Uses of Class
org.orekit.orbits.OrbitType

Packages that use OrbitType

Package	Description
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation	Propagation
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.utils	This package provides useful objects.

Uses of OrbitType in org.orekit.orbits

Methods in org.orekit.orbits that return OrbitType

Modifier and Type	Method	Description
OrbitType	CartesianOrbit.getType()	Get the orbit type.
OrbitType	CircularOrbit.getType()	Get the orbit type.
OrbitType	EquinoctialOrbit.getType()	Get the orbit type.
OrbitType	FieldCartesianOrbit.getType()	Get the orbit type.
OrbitType	FieldCircularOrbit.getType()	Get the orbit type.
OrbitType	FieldEquinoctialOrbit.getType()	Get the orbit type.
OrbitType	FieldKeplerianOrbit.getType()	Get the orbit type.
abstract OrbitType	FieldOrbit.getType()	Get the orbit type.
OrbitType	KeplerianOrbit.getType()	Get the orbit type.
abstract OrbitType	Orbit.getType()	Get the orbit type.
static OrbitType	OrbitType.valueOf(String name)	Returns the enum constant of this type with the specified name.
static OrbitType[]	OrbitType.values()	Returns an array containing the constants of this enum type, in the order they are declared.

Uses of OrbitType in org.orekit.propagation

Methods in org.orekit.propagation that return OrbitType

Modifier and Type	Method	Description
OrbitType	StateCovarianceMatrixProvider.getCovarianceOrbitType()	Get the orbit type in which the covariance matrix is expressed.
OrbitType	FieldStateCovariance.getOrbitType()	Get the covariance orbit type.
OrbitType	MatricesHarvester.getOrbitType()	Get the orbit type used for the matrix computation.
OrbitType	StateCovariance.getOrbitType()	Get the covariance orbit type.
OrbitType	AbstractStateCovarianceInterpolator.getOutOrbitType()	Get output orbit type.

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

Modifier and Type	Method	Description
FieldStateCovariance<T>	FieldStateCovariance.changeCovarianceType(FieldOrbit<T> orbit, OrbitType outOrbitType, PositionAngleType outAngleType)	Get the covariance matrix in another orbit type.
StateCovariance	StateCovariance.changeCovarianceType(Orbit orbit, OrbitType outOrbitType, PositionAngleType outAngleType)	Get the covariance matrix in another orbit type.
static void	StateCovariance.checkFrameAndOrbitTypeConsistency(Frame covarianceFrame, OrbitType inputType)	Check constructor's inputs consistency.
StateCovariance	StateCovarianceMatrixProvider.getStateCovariance(SpacecraftState state, OrbitType orbitType, PositionAngleType angleType)	Get the state covariance expressed in a given orbit type.

Constructors in org.orekit.propagation with parameters of type OrbitType

Constructor	Description
AbstractStateCovarianceInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor.
FieldStateCovariance(FieldMatrix<T> orbitalCovariance, FieldAbsoluteDate<T> epoch, Frame covarianceFrame, OrbitType orbitType, PositionAngleType angleType)	Constructor.
StateCovariance(RealMatrix orbitalCovariance, AbsoluteDate epoch, Frame covarianceFrame, OrbitType orbitType, PositionAngleType angleType)	Constructor.
StateCovarianceBlender(SmoothStepFactory.SmoothStepFunction blendingFunction, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor.
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, CartesianDerivativesFilter filter, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor using an output frame.
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, TimeInterpolator<Orbit> orbitInterpolator, CartesianDerivativesFilter filter, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor using an output frame and : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

Uses of OrbitType in org.orekit.propagation.analytical

Methods in org.orekit.propagation.analytical that return OrbitType

Modifier and Type	Method	Description
OrbitType	AbstractAnalyticalMatricesHarvester.getOrbitType()	Get the orbit type used for the matrix computation.

Uses of OrbitType in org.orekit.propagation.conversion

Methods in org.orekit.propagation.conversion that return OrbitType

Modifier and Type	Method	Description
OrbitType	AbstractPropagatorBuilder.getOrbitType()	Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
OrbitType	PropagatorBuilder.getOrbitType()	Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

Methods in org.orekit.propagation.conversion with parameters of type OrbitType

Modifier and Type	Method	Description
abstract AbstractFieldIntegrator<T>	AbstractFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	AbstractFieldIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType)	Build a first order integrator.
abstract AbstractFieldIntegrator<T>	AbstractVariableStepFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	AdamsBashforthFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	AdamsBashforthIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	AdamsMoultonFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	AdamsMoultonIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	ClassicalRungeKuttaFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	ClassicalRungeKuttaIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	DormandPrince54FieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	DormandPrince54IntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	DormandPrince853FieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	DormandPrince853IntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	EulerFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	EulerIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	FieldODEIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	FieldODEIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	GillFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	GillIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	GraggBulirschStoerIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	HighamHall54FieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	HighamHall54IntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	LutherFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	LutherIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	MidpointFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	MidpointIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	ODEIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractFieldIntegrator<T>	ThreeEighthesFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
AbstractIntegrator	ThreeEighthesIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.

Constructors in org.orekit.propagation.conversion with parameters of type OrbitType

Constructor	Description
BrouwerLyddanePropagatorBuilder(Orbit templateOrbit, double referenceRadius, double mu, TideSystem tideSystem, double c20, double c30, double c40, double c50, OrbitType orbitType, PositionAngleType positionAngleType, double positionScale, double M2)	Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit templateOrbit, double referenceRadius, double mu, TideSystem tideSystem, double c20, double c30, double c40, double c50, double c60, OrbitType orbitType, PositionAngleType positionAngleType, double positionScale)	Build a new instance.

Uses of OrbitType in org.orekit.propagation.events

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

Modifier and Type	Method	Description
OrbitType	PositionAngleDetector.getOrbitType()	Get the orbit type defining the angle type.

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

Constructor	Description
PositionAngleDetector(double maxCheck, double threshold, OrbitType orbitType, PositionAngleType positionAngleType, double angle)	Build a detector.
PositionAngleDetector(OrbitType orbitType, PositionAngleType positionAngleType, double angle)	Build a new detector.
PositionAngleDetector(AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler, OrbitType orbitType, PositionAngleType positionAngleType, double angle)	Protected constructor with full parameters.

Uses of OrbitType in org.orekit.propagation.integration

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

Modifier and Type	Method	Description
protected OrbitType	AbstractIntegratedPropagator.getOrbitType()	Get propagation parameter type.
protected OrbitType	FieldAbstractIntegratedPropagator.getOrbitType()	Get propagation parameter type.
OrbitType	FieldStateMapper.getOrbitType()	Get propagation parameter type.
OrbitType	StateMapper.getOrbitType()	Get propagation parameter type.

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

Modifier and Type	Method	Description
protected abstract StateMapper	AbstractIntegratedPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state.
protected abstract FieldStateMapper<T>	FieldAbstractIntegratedPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state.
protected void	AbstractIntegratedPropagator.setOrbitType(OrbitType orbitType)	Set propagation orbit type.
protected void	FieldAbstractIntegratedPropagator.setOrbitType(OrbitType orbitType)	Set propagation orbit type.

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

Constructor	Description
FieldStateMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Simple constructor.
StateMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Simple constructor.

Uses of OrbitType in org.orekit.propagation.numerical

Methods in org.orekit.propagation.numerical that return OrbitType

Modifier and Type	Method	Description
OrbitType	FieldNumericalPropagator.getOrbitType()	Get propagation parameter type.
OrbitType	NumericalPropagator.getOrbitType()	Get propagation parameter type.

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

Modifier and Type	Method	Description
protected FieldStateMapper<T>	FieldNumericalPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state.
protected StateMapper	GLONASSNumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)
protected StateMapper	NumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state.
void	FieldNumericalPropagator.setOrbitType(OrbitType orbitType)	Set propagation orbit type.
void	NumericalPropagator.setOrbitType(OrbitType orbitType)	Set propagation orbit type.
static <T extends CalculusFieldElement<T>> double[][]	FieldNumericalPropagator.tolerances(T dP, FieldOrbit<T> orbit, OrbitType type)	Estimate tolerance vectors for integrators.
static <T extends CalculusFieldElement<T>> double[][]	FieldNumericalPropagator.tolerances(T dP, T dV, FieldOrbit<T> orbit, OrbitType type)	Estimate tolerance vectors for integrators when propagating in orbits.
static double[][]	NumericalPropagator.tolerances(double dP, double dV, Orbit orbit, OrbitType type)	Estimate tolerance vectors for integrators when propagating in orbits.
static double[][]	NumericalPropagator.tolerances(double dP, Orbit orbit, OrbitType type)	Estimate tolerance vectors for integrators when propagating in orbits.

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

Methods in org.orekit.propagation.semianalytical.dsst that return OrbitType

Modifier and Type	Method	Description
OrbitType	DSSTHarvester.getOrbitType()	Get the orbit type used for the matrix computation.
OrbitType	DSSTPropagator.getOrbitType()	Get propagation parameter type.
OrbitType	FieldDSSTPropagator.getOrbitType()	Get propagation parameter type.

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

Modifier and Type	Method	Description
protected StateMapper	DSSTPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType ignoredOrbitType, PositionAngleType ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state.
protected FieldStateMapper<T>	FieldDSSTPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType ignoredOrbitType, PositionAngleType ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state.

Uses of OrbitType in org.orekit.utils

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

Modifier and Type	Method	Description
static StateJacobian	Differentiation.differentiate(StateFunction function, int dimension, AttitudeProvider provider, OrbitType orbitType, PositionAngleType positionAngleType, double dP, int nbPoints)	Differentiate a vector function using finite differences.