models.
GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth
The currently supported geomagnetic field models.
GeoMagneticModelLoader - Class in org.orekit.models.earth
Loads geomagnetic field models from a given input stream.
GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader
 
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Get the last 24H mean geomagnetic index.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
The Kp index is derived from the Ap index.
getA() - Method in class org.orekit.bodies.Ellipse
Get the semi major axis.
getA() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the first semi-axis.
getA() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit semi-major axis.
getA() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState
Get the semi-major axis.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the abscissa grid for the interpolation function.
getAbsorptionCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the absorption coefficient.
getAbsorptionCoefficient() - Method in interface org.orekit.forces.radiation.RadiationSensitive
Get the absorption coefficient.
getAbsorptionCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft
Get the absorption coefficient.
getAcceleration() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesDataLine
Get the ephemerides data line acceleration vector.
getAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the translation.
getAcceleration(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the acceleration due to the non conservative perturbing force.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates
Gets the acceleration.
getAccuracy() - Method in class org.orekit.files.general.SatelliteInformation
Returns the estimated accuracy of the orbit entries for this satellite (in m).
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the adapted propagator.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Get an additional state.
getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Compute the length of the one-dimensional additional state array needed.
getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator
Get an unmodifiable list of providers for additional state.
getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState
Get an unmodifiable map of additional states.
getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body reference radius.
getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the value of the central body reference radius.
getAgency() - Method in class org.orekit.files.sp3.SP3File
Returns the agency that prepared this SP3 file.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get all of the data in this cache.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine α for central body.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the threshold altitude value.
getAncestor(int) - Method in class org.orekit.frames.Frame
Get the nth ancestor of the frame.
getAngular() - Method in class org.orekit.frames.Transform
Get the underlying elementary angular part.
getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAnomaly() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly.
getAnomalyType() - Method in class org.orekit.files.ccsds.OGMFile
Get the type of anomaly (true or mean).
getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the Geomagnetic planetary 3-hour index Ap.
getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get facet area.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the atmospheric model.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState
Get the attitude.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the Attitude Provider to use during maneuver.
getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper
Get the attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator
Get attitude provider.
getAvailableParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the available free parameters.
getAvailableParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get the names of the available parameters in the propagator.
getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Get the available satellite numbers.
getAxis1() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the direction of FOV 1st dihedral axis.
getAxis2() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the direction of FOV 2nd dihedral axis.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getB() - Method in class org.orekit.bodies.Ellipse
Get the semi minor axis.
getB() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the second semi-axis.
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get B = sqrt(1 - e²).
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine β for central body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Get a celestial body.
getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get third body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get body frame related to body shape.
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get a body oriented, body centered frame.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the body shape.
getBStar() - Method in class org.orekit.files.ccsds.OMMFile
Get the SGP/SGP4 drag-like coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the ballistic coefficient.
getC() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the third semi-axis.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get C = 1 + p² + q².
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration
Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents
Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month
Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month
Get the capitalized full name.
getCartesian() - Method in class org.orekit.frames.Transform
Get the underlying elementary cartesian part.
getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName
Get the celestial body corresponding to the CCSDS constant.
getCenter() - Method in class org.orekit.bodies.Ellipse
Get the center of the 2D ellipse.
getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get the direction of FOV center.
getCenter() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the direction of FOV center.
getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the CelestialBody corresponding to the center name.
getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the origin of reference frame.
getChildren() - Method in class org.orekit.frames.OrphanFrame
Get all children of the instance.
getCircularEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector.
getCircularEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector.
getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the CIRF2000 reference frame.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Cj coefficient.
getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the classification.
getClassificationType() - Method in class org.orekit.files.ccsds.OMMFile
Get the classification type.
getClockCorrection() - Method in class org.orekit.files.general.SatelliteTimeCoordinate
Returns the clock correction value.
getClockRateChange() - Method in class org.orekit.files.general.SatelliteTimeCoordinate
Returns the clock rate change value.
getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Get the closest TLE to the selected date.
getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Get the load deformation coefficients for ocean tides.
getComment() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the meta-data comment.
getComment() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get the maneuvers data comment, each string in the list corresponds to one line of comment.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components.
getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a time-independent provider for read spherical harmonics coefficients.
getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConventions() - Method in class org.orekit.files.ccsds.ODMFile
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.ODMParser
Get IERS conventions.
getConventions() - Method in class org.orekit.frames.EOPHistory
Get the IERS conventions to which these EOP apply.
getCoordinate() - Method in class org.orekit.files.general.SatelliteTimeCoordinate
Returns the coordinate of this entry.
getCoordinateSystem() - Method in class org.orekit.files.ccsds.OEMFile
Returns the coordinate system of the entries in this orbit file.
getCoordinateSystem() - Method in class org.orekit.files.ccsds.OMMFile
Returns the coordinate system of the entries in this orbit file.
getCoordinateSystem() - Method in class org.orekit.files.ccsds.OPMFile
Returns the coordinate system of the entries in this orbit file.
getCoordinateSystem() - Method in interface org.orekit.files.general.OrbitFile
Returns the coordinate system of the entries in this orbit file.
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File
Returns the coordinate system of the entries in this orbit file.
getCovarianceComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for covariance.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the list of Covariance Matrices.
getCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile
Get the Position/Velocity covariance matrix.
getCovRefFrame() - Method in class org.orekit.files.ccsds.OGMFile
Get coordinate system for covariance matrix, for absolute frames.
getCovRefLofType() - Method in class org.orekit.files.ccsds.OGMFile
Get coordinate system for covariance matrix, for Local Orbital Frames.
getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile
Get the file creation date and time in UTC.
getCurrentDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the current grid date.
getD() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun.
getD() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun.
getDataUsed() - Method in class org.orekit.files.sp3.SP3File
Returns the data used indicator from the SP3 file.
getDate() - Method in class org.orekit.attitudes.Attitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.data.DelaunayArguments
Get the date.
getDate() - Method in class org.orekit.data.FieldDelaunayArguments
Get the date.
getDate() - Method in class org.orekit.files.general.SatelliteTimeCoordinate
Get the date.
getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the date of the maneuver.
getDate() - Method in class org.orekit.frames.EOPEntry
Get the date.
getDate() - Method in class org.orekit.frames.Transform
Get the date.
getDate() - Method in class org.orekit.orbits.Orbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the TLE current date.
getDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the date of the initial state.
getDate() - Method in class org.orekit.propagation.events.DateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState
Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate
Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents
Get the date component.
getDate() - Method in interface org.orekit.time.TimeStamped
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get the date.
getDay() - Method in class org.orekit.time.DateComponents
Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3File
Returns the day fraction for this SP3 file.
getDayOfWeek() - Method in class org.orekit.time.DateComponents
Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents
Get the day number in year.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dk coefficient.
getDdEps() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in obliquity δΔε.
getDdPsi() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in longitude δΔΨ.
getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField
Utility function to get a decimal year for a given day.
getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the declination of the magnetic field in degrees.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the decreasing events time shift.
getDefaultModel() - Static method in class org.orekit.models.earth.FixedTroposphericDelay
Returns the default model, loading delay values from the file "tropospheric-delay.txt".
getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get mass change during maneuver (value is < 0).
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the velocity increment in satellite frame.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.Atmosphere
Get the local density.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.DTM2000
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.DTM2000
Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.HarrisPriester
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.HarrisPriester
Get the local density at some position.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.JB2006
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.JB2006
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere
Get the local density.
getDepth() - Method in class org.orekit.frames.Frame
Get the depth of the frame.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function derivative.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the derivative dKj-n-1, s / de².
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dk coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dk coefficient.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dk coefficient.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dk coefficient.
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of dLns / dγ (γ).
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the Doodson number for the wave.
getDragArea() - Method in class org.orekit.files.ccsds.OGMFile
Get the drag area.
getDragCoeff() - Method in class org.orekit.files.ccsds.OGMFile
Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drag coefficient.
getDragCoefficient() - Method in interface org.orekit.forces.drag.DragSensitive
Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft
Get the drag coefficient.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dk coefficient.
getDuration() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get duration (value is 0 for impulsive maneuver).
getDV() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get velocity increment.
getDx() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getE() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit eccentricity.
getE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.Orbit
Get the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentricity.
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the earliest cached entry.
getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
 
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
Get the earliest entry in this cache.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth singleton body.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth-Moon barycenter singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEast() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame
Get the east direction of topocentric frame, expressed in parent shape frame.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentricity.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly.
getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the ecliptic frame.
getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the differential effects.
getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get the value of an element.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the element number.
getElementSetNumber() - Method in class org.orekit.files.ccsds.OMMFile
Get the element set number for this satellite.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(double) - Method in class org.orekit.utils.ElevationMask
Get the interpolated elevation for a given azimuth according to the mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured elevation mask.
getEME2000() - Static method in class org.orekit.frames.FramesFactory
Get the unique EME2000 frame.
getEndDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the last available Earth Orientation Parameters.
getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the total number of entries cached.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get Earth Orientation Parameters history.
getEOPHistory() - Method in class org.orekit.time.UT1Scale
Get the EOP history.
getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions
Get the function computing tidal corrections for Earth Orientation Parameters.
getEphemeridesBlocks() - Method in class org.orekit.files.ccsds.OEMFile
Get the list of ephemerides blocks as an unmodifiable list.
getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the list of Ephemerides data lines.
getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the ephemerides data lines comment.
getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile
Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the type of ephemeris.
getEpoch() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get the epoch relative to the covariance matrix.
getEpoch() - Method in class org.orekit.files.ccsds.OEMFile
Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.files.ccsds.OGMFile
Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in interface org.orekit.files.general.OrbitFile
Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.files.general.SatelliteTimeCoordinate
Returns the epoch for this coordinate.
getEpoch() - Method in class org.orekit.files.sp3.SP3File
Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.frames.HelmertTransformation
Get the reference epoch of the transform.
getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the epoch for this magnetic field model.
getEpochComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for epoch.
getEpochIgnition() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.ccsds.ODMFile
Not supported by CCSDS orbit messages.
getEpochInterval() - Method in interface org.orekit.files.general.OrbitFile
Returns the time interval between epochs (in seconds).
getEpochInterval() - Method in class org.orekit.files.sp3.SP3File
Returns the time interval between epochs (in seconds).
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the equatorial radius of the body.
getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the central body equatorial radius.
getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the number of objective function evaluations.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState
Get the underlying event detector.
getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce
There are no discrete events for this model.
getEventsDetectors() - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity
 
getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the discrete events related to the model.
getEventTime() - Method in class org.orekit.propagation.events.EventState
Get the occurrence time of the event triggered in the current step.
getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper
Get the wrapped exception.
getExosphericTemp() - Method in class org.orekit.forces.drag.JB2006
Get the exospheric temperature above input position.
getF() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame
Get the key of the frame within the factory.
getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the GeoMagneticField for the given model type and year.
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the magnetic field vector in nTesla.
getFileDate(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Get the date of the file from which data at the specified date comes from.
getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter
Get the filter corresponding to a maximum derivation order.
getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Get the filter corresponding to a maximum derivation order.
getFirst() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Get the first TLE.
getFirstDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Get the start date of the series.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the first known leap second.
getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic
Get a copy of the last fitted parameters.
getFixedStepSize() - Method in class org.orekit.propagation.AbstractPropagator
Get the fixed step size.
getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the flattening of the body: f = (a-b)/a.
getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the flow rate.
getForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get perturbing force models list.
getFormatVersion() - Method in class org.orekit.files.ccsds.ODMFile
Get the CCSDS ODM (OPM, OMM or OEM) format version.
getFrame() - Method in class org.orekit.bodies.Ellipse
Get the defining frame.
getFrame() - Method in class org.orekit.bodies.Ellipsoid
Get the ellipsoid central frame.
getFrame(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame
Get the frame corresponding to the CCSDS constant.
getFrame() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get coordinate system for covariance matrix, for absolute frames.
getFrame() - Method in interface org.orekit.forces.drag.Atmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.DTM2000
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.HarrisPriester
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.JB2006
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere
Get the frame of the central body.
getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory
Get one of the predefined frames.
getFrame() - Method in class org.orekit.frames.OrphanFrame
Get the associated frame.
getFrame() - Method in class org.orekit.orbits.Orbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
 
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the frame of the initial state.
getFrame() - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.StateMapper
Get the inertial frame.
getFrame() - Method in interface org.orekit.propagation.Propagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.SpacecraftState
Get the inertial frame.
getFrameEpoch() - Method in class org.orekit.files.ccsds.ODMMetaData
Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameEpochString() - Method in class org.orekit.files.ccsds.ODMMetaData
Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFreeParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the free parameters.
getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame
Get a new version of the instance, frozen with respect to a reference frame.
getGamma() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine γ for central body.
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique GCRF frame.
getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the generate method.
getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator
Get the ephemeris generated during propagation.
getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the generator.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Gjs coefficient.
getGM() - Method in interface org.orekit.bodies.CelestialBody
Get the attraction coefficient of the body.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Gmsj coefficient.
getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Greenwich Mean Sidereal Time scale.
getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Global Positioning System scale.
getGpsWeek() - Method in class org.orekit.files.sp3.SP3File
Returns the GPS week as contained in the SP3 file.
getGradient() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian
Get a reference to the gradient.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the number of interpolation grid points.
getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.VariableStepInterpolationGrid
Get grid points that are within the current step.
getGST() - Static method in class org.orekit.time.TimeScalesFactory
Get the Galileo System Time scale.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of eccentricity vector.
getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get FOV half aperture angle.
getHalfAperture1() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the half aperture angle of FOV 1st dihedra.
getHalfAperture2() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the half aperture angle of FOV 2nd dihedra.
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
Get the handler.
getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic
Get an upper bound of the fitted harmonic amplitude.
getHasCreatableBody() - Method in class org.orekit.files.ccsds.ODMMetaData
Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodyFactory.
getHasManeuver() - Method in class org.orekit.files.ccsds.OPMFile
Get boolean testing whether the OPM contains at least one maneuver.
getHasRefFrameEpoch() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get boolean testing whether the reference frame has an epoch associated to it.
getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile
Get the header comment.
getHessian() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian
Get a reference to the Hessian.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Hjs coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Hmsj coefficient.
getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).
getHour() - Method in class org.orekit.time.TimeComponents
Get the hour number.
getHP() - Method in class org.orekit.propagation.numerical.ParameterConfiguration
Get parameter step.
getHx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getI() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit inclination.
getI() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.Orbit
Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState
Get the inclination.
getICRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique ICRF frame.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the IGRF model for the given year.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Ijs coefficient.
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the imaginary part of a nominal Love numbers.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the inclination of the magnetic field in degrees.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the increasing events time shift.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial frame in which the velocity increment is defined.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get an inertially oriented, body centered frame.
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator
Get the propagator initial state.
getInstance() - Static method in class org.orekit.data.DataProvidersManager
Get the unique instance.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Get the value of the instantaneous solar flux.
getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the integrator used by the propagator.
getInterpolatedDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the interpolated date.
getInterpolatedState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the interpolated state.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the interpolation method to be used.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getInverse() - Method in class org.orekit.frames.Transform
Get the inverse transform of the instance.
getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the specific impulse.
getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the ITRF2008 reference frame, using IERS 2010 conventions.
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the equinox-based ITRF reference frame.
getJ2000Day() - Method in class org.orekit.time.DateComponents
Get the day number with respect to J2000 epoch.
getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(double[][]) - Method in class org.orekit.frames.Transform
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform
Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.CartesianOrbit
 
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Jjs coefficient.
getJulianDay() - Method in class org.orekit.files.sp3.SP3File
Returns the julian day for this SP3 file.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Jupiter singleton body.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of eccentricity vector.
getKeplerianElementsComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for Keplerian elements.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit
Get the keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState
Get the keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit
Get the keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
Get the keplerian period.
getL() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon.
getL() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon.
getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument.
getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Get the last TLE.
getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Get the last date of the series.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the last known leap second.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the latest cached entry.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
 
getLatest() - Method in interface org.orekit.utils.TimeStampedCache
Get the latest entry in this cache.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the latitude.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMParser
Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch number.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMParser
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch piece.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMParser
Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch year.
getLE() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentric longitude.
getLightningRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lightning ratio ([0-1]).
getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the first line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the second line.
getLJu() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude.
getLJu() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Jupiter longitude.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState
Get the mean latitude argument (as per equinoctial parameters).
getLMa() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude.
getLMa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude.
getLMe() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude.
getLNe() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude.
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of Lns(γ).
getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get astronomical unit.
getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get a constant defined in the ephemerides headers.
getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the set of data file names that have been loaded.
getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get Earth/Moon mass ratio.
getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the gravitational coefficient of a body.
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
getLocalTemp() - Method in class org.orekit.forces.drag.JB2006
Get the temperature at input position.
getLOD() - Method in class org.orekit.frames.EOPEntry
Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLofType() - Method in enum org.orekit.files.ccsds.CCSDSFrame
Get the type of Local Orbital frame.
getLofType() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get coordinate system for covariance matrix, for Local Orbital Frames.
getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
Get an immutable copy of the logged events.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the longitude.
getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions
Get the Love numbers.
getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the lower case three letters abbreviation.
getLowerCaseName() - Method in enum org.orekit.time.Month
Get the lower case full name.
getLPrime() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun.
getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun.
getLSa() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude.
getLSa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude.
getLUr() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude.
getLv() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.SpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLVe() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude.
getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the differential equations to integrate (for main state only).
getMam() - Method in class org.orekit.forces.drag.DTM2000
Get the local mean atomic mass.
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator
Get all the names of all managed states.
getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile
Get a maneuver.
getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
Get a list of all maneuvers.
getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the angular margin to apply (radians).
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mars singleton body.
getMass() - Method in class org.orekit.files.ccsds.OGMFile
Get the spacecraft mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState
Gets the current mass.
getMatrix() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get the covariance matrix.
getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get a line of the matrix.
getMaxAlt() - Method in class org.orekit.forces.drag.HarrisPriester
Get the maximal altitude for the model.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal degree available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal order available in the last file parsed.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the maximal chunks duration.
getMaxDate() - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.JB2006InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported degree.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal number of iterations in the event time search.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported order.
getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter
Get the maximum derivation order.
getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter
Get the maximum derivation order.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the degree limit for the next file parsing.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the degree limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the order limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the order limit for the next file parsing.
getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum number of independent cached time slots.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum duration span in seconds of one slot.
getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean anomaly.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementTheory() - Method in class org.orekit.files.ccsds.OMMFile.OMMMetaData
Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile
Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian mean motion.
getMeanMotionDot() - Method in class org.orekit.files.ccsds.OMMFile
Get the first time derivative of the mean motion.
getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.OMMFile
Get the second time derivative of the mean motion.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion first derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion second derivative.
getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing mean obliquity of the ecliptic.
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mercury singleton body.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMetaData() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the meta-data for the block.
getMetaData() - Method in class org.orekit.files.ccsds.OGMFile
Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OMMFile
Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OPMFile
Get the meta data.
getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile
Get the comment for meta-data.
getMinAlt() - Method in class org.orekit.forces.drag.HarrisPriester
Get the minimal altitude for the model.
getMinDate() - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.JB2006InputParameters
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the first date of the range.
getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured minimum valid elevation value.
getMinute() - Method in class org.orekit.time.TimeComponents
Get the minute number.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMFile
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMParser
Get initial date.
getMjd() - Method in class org.orekit.frames.EOPEntry
Get the entry date (modified julian day, 00h00 UTC scale).
getMJD() - Method in class org.orekit.time.DateComponents
Get the modified julian day.
getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMode() - Method in class org.orekit.propagation.AbstractPropagator
Get the current operating mode of the propagator.
getMode() - Method in interface org.orekit.propagation.Propagator
Get the current operating mode of the propagator.
getModelName() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the model name.
getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Returns a Collection of the GeoMagneticField models that have been successfully loaded.
getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the momentum.
getMomentum() - Method in class org.orekit.utils.PVCoordinates
Gets the momentum.
getMonth() - Method in class org.orekit.time.DateComponents
Get the month.
getMonth(int) - Static method in enum org.orekit.time.Month
Get the month corresponding to a number.
getMonthEnum() - Method in class org.orekit.time.DateComponents
Get the month as an enumerate.
getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Moon singleton body.
getMu() - Method in class org.orekit.files.ccsds.ODMParser
Get gravitational coefficient.
getMu() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body attraction coefficient.
getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.orbits.Orbit
Get the central acceleration constant.
getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the Earth gravity coefficient used for TLE propagation.
getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.StateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.propagation.SpacecraftState
Get the central attraction coefficient.
getMuCreated() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient created from the knowledge of the central body.
getMuParsed() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient parsed in the ODM File.
getMuSet() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient set by the user.
getMuUsed() - Method in class org.orekit.files.ccsds.ODMFile
Get the used gravitational coefficient.
getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get n.
getNadir() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.frames.TopocentricFrame
Get the nadir direction of topocentric frame, expressed in parent shape frame.
getName() - Method in interface org.orekit.bodies.CelestialBody
Get the name of the body.
getName() - Method in class org.orekit.frames.Frame
Get the name.
getName() - Method in enum org.orekit.frames.Predefined
Get the name of the frame.
getName() - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.integration.AdditionalEquations
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the name of the partial Jacobians.
getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get the name of the additional state.
getName() - Method in class org.orekit.time.GalileoScale
Get the name time scale.
getName() - Method in class org.orekit.time.GMSTScale
Get the name time scale.
getName() - Method in class org.orekit.time.GPSScale
Get the name time scale.
getName() - Method in class org.orekit.time.TAIScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCBScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCGScale
Get the name time scale.
getName() - Method in class org.orekit.time.TDBScale
Get the name time scale.
getName() - Method in interface org.orekit.time.TimeScale
Get the name time scale.
getName() - Method in class org.orekit.time.TTScale
Get the name time scale.
getName() - Method in class org.orekit.time.UT1Scale
Get the name time scale.
getName() - Method in class org.orekit.time.UTCScale
Get the name time scale.
getNbManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
Get the number of maneuvers present in the OPM.
getNeighbors(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.GenericTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache
Get the entries surrounding a central date.
getNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the fixed size of the arrays to be returned by GenericTimeStampedCache.getNeighbors(AbsoluteDate).
getNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache
 
getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache
Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Neptune singleton body.
getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache
Get quantum gap above which a new slot is created instead of extending an existing one.
getNewtonianAttractionForceModel() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the Newtonian attraction from the central body force model.
getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory
Get the transform between two frames, suppressing all interpolation.
getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries
Get the number of different terms in the non-polynomial part.
getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNoradID() - Method in class org.orekit.files.ccsds.OMMFile
Get the NORAD Catalog Number ("Satellite Number").
getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get unit normal vector.
getNormal(AbsoluteDate, Frame, Vector3D, Rotation) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get solar array normal in spacecraft frame.
getNormal(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get solar array normal in spacecraft frame.
getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.
getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getNorth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.frames.TopocentricFrame
Get the north direction of topocentric frame, expressed in parent shape frame.
getNumber() - Method in enum org.orekit.time.Month
Get the month number.
getNumberOfEpochs() - Method in class org.orekit.files.ccsds.ODMFile
Not supported by CCSDS orbit messages.
getNumberOfEpochs() - Method in interface org.orekit.files.general.OrbitFile
Returns the number of epochs contained in this orbit file.
getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3File
Returns the number of epochs contained in this orbit file.
getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions
Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the nutation angles.
getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions
Get the reference epoch for fundamental nutation arguments.
getObjectID() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the spacecraft ID for which the orbit state is provided.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getObjectName() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the spacecraft name for which the orbit state is provided.
getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulted body.
getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulted body radius (m).
getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulting body.
getOccultingRadius() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulting body radius (m).
getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the configured ocean load deformation coefficients.
getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the ocean tides waves from the first supported file.
getODMFile() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the ODM file to which these meta-data belong.
getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the offset from reference date for the harmonics.
getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the offset from reference date for the harmonics.
getOmega() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOrbit() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesDataLine
Get the ephemerides data line orbit.
getOrbit() - Method in class org.orekit.propagation.SpacecraftState
Gets the current orbit.
getOrbitType() - Method in class org.orekit.files.sp3.SP3File
Returns the SP3File.SP3OrbitType for this SP3 file.
getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get propagation parameter type.
getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the ordinate grid for the interpolation function.
getOrientation() - Method in class org.orekit.attitudes.Attitude
Get the complete orientation including spin.
getOriginator() - Method in class org.orekit.files.ccsds.ODMFile
Get the file originator.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of inclination vector.
getPa() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.data.FieldBodiesElements
Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit argument of pericenter.
getParameter(String) - Method in class org.orekit.forces.drag.DragForce
getParameter(String) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
getParameter(String) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
getParameter(String) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
getParameter(String) - Method in class org.orekit.forces.gravity.NewtonianAttraction
getParameter(String) - Method in class org.orekit.forces.gravity.OceanTides
getParameter(String) - Method in class org.orekit.forces.gravity.Relativity
 
getParameter(String) - Method in class org.orekit.forces.gravity.SolidTides
getParameter(String) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
getParameter(String) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
getParameter(String) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
getParameter(String) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
getParameter(String) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
getParameter(String) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
getParameter(String) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
getParameterName() - Method in class org.orekit.propagation.numerical.ParameterConfiguration
Get parameter name.
getParameters() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the number of parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get theJacobian with respect to parameters from a one-dimensional additional state array.
getParametersNames() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
getParent() - Method in class org.orekit.frames.Frame
Get the parent frame.
getParentShape() - Method in class org.orekit.frames.TopocentricFrame
Get the body shape on which the local point is defined.
getPartialDensities(int) - Method in class org.orekit.forces.drag.DTM2000
Get the local partial density of the selected element.
getParts() - Method in exception org.orekit.errors.OrekitException
Get the variable parts of the error message.
getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit
Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the argument of perigee.
getPermanentTide() - Method in enum org.orekit.utils.IERSConventions
Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.
getPlaneSection(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.
getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the real part of a nominal Love numbers.
getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Pluto singleton body.
getPoint() - Method in class org.orekit.frames.TopocentricFrame
Get the surface point defining the origin of the frame.
getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the body North pole direction in ICRF frame.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the pole IERS Reference Pole correction.
getPolynomial() - Method in class org.orekit.data.PoissonSeries
Get the polynomial part of the series.
getPosition() - Method in class org.orekit.files.ccsds.OPMFile
Get position vector.
getPosition() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the position.
getPosition() - Method in class org.orekit.utils.PVCoordinates
Gets the position.
getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get propagation parameter type.
getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the precession angles.
getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local pressure at the evaluation location.
getPreviousDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the previous grid date.
getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the prime meridian angle.
getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the reference propagator.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider() - Method in class org.orekit.propagation.numerical.ParameterConfiguration
Get the povider handling this parameter.
getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Get the spherical harmonics provider.
getProviders() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the list of supported providers.
getPVCoordinates() - Method in class org.orekit.files.ccsds.OPMFile
Get the position/velocity coordinates contained in the OPM.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Get the extrapolated position and velocity from an initial date.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in given output frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider
Get the PVCoordinates of the body in the selected frame.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the body to align.
getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get PV coordinates provider.
getPVTarget() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get the position/velocity provider of the target .
getPVTarget() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the position/velocity provider of the target .
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of inclination vector.
getRaan() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit right ascension of ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE
Get Right Ascension of the Ascending node.
getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the underlying provider for raw (non-interpolated) transforms.
getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position-velocity at date.
getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
Get a spherical harmonic sine coefficient.
getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the critical distance.
getReal(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the real part of a nominal Love numbers.
getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate
Get the reference attitude.
getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the reference date for the harmonics.
getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the reference date for the harmonics.
getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper
Get reference date.
getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic
Get the reference date.
getReferenceFrame() - Method in class org.orekit.attitudes.Attitude
Get the reference frame.
getRefFrame() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get Coordinate system for velocity increment vector, for absolute frames.
getReflectionCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the specular reflection coefficient.
getReflectionCoefficient() - Method in interface org.orekit.forces.radiation.RadiationSensitive
Get the specular reflection coefficient.
getReflectionCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft
Get the specular reflection coefficient.
getRefLofType() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get coordinate system for velocity increment vector, for Local Orbital Frames.
getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel
Compute the refraction angle from the true (geometrical) elevation.
getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
 
getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured refraction model.
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the retrograde factor.
getRevAtEpoch() - Method in class org.orekit.files.ccsds.OMMFile
Get the revolution rumber.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the revolution number.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit
Get the right ascension of the ascending node.
getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the Root Mean Square Deviation of the fitting.
getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Rεn,m,l(γ).
getRoot() - Static method in class org.orekit.frames.Frame
Get the unique root frame.
getRotation() - Method in class org.orekit.attitudes.Attitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.frames.Transform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation.
getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the FieldRotation.
getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation acceleration.
getRotationRate() - Method in class org.orekit.frames.Transform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation rate.
getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the FieldRotation rate.
getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get s.
getS10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the EUV index (26-34 nm) scaled to F10.
getS10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the EUV 81-day averaged centered index.
getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the states sample.
getSatellite(String) - Method in class org.orekit.files.ccsds.OEMFile
Get additional information about a satellite.
getSatellite(String) - Method in class org.orekit.files.ccsds.OGMFile
Get additional information about a satellite.
getSatellite(String) - Method in interface org.orekit.files.general.OrbitFile
Get additional information about a satellite.
getSatellite(String) - Method in class org.orekit.files.sp3.SP3File
Get additional information about a satellite.
getSatellite(int) - Method in class org.orekit.files.sp3.SP3File
Returns the nth satellite as contained in the SP3 file.
getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.ODMFile
Get the time coordinates for the given satellite.
getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.OEMFile
Get the time coordinates for the given satellite.
getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.OPMFile
Get the time coordinates for the given satellite.
getSatelliteCoordinates(String) - Method in interface org.orekit.files.general.OrbitFile
Get the time coordinates for the given satellite.
getSatelliteCoordinates(String) - Method in class org.orekit.files.sp3.SP3File
Get the time coordinates for the given satellite.
getSatelliteCoordinatesOPM() - Method in class org.orekit.files.ccsds.OPMFile
Get the SatelliteTimeCoordinate of the OPM.
getSatelliteCount() - Method in class org.orekit.files.ccsds.OEMFile
Get the number of satellites contained in this orbit file.
getSatelliteCount() - Method in class org.orekit.files.ccsds.OGMFile
Get the number of satellites contained in this orbit file.
getSatelliteCount() - Method in interface org.orekit.files.general.OrbitFile
Get the number of satellites contained in this orbit file.
getSatelliteCount() - Method in class org.orekit.files.sp3.SP3File
Get the number of satellites contained in this orbit file.
getSatelliteId() - Method in class org.orekit.files.general.SatelliteInformation
Returns the id for this satellite object.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the satellite id.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatellites() - Method in class org.orekit.files.ccsds.OEMFile
Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.
getSatellites() - Method in class org.orekit.files.ccsds.OGMFile
Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.
getSatellites() - Method in interface org.orekit.files.general.OrbitFile
Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.
getSatellites() - Method in class org.orekit.files.sp3.SP3File
Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.
getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Saturn singleton body.
getSecond() - Method in class org.orekit.time.TimeComponents
Get the seconds number.
getSecondsInDay() - Method in class org.orekit.time.TimeComponents
Get the second number within the day.
getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3File
Returns the seconds of the GPS week as contained in the SP3 file.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the short periodic variations.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Computes the short periodic variations.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the short periodic variations.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the short periodic variations.
getSize() - Method in class org.orekit.utils.LoveNumbers
Get the size of the arrays.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Sj coefficient.
getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of slots in use.
getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of slots evictions.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the semi-major axis.
getSolarRadArea() - Method in class org.orekit.files.ccsds.OGMFile
Get the solar radiation pressure area.
getSolarRadCoeff() - Method in class org.orekit.files.ccsds.OGMFile
Get the solar radiation pressure coefficient.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the solar system barycenter aggregated body.
getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
getSourceString() - Method in enum org.orekit.errors.OrekitMessages
getSouth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.frames.TopocentricFrame
Get the south direction of topocentric frame, expressed in parent shape frame.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get spacecraft shape.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get spacecraft shape.
getSpacecraftComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for spacecraft.
getSpecifier() - Method in exception org.orekit.errors.OrekitException
Get the localizable specifier of the error message.
getSpin() - Method in class org.orekit.attitudes.Attitude
Get the satellite spin.
getStandardModel() - Static method in class org.orekit.models.earth.SaastamoinenModel
Create a new Saastamoinen model using a standard atmosphere model.
getStartDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the first available Earth Orientation Parameters.
getStartDate() - Method in class org.orekit.propagation.AbstractPropagator
Get the start date.
getStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get start of total time span covered by ephemerides data and covariance data.
getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the triggering state.
getStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the state vector dimension.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the grid points time step.
getStepHandler() - Method in class org.orekit.propagation.AbstractPropagator
Get the step handler.
getStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get end of total time span covered by ephemerides data and covariance data.
getStrengthLevel() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Get the strength level for activity.
getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Sun singleton body.
getSupportedNames() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Get the supported names for data files.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the regular expression for supported files names.
getSupportedNames() - Method in interface org.orekit.time.UTCTAILoader
Get the regular expression for supported UTC-TAI offsets files names.
getT() - Method in class org.orekit.forces.drag.DTM2000
Get the local temperature.
getTabDensity() - Method in class org.orekit.forces.drag.HarrisPriester
Get the current density table.
getTAI() - Static method in class org.orekit.time.TimeScalesFactory
Get the International Atomic Time scale.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the target point position/velocity in specified frame.
getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the size of the target.
getTC() - Method in class org.orekit.data.DelaunayArguments
Get the offset in Julian centuries.
getTC() - Method in class org.orekit.data.FieldDelaunayArguments
Get the offset in Julian centuries.
getTCB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Coordinate Time scale.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory
Get the Geocentric Coordinate Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Dynamic Time scale.
getTEME() - Static method in class org.orekit.frames.FramesFactory
Get the TEME reference frame.
getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local temperature at the evaluation location.
getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Get the value of the 3 hours geomagnetic index.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Get the value of the 3 hours geomagnetic index.
getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.EventDetector
Get the convergence threshold in the event time search.
getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust.
getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideSystem() - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the TideSystem used in the gravity field.
getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider
Get the TideSystem used in the gravity field.
getTime() - Method in class org.orekit.time.DateTimeComponents
Get the time component.
getTimeSystem() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
getTimeSystem() - Method in class org.orekit.files.ccsds.OEMFile
Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in class org.orekit.files.ccsds.OMMFile
Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in class org.orekit.files.ccsds.OPMFile
Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in interface org.orekit.files.general.OrbitFile
Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in class org.orekit.files.sp3.SP3File
Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTinf() - Method in class org.orekit.forces.drag.DTM2000
Get the current exospheric temperature above input position.
getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame.
getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the underlying TLE.
getTLERelatedParametersComment() - Method in class org.orekit.files.ccsds.OMMFile
Get the comment for TLE related parameters.
getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured topocentric frame definitions.
getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector
Get the total eclipse detection flag.
getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the total intensity of the magnetic field (= norm of the field vector).
getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
Get the transform from TOD at specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
Compute the transform at some date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
Get the Transform corresponding to specified date.
getTransformProvider() - Method in class org.orekit.frames.Frame
Get the provider for transform from parent frame to instance.
getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
Get the transform from the instance to another frame.
getTranslation() - Method in class org.orekit.frames.Transform
Get the underlying elementary translation.
getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the triggering event.
getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType
Get the increasing status of triggered events.
getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly.
getTT() - Static method in class org.orekit.time.TimeScalesFactory
Get the Terrestrial Time scale.
getType() - Method in class org.orekit.files.sp3.SP3File
Returns the SP3File.SP3FileType associated with this SP3 file.
getType() - Method in class org.orekit.orbits.CartesianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.CircularOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.KeplerianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.Orbit
Get the orbit type.
getU() - Method in class org.orekit.bodies.Ellipse
Get the unit vector along the major axis.
getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier
Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized
Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawCompensation
Get the underlying (ground pointing) attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawSteering
Get the underlying (ground pointing) attitude provider.
getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get a un-normalization factors array.
getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.
getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the upper case three letters abbreviation.
getUpperCaseName() - Method in enum org.orekit.time.Month
Get the upper case full name.
getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Uranus singleton body.
getUseableStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUserDefinedParameters() - Method in class org.orekit.files.ccsds.OGMFile
Get the map of user defined parameter keywords and their corresponding values.
getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry
Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUTC() - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time Coordinate scale.
getV() - Method in class org.orekit.bodies.Ellipse
Get the unit vector along the minor axis.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function value.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the Hansen coefficient Kj-n-1, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient K₀n, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the K₀-n-1,s coefficient value.
getValue(int, int, int, DerivativeStructure) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators
Get the Newcomb operator evaluated at n, s, ρ, σ.
getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the values samples for the interpolation function.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector f.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector g.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector w.
getVeis1950() - Static method in class org.orekit.frames.FramesFactory
Get the VEIS 1950 reference frame.
getVelocity() - Method in class org.orekit.files.ccsds.OPMFile
Get velocity vector.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.DTM2000
Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.HarrisPriester
Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.JB2006
Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity() - Method in class org.orekit.frames.Transform
Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the velocity.
getVelocity() - Method in class org.orekit.utils.PVCoordinates
Gets the velocity.
getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Venus singleton body.
getVmns(int, int, int, double, double) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Get the Vn,sm coefficient from Vn,s.
getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the loaded waves.
getWest() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.frames.TopocentricFrame
Get the west direction of topocentric frame, expressed in parent shape frame.
getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the WMM model for the given year.
getX() - Method in class org.orekit.frames.EOPEntry
Get the X component of the pole motion.
getXM10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the MG2 index scaled to F10.
getXM10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the MG2 81-day average centered index.
getXp() - Method in class org.orekit.frames.PoleCorrection
Get the xp parameter.
getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getY() - Method in class org.orekit.frames.EOPEntry
Get the Y component of the pole motion.
getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYear() - Method in class org.orekit.time.DateComponents
Get the year number.
getYp() - Method in class org.orekit.frames.PoleCorrection
Get the yp parameter.
getZenith() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.frames.TopocentricFrame
Get the zenith direction of topocentric frame, expressed in parent shape frame.
getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the geographic zone.
GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gjs, Hjs, Ijs and Jjs polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gmsj and the Hmsj polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Create a set of Gmsj and Hmsj polynomials.
GillIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GillIntegrator.
GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a new instance.
GMSTScale - Class in org.orekit.time
Greenwich Mean Sidereal Time.
GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
GPS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for GPS weeks: 1980-01-06.
GPSScale - Class in org.orekit.time
GPS time scale.
gradient(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the gradient of the non-central part of the gravity field.
gradientHessian(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute both the gradient and the hessian of the non-central part of the gravity field.
GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GraggBulirschStoerIntegrator.
GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a new instance.
GravityFieldFactory - Class in org.orekit.forces.gravity.potential
Factory used to read gravity field files in several supported formats.
GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for GRGS files.
GRGSFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the GRGS gravity field format.
GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².
GroundPointing - Class in org.orekit.attitudes
Base class for ground pointing attitude providers.
GroundPointing(Frame) - Constructor for class org.orekit.attitudes.GroundPointing
Default constructor.
GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.
GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.
GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRS80 model: 6378137.0 m.
GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRS80 model: 1.0 / 298.257222101.
GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².
GTODProvider - Class in org.orekit.frames
Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).
GTODProvider(IERSConventions, EOPHistory) - Constructor for class org.orekit.frames.GTODProvider
Simple constructor.
GZIP_FILE_PATTERN - Static variable in interface org.orekit.data.DataProvider
Pattern for name of gzip files.

H

h - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
ey.
H00 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 00:00:00.
H12 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 12:00:00.
handleStep(SpacecraftState, boolean) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Handle the last accepted step.
HansenTesseralLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t!=0 and n < 0.
HansenTesseralLinear(int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Constructor.
HansenThirdBodyLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n > 0.
HansenThirdBodyLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Constructor.
HansenUtilities - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Utilities class.
HansenZonalLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n < 0.
HansenZonalLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Constructor.
HarrisPriester - Class in org.orekit.forces.drag
This atmosphere model is the realization of the Modified Harris-Priester model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.forces.drag.HarrisPriester
Simple constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.forces.drag.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.forces.drag.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.forces.drag.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
hasAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Check if an additional state is available.
hasCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile
Check whether the OPM contains covariance matrix data.
hasDataFor(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Check if the cache has data for the given date using EOPHistory.getStartDate() and EOPHistory.getEndDate().
hashCode() - Method in class org.orekit.bodies.GeodeticPoint
 
hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey
hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
hashCode() - Method in class org.orekit.time.AbsoluteDate
Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.DateComponents
hashCode() - Method in class org.orekit.time.DateTimeComponents
hashCode() - Method in class org.orekit.time.TimeComponents
hasKeplerianElements() - Method in class org.orekit.files.ccsds.OGMFile
Check whether the OPM contains Keplerian elements data.
HELIUM - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for helium.
HelmertTransformation - Class in org.orekit.frames
Transformation class for geodetic systems.
HelmertTransformation(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.HelmertTransformation
Build a transform from its primitive operations.
HelmertTransformation.Predefined - Enum in org.orekit.frames
Enumerate for predefined Helmert transformations.
HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for HighamHall54Integrator.
HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a new instance.
HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Creates a new instance.
HolmesFeatherstoneAttractionModel.GradientHessian - Class in org.orekit.forces.gravity
Container for gradient and Hessian.
HolmesFeatherstoneAttractionModel.GradientHessian(double[], double[][]) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian
Simple constructor.
HYDROGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for hydrogen.

I

i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final inclination.
I - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Retrograde factor.
IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.
IAUPole - Interface in org.orekit.bodies
Interface for IAU pole and primer meridian orientations.
ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for ICGEM files.
ICGEMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the ICGEM gravity field format.
ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader
Simple constructor.
IDENTITY - Static variable in class org.orekit.frames.Transform
Identity transform.
IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
IERSConventions - Enum in org.orekit.utils
Supported IERS conventions.
IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils
Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.
ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
A cache of TimeStamped data that provides concurrency through immutability.
ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache
Create a new cache with the given neighbors size and data.
ImpulseManeuver<T extends EventDetector> - Class in org.orekit.forces.maneuvers
Impulse maneuver model.
ImpulseManeuver(T, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
ImpulseManeuver(T, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
InertialProvider - Class in org.orekit.attitudes
This class handles an inertial attitude provider.
InertialProvider(Rotation) - Constructor for class org.orekit.attitudes.InertialProvider
Creates new instance.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventFilter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Initialize step handler at the start of a propagation.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Check if the initial state is provided in osculating elements.
initialize(boolean) - Method in interface org.orekit.propagation.integration.ModeHandler
Initialize the mode handler.
initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, boolean) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Performs initialization at each integration step for the current force model.
initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Initialize the mapper.
initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.Orbit
Compute the position/velocity coordinates from the canonical parameters.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Check if date is within a leap second introduction.
IntegratedEphemeris - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, boolean, ContinuousOutputModel, Map<String, double[]>, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
interpolate(AbsoluteDate, Collection<Attitude>) - Method in class org.orekit.attitudes.Attitude
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<Transform>) - Method in class org.orekit.frames.Transform
Get an interpolated instance.
interpolate(AbsoluteDate, boolean, boolean, Collection<Transform>) - Static method in class org.orekit.frames.Transform
interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform
Interpolate a transform from a sample set of existing transforms.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.CartesianOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.CircularOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.EquinoctialOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.KeplerianOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftState
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolable
Get an interpolated instance.
interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, AngularCoordinates>>) - Static method in class org.orekit.utils.AngularCoordinates
interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, FieldAngularCoordinates<T>>>) - Static method in class org.orekit.utils.FieldAngularCoordinates
interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, FieldPVCoordinates<T>>>) - Static method in class org.orekit.utils.FieldPVCoordinates
interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, PVCoordinates>>) - Static method in class org.orekit.utils.PVCoordinates
interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedAngularCoordinates>) - Static method in class org.orekit.utils.TimeStampedAngularCoordinates
Interpolate angular coordinates.
interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Interpolate angular coordinates.
interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Interpolate position-velocity.
interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection<TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates
Interpolate position-velocity.
InterpolatingTransformProvider - Class in org.orekit.frames
Transform provider using thread-safe interpolation on transforms sample.
InterpolatingTransformProvider(TransformProvider, boolean, boolean, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider
InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider
Simple constructor.
InterpolationGrid - Interface in org.orekit.propagation.semianalytical.dsst.utilities
Interface for interpolation grids.
InterpolationTableLoader - Class in org.orekit.utils
Used to read an interpolation table from a data file.
InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader
 
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator
Check if an additional state is managed.
isAvailable(String) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Check if a parameter can be free.
isChildOf(Frame) - Method in class org.orekit.frames.Frame
Determine if a Frame is a child of another one.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE
Check the lines format validity.
isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Check is integration direction is forward in date.
isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the Increasing/decreasing status of the event.
isLof() - Method in enum org.orekit.files.ccsds.CCSDSFrame
Check if the frame is a Local Orbital frame.
isMeanOrbit() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Check if only the mean elements should be used in a semianalitical propagation.
isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Check if fitting uses only sample positions.
isPseudoInertial() - Method in class org.orekit.frames.Frame
Check if the frame is pseudo-inertial.
isSimpleEOP() - Method in class org.orekit.files.ccsds.ODMParser
Get EOP interpolation method.
isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Check if some provider is supported.
isSupported(String) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

J

J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
J2000_EPOCH - Static variable in class org.orekit.time.DateComponents
J2000.0 Reference epoch: 2000-01-01.
J2DifferentialEffect - Class in org.orekit.propagation.analytical
Analytical model for J2 effect.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
Jacobianizer - Class in org.orekit.propagation.numerical
Class helping implementation of partial derivatives in force models implementations.
Jacobianizer(ForceModel, double, Collection<ParameterConfiguration>, double) - Constructor for class org.orekit.propagation.numerical.Jacobianizer
Simple constructor.
JacobianPropagatorConverter - Class in org.orekit.propagation.conversion
Propagator converter using the real jacobian.
JacobianPropagatorConverter(NumericalPropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.JacobianPropagatorConverter
Simple constructor.
JacobiansMapper - Class in org.orekit.propagation.numerical
Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
JacobiPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Provider of the Jacobi polynomials Plv,w.
JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents
Java Reference epoch: 1970-01-01.
JB2006 - Class in org.orekit.forces.drag
This is the realization of the Jacchia-Bowman 2006 atmospheric model.
JB2006(JB2006InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.JB2006
Constructor with space environment information for internal computation.
JB2006InputParameters - Interface in org.orekit.forces.drag
Interface for solar activity and magnetic activity data.
JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical Unit: 149597870691 m.
JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants
Earth attraction coefficient (m³/s²).
JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Earth/Moon mass ratio: 81.30059.
JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) attraction coefficient (m³/s²).
JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants
Gaussian gravitational constant: 0.01720209895 √(AU³/d²).
JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) ttraction coefficient (m³/s²).
JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) attraction coefficient (m³/s²).
JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants
Sun/Mercury attraction coefficient (m³/s²).
JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants
Moon attraction coefficient (m³/s²).
JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) attraction coefficient (m³/s²).
JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) ttraction coefficient (m³/s²).
JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) attraction coefficient (m³/s²).
JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) mass ratio: 328900.56.
JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants
Sun attraction coefficient (m³/s²).
JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) mass ratio: 1047.3486.
JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) mass ratio: 3098708.0.
JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Mercury mass ratio: 6023600.
JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) mass ratio: 19412.24.
JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) mass ratio: 1.35e8.
JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) mass ratio: 3497.898.
JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) mass ratio: 22902.98.
JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Venus mass ratio: 408523.71.
JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) attraction coefficient (m³/s²).
JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants
Sun/Venus attraction coefficient (m³/s²).
JPLEphemeridesLoader - Class in org.orekit.bodies
Loader for JPL ephemerides binary files (DE 4xx) and similar formats (INPOP 06/08/10).
JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader
Create a loader for JPL ephemerides binary files.
JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies
List of supported ephemerides types.
JPLEphemeridesLoader.RawPVProvider - Interface in org.orekit.bodies
Interface for raw position-velocity retrieval.
JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants
Duration of a Julian century: 36525 Constants.JULIAN_DAY.
JULIAN_DAY - Static variable in interface org.orekit.utils.Constants
Duration of a mean solar day: 86400.0 s.
JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for julian dates: -4712-01-01.
JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Julian year: 365.25 Constants.JULIAN_DAY.
JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Jupiter.

K

k - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
ex.
KeplerianOrbit - Class in org.orekit.orbits
This class handles traditional keplerian orbital parameters.
KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from cartesian parameters.
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from cartesian parameters.
KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from any kind of orbital parameters.
KeplerianPropagator - Class in org.orekit.propagation.analytical
Simple keplerian orbit propagator.
KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit only.
KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and attitude provider.
KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Keplerian propagator.
KeplerianPropagatorBuilder(double, Frame) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new instance.
Keyword - Enum in org.orekit.files.ccsds
Keywords for CCSDS orbit data messages.

L

lm - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Mean longitude.
LnsCoefficients - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Lns(γ).
LnsCoefficients(int, int, double[][], TreeMap<CoefficientsFactory.NSKey, Double>, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Create a set of Lns(γ) coefficients.
loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader
Load celestial body.
loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Load celestial body.
loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCHatEpsilonReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCnmSnmReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.utils.InterpolationTableLoader
Loads an bi-variate interpolation table from the given InputStream.
loadLoveNumbers(String) - Method in enum org.orekit.utils.IERSConventions
Load the Love numbers.
loadTimeSteps() - Method in interface org.orekit.time.UTCTAILoader
Load UTC-TAI offsets entries.
loadTLEData() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Load TLE data for a specified object.
loadTLEData(int) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Load TLE data for a specified object.
loadTLEData(int, int, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Load TLE data for a specified object.
LocalOrbitalFrame - Class in org.orekit.frames
Class for frames moving with an orbiting satellite.
LocalOrbitalFrame(Frame, LOFType, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame
Build a new instance.
LofOffset - Class in org.orekit.attitudes
Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.
LofOffset(Frame, LOFType) - Constructor for class org.orekit.attitudes.LofOffset
Create a LOF-aligned attitude.
LofOffset(Frame, LOFType, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset
Creates new instance.
LofOffsetPointing - Class in org.orekit.attitudes
This class provides a default attitude provider.
LofOffsetPointing(BodyShape, AttitudeProvider, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing
Creates new instance.
LOFType - Enum in org.orekit.frames
Enumerate for different types of Local Orbital Frames.
LoveNumbers - Class in org.orekit.utils
Container for Love numbers.
LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers
Simple constructor.

M

mapArrayToOrbit(double[], PositionAngle, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType
Convert state array to orbital parameters.
mapArrayToState(double, double[], boolean) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper
Map a date to a raw double time offset.
mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double time offset to a date.
mapOrbitToArray(Orbit, PositionAngle, double[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mapStateToArray(SpacecraftState, double[]) - Method in class org.orekit.propagation.integration.StateMapper
Map a spacecraft state to raw double components.
MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mars.
MarshallSolarActivityFutureEstimation - Class in org.orekit.forces.drag
This class reads and provides solar activity data needed by atmospheric models: F107 solar flux and Kp indexes.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation
Simple constructor.
MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.forces.drag
Strength level of activity.
MASTER_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for master mode.
meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean derivative, truncated to first components.
meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean second derivative, truncated to first components.
meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean value, truncated to first components.
MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mercury.
MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for MidpointIntegrator.
MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a new instance.
missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if missing coefficients are allowed in the input data.
ModeHandler - Interface in org.orekit.propagation.integration
Common interface for all propagator mode handlers initialization.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for modified julian dates: 1858-11-17.
MOLECULAR_NITROGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for molecular nitrogen.
MOLECULAR_OXYGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for molecular oxygen.
monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger
Monitor an event detector.
Month - Enum in org.orekit.time
Enumerate representing a calendar month.
MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Moon.
MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Moon equatorial radius: 1737400 m.
mu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
μ .
multiply(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Multiply the argument matrix with the current matrix.

N

n - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Kepler mean motion: n = sqrt(μ / a³).
NadirPointing - Class in org.orekit.attitudes
This class handles nadir pointing attitude provider.
NadirPointing(BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing
Creates new instance.
negate() - Method in class org.orekit.utils.FieldPVCoordinates
Get the opposite of the instance.
negate() - Method in class org.orekit.utils.PVCoordinates
Get the opposite of the instance.
NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Neptune.
NetworkCrawler - Class in org.orekit.data
Provider for data files directly fetched from network.
NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler
Build a data classpath crawler.
newBundle(String, Locale, String, ClassLoader, boolean) - Method in class org.orekit.errors.OrekitMessages.UTF8Control
NewcombOperators - Class in org.orekit.propagation.semianalytical.dsst.utilities
Implementation of the Modified Newcomb Operators.
NewtonianAttraction - Class in org.orekit.forces.gravity
Force model for Newtonian central body attraction.
NewtonianAttraction(double) - Constructor for class org.orekit.forces.gravity.NewtonianAttraction
Simple constructor.
NodeDetector - Class in org.orekit.propagation.events
Finder for node crossing events.
NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
nonCentralPart(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the non-central part of the gravity field.
normalize() - Method in class org.orekit.utils.FieldPVCoordinates
Normalize the position part of the instance.
normalize() - Method in class org.orekit.utils.PVCoordinates
Normalize the position part of the instance.
NormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide normalized spherical harmonics coefficients.
NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
The normalized geopotential coefficients at a specific instance in time.
NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection
Null correction (xp = 0, yp = 0).
NumericalPropagator - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
NumericalPropagator(AbstractIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
NumericalPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for numerical propagator.
NumericalPropagatorBuilder(double, Frame, FirstOrderIntegratorBuilder) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new instance.

O

OceanLoadDeformationCoefficients - Enum in org.orekit.forces.gravity.potential
Supported Ocean load Deformation coefficients (Love numbers k'i).
OceanTides - Class in org.orekit.forces.gravity
Ocean tides force model.
OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTidesReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides coefficients.
OceanTidesReader(String) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesReader
Simple constructor.
OceanTidesWave - Class in org.orekit.forces.gravity.potential
Container for ocen tides coefficients for one tide wave.
OceanTidesWave(int, int, int, double[][][]) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesWave
Simple constructor.
ODMFile - Class in org.orekit.files.ccsds
The ODMFile (Orbit Data Message) class represents any of the three orbit messages used by the CCSDS, i.e.
ODMFile() - Constructor for class org.orekit.files.ccsds.ODMFile
ODMFile constructor.
ODMMetaData - Class in org.orekit.files.ccsds
This class gathers the meta-data present in the Orbital Data Message (ODM).
ODMParser - Class in org.orekit.files.ccsds
Base class for all CCSDS Orbit Data Message parsers.
ODMParser(AbsoluteDate, double, IERSConventions, boolean, int, int, String) - Constructor for class org.orekit.files.ccsds.ODMParser
Complete constructor.
OEMFile - Class in org.orekit.files.ccsds
This class stocks all the information of the OEM File parsed by OEMParser.
OEMFile() - Constructor for class org.orekit.files.ccsds.OEMFile
OEMFile constructor.
OEMFile.CovarianceMatrix - Class in org.orekit.files.ccsds
The CovarianceMatrix class represents a covariance matrix and its metadata: epoch and frame.
OEMFile.EphemeridesBlock - Class in org.orekit.files.ccsds
The Ephemerides Blocks class contain metadata, the list of ephemerides data lines and optional covariance matrices (and their metadata).
OEMFile.EphemeridesBlock() - Constructor for class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
EphemeridesBlock constructor.
OEMFile.EphemeridesDataLine - Class in org.orekit.files.ccsds
The EphemeridesDataLine class represents the content of an OEM ephemerides data line and consists of a cartesian orbit and an optional acceleration vector.
OEMParser - Class in org.orekit.files.ccsds
A parser for the CCSDS OEM (Orbit Ephemeris Message).
OEMParser() - Constructor for class org.orekit.files.ccsds.OEMParser
Simple constructor.
offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
Compute the seconds offset between two instances.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GalileoScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GMSTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UT1Scale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from TAIScale to instance.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GalileoScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GMSTScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TCBScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UT1Scale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from instance to TAIScale.
OGMFile - Class in org.orekit.files.ccsds
This class gathers the general state data present in both OPM and OMM files.
omega - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final perigee argument.
omgdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for perigee argument (omega) computation.
OMMFile - Class in org.orekit.files.ccsds
This class gathers the informations present in the Orbital Mean-Elements Message (OMM), and contains methods to generate a CartesianOrbit, a KeplerianOrbit, a SpacecraftState and, eventually, a TLE.
OMMFile.OMMMetaData - Class in org.orekit.files.ccsds
 
OMMParser - Class in org.orekit.files.ccsds
A parser for the CCSDS OMM (Orbiter Mean-Elements Message).
OMMParser() - Constructor for class org.orekit.files.ccsds.OMMParser
Simple constructor.
onDate(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider
Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider
Get the raw spherical harmonic coefficients on a specific date.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider
Get the un-normalized spherical harmonic coefficients at a specific instance in time.
ONE - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
1 represented as a polynomial.
OneAxisEllipsoid - Class in org.orekit.bodies
Modeling of a one-axis ellipsoid.
OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid
Simple constructor.
ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
1 / A .
ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
1 / (A * B) .
ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
1 / (1 + B) .
ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
1 / μ .
OPMFile - Class in org.orekit.files.ccsds
This class gathers the informations present in the Orbital Parameter Message (OPM), and contains methods to generate CartesianOrbit, KeplerianOrbit or SpacecraftState.
OPMFile.Maneuver - Class in org.orekit.files.ccsds
Maneuver in an OPM file.
OPMFile.Maneuver() - Constructor for class org.orekit.files.ccsds.OPMFile.Maneuver
Simple constructor.
OPMParser - Class in org.orekit.files.ccsds
A parser for the CCSDS OPM (Orbit Parameter Message).
OPMParser() - Constructor for class org.orekit.files.ccsds.OPMParser
Simple constructor.
Orbit - Class in org.orekit.orbits
This class handles orbital parameters.
Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit
Default constructor.
Orbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.Orbit
Set the orbit from Cartesian parameters.
OrbitFile - Interface in org.orekit.files.general
Interface for orbit file representations.
OrbitFile.TimeSystem - Enum in org.orekit.files.general
Time system used throughout this orbit file.
OrbitFileParser - Interface in org.orekit.files.general
Interface for orbit file parsers.
OrbitType - Enum in org.orekit.orbits
Enumerate for orbital parameters types.
OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager
Name of the property defining the root directories or zip/jar files path for default configuration.
OrekitConfiguration - Class in org.orekit.utils
Utility class for setting global configuration parameters.
OrekitException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by the orekit classes.
OrekitException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException
Copy constructor.
OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(ExceptionContextProvider) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitExceptionWrapper - Exception in org.orekit.errors
This class allows to wrap OrekitException instances in RuntimeException.
OrekitExceptionWrapper(OrekitException) - Constructor for exception org.orekit.errors.OrekitExceptionWrapper
Simple constructor.
OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
OrekitMessages - Enum in org.orekit.errors
Enumeration for localized messages formats.
OrekitMessages.UTF8Control - Class in org.orekit.errors
Control class loading properties in UTF-8 encoding.
OrekitMessages.UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control
 
OrekitStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
OrekitStepHandlerMultiplexer - Class in org.orekit.propagation.sampling
This class gathers several OrekitStepHandler instances into one.
OrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Simple constructor.
OrekitStepInterpolator - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
OrekitStepNormalizer - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer
Simple constructor.
org.orekit.attitudes - package org.orekit.attitudes
This package provides classes to represent simple attitudes.
org.orekit.bodies - package 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 - package 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.errors - package org.orekit.errors
This package provides classes to generate and handle exceptions.
org.orekit.files.ccsds - package org.orekit.files.ccsds
This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.
org.orekit.files.general - package org.orekit.files.general
This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.files.sp3 - package org.orekit.files.sp3
This package provides a parser for orbit data stored in SP3 format.
org.orekit.forces - package 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 - package org.orekit.forces.drag
 
org.orekit.forces.gravity - package org.orekit.forces.gravity
This package provides all gravity-related forces.
org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential
This package provides classes to read gravity field files and supports several different formats.
org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers
This package provides models of simple maneuvers.
org.orekit.forces.radiation - package org.orekit.forces.radiation
 
org.orekit.frames - package org.orekit.frames
This package provides classes to handle frames and transforms between them.
org.orekit.models - package org.orekit.models
 
org.orekit.models.earth - package org.orekit.models.earth
This package provides models that simulate certain physical phenomena experienced in the atmosphere of the earth.
org.orekit.orbits - package org.orekit.orbits
This package provides classes to represent orbits.
org.orekit.propagation - package org.orekit.propagation
This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.analytical - package org.orekit.propagation.analytical
 
org.orekit.propagation.analytical.tle - package org.orekit.propagation.analytical.tle
This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion - package org.orekit.propagation.conversion
This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.events - package org.orekit.propagation.events
This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.events.handlers - package org.orekit.propagation.events.handlers
This package provides an interface and classes dealing with events occurrence only.
org.orekit.propagation.integration - package org.orekit.propagation.integration
 
org.orekit.propagation.numerical - package org.orekit.propagation.numerical
 
org.orekit.propagation.sampling - package org.orekit.propagation.sampling
This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.propagation.semianalytical.dsst - package org.orekit.propagation.semianalytical.dsst
This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces - package org.orekit.propagation.semianalytical.dsst.forces
 
org.orekit.propagation.semianalytical.dsst.utilities - package org.orekit.propagation.semianalytical.dsst.utilities
 
org.orekit.propagation.semianalytical.dsst.utilities.hansen - package org.orekit.propagation.semianalytical.dsst.utilities.hansen
 
org.orekit.time - package org.orekit.time
This independent package provides classes to handle epochs, time scales, and to compare instants together.
org.orekit.utils - package org.orekit.utils
This package provides useful objects.
OrphanFrame - Class in org.orekit.frames
Prototype frame that can be built from leaf to roots and later attached to a tree.
OrphanFrame(String) - Constructor for class org.orekit.frames.OrphanFrame
Simple constructor.
osculatingDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating derivative.
osculatingSecondDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating second derivative.
OsculatingToMeanElementsConverter - Class in org.orekit.propagation.conversion
This class converts osculating orbital elements into mean elements.
OsculatingToMeanElementsConverter(SpacecraftState, int, Propagator) - Constructor for class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Constructor.
osculatingValue(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating value.

P

p - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
hy.
ParameterConfiguration - Class in org.orekit.propagation.numerical
Simple container associating a parameter name with a step to compute its jacobian and the provider that manages it.
ParameterConfiguration(String, double) - Constructor for class org.orekit.propagation.numerical.ParameterConfiguration
Parameter name and step pair constructor.
parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser
Parse a stream.
parse(String) - Method in class org.orekit.data.PolynomialParser
Parse a polynomial expression.
parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser
Parse a stream.
parse(String) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OEMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OEMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OMMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OMMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OPMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OPMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in interface org.orekit.files.general.OrbitFileParser
Reads an orbit file from the given stream and returns a parsed OrbitFile.
parse(String) - Method in interface org.orekit.files.general.OrbitFileParser
Reads the orbit file and returns a parsed OrbitFile.
parse(String) - Method in class org.orekit.files.sp3.SP3Parser
Reads the orbit file and returns a parsed OrbitFile.
parse(InputStream) - Method in class org.orekit.files.sp3.SP3Parser
Reads an orbit file from the given stream and returns a parsed OrbitFile.
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSFrame(String) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS frame.
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCoefficient(String, List<List<Double>>, int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a coefficient.
parseCoefficient(String, double[][], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a coefficient.
parseComment(KeyValue, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse a comment line.
parseDate(String, OrbitFile.TimeSystem) - Method in class org.orekit.files.ccsds.ODMParser
Parse a date.
parseDate(String) - Static method in class org.orekit.time.DateComponents
Parse a string in ISO-8601 format to build a date.
parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents
Parse a string in ISO-8601 format to build a date/time.
parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a double from a string.
parseGeneralStateDataEntry(KeyValue, OGMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse a general state data key = value entry.
parseHeaderEntry(KeyValue, ODMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse an entry from the header.
parseMetaDataEntry(KeyValue, ODMMetaData, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse a meta-data key = value entry.
parseMonth(String) - Static method in enum org.orekit.time.Month
Parse the string to get the month.
parseTime(String) - Static method in class org.orekit.time.TimeComponents
Parse a string in ISO-8601 format to build a time.
PartialDerivativesEquations - Class in org.orekit.propagation.numerical
Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.
PartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.PartialDerivativesEquations
Simple constructor.
PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the past direction.
perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
perigee, expressed in KM and ALTITUDE.
PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Pluto.
pointAt(double) - Method in class org.orekit.bodies.Ellipse
Get a point of the 2D ellipse.
pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the point observed from the station at some specified distance.
PoissonSeries<T extends RealFieldElement<T>> - Class in org.orekit.data
Class representing a Poisson series for nutation or ephemeris computations.
PoissonSeries(PolynomialNutation<T>, Map<Long, SeriesTerm<T>>) - Constructor for class org.orekit.data.PoissonSeries
Build a Poisson series from an IERS table file.
PoissonSeries.CompiledSeries<S extends RealFieldElement<S>> - Interface in org.orekit.data
This interface represents a fast evaluator for Poisson series.
PoissonSeriesParser<T extends RealFieldElement<T>> - Class in org.orekit.data
Parser for Poisson series files.
PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser
Build a parser for a Poisson series from an IERS table file.
PoleCorrection - Class in org.orekit.frames
Simple container class for pole correction parameters.
PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection
Simple constructor.
PolynomialFunctionMatrix - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
A quadratic matrix of PolynomialFunction.
PolynomialNutation<T extends RealFieldElement<T>> - Class in org.orekit.data
Polynomial nutation function.
PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation
Build a polynomial from its coefficients.
PolynomialParser - Class in org.orekit.data
Parser for polynomials in IERS tables.
PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser
Simple constructor.
PolynomialParser.Unit - Enum in org.orekit.data
Unit for the coefficients.
PositionAngle - Enum in org.orekit.orbits
Enumerate for true, eccentric and mean position angles.
PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential
This abstract class represents a Gravitational Potential Coefficients file reader.
PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Simple constructor.
Predefined - Enum in org.orekit.frames
Predefined frames provided by FramesFactory.
projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the closest ellipse point.
projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse
Project position-velocity-acceleration on an ellipse.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a moving point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a moving point to the ground.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagation with or without event detection.
propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate from a start date towards a target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Extrapolate an orbit up to a specific target date.
PropagationException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by during the propagation computation.
PropagationException(Localizable, Object...) - Constructor for exception org.orekit.errors.PropagationException
Simple constructor.
PropagationException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.PropagationException
Simple constructor.
PropagationException(OrekitException) - Constructor for exception org.orekit.errors.PropagationException
Simple constructor.
PropagationException(ExceptionContextProvider) - Constructor for exception org.orekit.errors.PropagationException
Simple constructor.
Propagator - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
PropagatorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build propagators for conversion.
PropagatorConverter - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction for propagators conversions.
PVCoordinates - Class in org.orekit.utils
Simple container for Position/Velocity/Acceleration triplets.
PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates
Simple constructor.
PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet with zero acceleration.
PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet.
PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Multiplicative constructor.
PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Subtractive constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
PVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers.

Q

q - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
hx.

R

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure, with state derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure, with state derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in class org.orekit.forces.SphericalSpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.SphericalSpacecraft
Compute the acceleration due to radiation pressure, with state derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in class org.orekit.forces.SphericalSpacecraft
Compute the acceleration due to radiation pressure, with parameters derivatives.
RadiationSensitive - Interface in org.orekit.forces.radiation
Interface for spacecraft that are sensitive to radiation pressure forces.
RAPID_DATA_PREDICITON_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).
RAPID_DATA_PREDICITON_XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP XML files (IAU2000 compatibles).
RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).
RAPID_DATA_PREDICTION_XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP XML files (IAU1980 compatibles).
RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide raw spherical harmonics coefficients.
RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
The raw spherical harmonics at a particular instant.
readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Read a gravity field coefficients provider from the first supported file.
REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for reflection coefficient.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Register an attitude provider.
registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
reinitializeBegin(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.EventState
Reinitialize the beginning of the step.
Relativity - Class in org.orekit.forces.gravity
Post-Newtonian correction force due to general relativity.
Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity
Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.
removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Remove all perturbing force models from the global perturbation model.
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Remove all perturbing force models from the global perturbation model.
removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Remove one provider.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Determines whether this handler needs dense output.
rescale(double, boolean, double[][], double[][], boolean, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Rescale coefficients arrays.
reset(SpacecraftState) - Method in class org.orekit.propagation.events.EventState
Let the event detector reset the state if it wants.
resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence
Reset the active provider.
resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic
Reset fitting.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris
Try (and fail) to reset the initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Reset the initial state.
resetShortPeriodicsCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Reset the coefficients used for short periodic variations.
resetShortPeriodicsCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody
Reset the coefficients used for short periodic variations.
resetShortPeriodicsCoefficients() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Reset the coefficients used for short periodic variations.
resetShortPeriodicsCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
 
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent
Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing
Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnEvent
Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing
Reset the state prior to continue propagation.
revert() - Method in class org.orekit.utils.AngularCoordinates
Revert a rotation/rotation rate/ rotation acceleration triplet.
revert() - Method in class org.orekit.utils.FieldAngularCoordinates
Revert a FieldRotation/FieldRotation/FieldRotation acceleration triplet.
revert() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Revert a rotation/rotation rate pair.
revert() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Revert a rotation/rotation rate pair.
rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.

S

s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
s* new value for the contant s.
SaastamoinenModel - Class in org.orekit.models.earth
The modified Saastamoinen model.
SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.SaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
SatelliteInformation - Class in org.orekit.files.general
Contains general information about a satellite as contained in an orbit file.
SatelliteInformation(String) - Constructor for class org.orekit.files.general.SatelliteInformation
Create a new SatelliteInformation object with a given satellite id.
SatelliteTimeCoordinate - Class in org.orekit.files.general
Contains the position/velocity of a satellite at an specific epoch.
SatelliteTimeCoordinate(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.files.general.SatelliteTimeCoordinate
Creates a new SatelliteTimeCoordinate instance with a given epoch and coordinate.
SatelliteTimeCoordinate(AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.files.general.SatelliteTimeCoordinate
Creates a new