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.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 and Description
OrbitType	FieldKeplerianOrbit.getType() Get the orbit type.
OrbitType	FieldCircularOrbit.getType() Get the orbit type.
OrbitType	EquinoctialOrbit.getType() Get the orbit type.
abstract OrbitType	Orbit.getType() Get the orbit type.
OrbitType	KeplerianOrbit.getType() Get the orbit type.
OrbitType	CircularOrbit.getType() Get the orbit type.
OrbitType	FieldEquinoctialOrbit.getType() Get the orbit type.
OrbitType	CartesianOrbit.getType() Get the orbit type.
OrbitType	FieldCartesianOrbit.getType() Get the orbit type.
abstract OrbitType	FieldOrbit.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 and Description
OrbitType	StateCovarianceMatrixProvider.getCovarianceOrbitType() Get the orbit type in which the covariance matrix is expressed.
OrbitType	StateCovariance.getOrbitType() Get the covariance orbit type.

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

Modifier and Type	Method and Description
StateCovariance	StateCovariance.changeCovarianceType(Orbit orbit, OrbitType outOrbitType, PositionAngle outAngleType) Get the covariance matrix in another orbit type.
StateCovariance	StateCovarianceMatrixProvider.getStateCovariance(SpacecraftState state, OrbitType orbitType, PositionAngle angleType) Get the state covariance expressed in a given orbit type.

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

Constructor and Description
StateCovariance(RealMatrix orbitalCovariance, AbsoluteDate epoch, Frame covarianceFrame, OrbitType orbitType, PositionAngle angleType) Constructor.
StateCovarianceMatrixProvider(String additionalName, String stmName, MatricesHarvester harvester, OrbitType stmOrbitType, PositionAngle stmAngleType, StateCovariance covInit) Constructor.

Uses of OrbitType in org.orekit.propagation.conversion

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

Modifier and Type	Method and 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 and Description
abstract AbstractFieldIntegrator<T>	AbstractFieldIntegratorBuilder.buildIntegrator(Field<T> field, 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.
AbstractFieldIntegrator<T>	MidpointFieldIntegratorBuilder.buildIntegrator(Field<T> field, 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.
AbstractFieldIntegrator<T>	GillFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit 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>	DormandPrince54FieldIntegratorBuilder.buildIntegrator(Field<T> field, 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>	HighamHall54FieldIntegratorBuilder.buildIntegrator(Field<T> field, 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.
AbstractFieldIntegrator<T>	AdamsBashforthFieldIntegratorBuilder.buildIntegrator(Field<T> field, 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.
AbstractFieldIntegrator<T>	LutherFieldIntegratorBuilder.buildIntegrator(Field<T> field, 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.
AbstractFieldIntegrator<T>	AbstractFieldIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType) Build a first order integrator.
AbstractFieldIntegrator<T>	FieldODEIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	HighamHall54IntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	DormandPrince853IntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	DormandPrince54IntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	EulerIntegratorBuilder.buildIntegrator(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.
AbstractIntegrator	ClassicalRungeKuttaIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	AdamsBashforthIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	AdamsMoultonIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	LutherIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	GraggBulirschStoerIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType) Build a first order integrator.
AbstractIntegrator	GillIntegratorBuilder.buildIntegrator(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 and Description
BrouwerLyddanePropagatorBuilder(Orbit templateOrbit, double referenceRadius, double mu, TideSystem tideSystem, double c20, double c30, double c40, double c50, OrbitType orbitType, PositionAngle positionAngle, 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, PositionAngle positionAngle, 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 and Description
OrbitType	PositionAngleDetector.getOrbitType() Get the orbit type defining the angle type.

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

Constructor and Description
PositionAngleDetector(double maxCheck, double threshold, OrbitType orbitType, PositionAngle positionAngle, double angle) Build a detector.
PositionAngleDetector(OrbitType orbitType, PositionAngle positionAngle, double angle) Build a new detector.

Uses of OrbitType in org.orekit.propagation.integration

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

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

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

Modifier and Type	Method and Description
protected abstract StateMapper	AbstractIntegratedPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle 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, PositionAngle 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 and Description
FieldStateMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Simple constructor.
StateMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle 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 and Description
OrbitType	NumericalPropagator.getOrbitType() Get propagation parameter type.
OrbitType	FieldNumericalPropagator.getOrbitType() Get propagation parameter type.

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

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

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

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

Modifier and Type	Method and Description
OrbitType	FieldDSSTPropagator.getOrbitType() Get propagation parameter type.
OrbitType	DSSTPropagator.getOrbitType() Get propagation parameter type.

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

Modifier and Type	Method and Description
protected StateMapper	DSSTPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType ignoredOrbitType, PositionAngle 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, PositionAngle 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 and Description
static StateJacobian	Differentiation.differentiate(StateFunction function, int dimension, AttitudeProvider provider, OrbitType orbitType, PositionAngle positionAngle, double dP, int nbPoints) Differentiate a vector function using finite differences.