Uses of Enum Class
org.orekit.orbits.PositionAngleType

Packages that use PositionAngleType

Package	Description
org.orekit.estimation.sequential	The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.
org.orekit.files.ccsds.ndm.odm	This package contains class managing CCSDS Orbit Data Message.
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
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.conversion.averaging	This package wraps methods from various (semi)analytical models in Orekit to convert back and forth between an averaged orbital state and an osculating one.
org.orekit.propagation.covariance	This package provides tools to represent and propagate covariance.
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 PositionAngleType in org.orekit.estimation.sequential

Methods in org.orekit.estimation.sequential that return PositionAngleType

Modifier and Type	Method	Description
PositionAngleType	UnivariateProcessNoise.getPositionAngleType()	Getter for the positionAngle.

Constructors in org.orekit.estimation.sequential with parameters of type PositionAngleType

Modifier	Constructor	Description
	UnivariateProcessNoise(RealMatrix initialCovarianceMatrix, LOFType lofType, PositionAngleType positionAngleType, UnivariateFunction[] lofCartesianOrbitalParametersEvolution, UnivariateFunction[] propagationParametersEvolution)	Simple constructor.
	UnivariateProcessNoise(RealMatrix initialCovarianceMatrix, LOFType lofType, PositionAngleType positionAngleType, UnivariateFunction[] lofCartesianOrbitalParametersEvolution, UnivariateFunction[] propagationParametersEvolution, UnivariateFunction[] measurementsParametersEvolution)	Simple constructor.

Uses of PositionAngleType in org.orekit.files.ccsds.ndm.odm

Methods in org.orekit.files.ccsds.ndm.odm that return PositionAngleType

Modifier and Type	Method	Description
PositionAngleType	KeplerianElements.getAnomalyType()	Get the type of anomaly (true or mean).

Methods in org.orekit.files.ccsds.ndm.odm with parameters of type PositionAngleType

Modifier and Type	Method	Description
void	KeplerianElements.setAnomalyType(PositionAngleType anomalyType)	Set the type of anomaly.

Uses of PositionAngleType in org.orekit.forces.maneuvers

Methods in org.orekit.forces.maneuvers with parameters of type PositionAngleType

Modifier and Type	Method	Description
void	SmallManeuverAnalyticalModel.getJacobian(Orbit orbit1, PositionAngleType positionAngleType, double[][] jacobian)	Compute the Jacobian of the orbit with respect to maneuver parameters.

Uses of PositionAngleType in org.orekit.orbits

Methods in org.orekit.orbits that return PositionAngleType

Modifier and Type	Method	Description
PositionAngleType	CircularOrbit.getCachedPositionAngleType()	Get the cached PositionAngleType.
PositionAngleType	EquinoctialOrbit.getCachedPositionAngleType()	Get the cached PositionAngleType.
PositionAngleType	FieldCircularOrbit.getCachedPositionAngleType()	Get the cached PositionAngleType.
PositionAngleType	FieldEquinoctialOrbit.getCachedPositionAngleType()	Get the cached PositionAngleType.
PositionAngleType	FieldKeplerianOrbit.getCachedPositionAngleType()	Get the cached PositionAngleType.
PositionAngleType	KeplerianOrbit.getCachedPositionAngleType()	Get the cached PositionAngleType.
PositionAngleType	PositionAngleBased.getCachedPositionAngleType()	Get the cached PositionAngleType.
PositionAngleType	FieldKeplerianParameters.positionAngleType()	Returns the value of the positionAngleType record component.
PositionAngleType	KeplerianParameters.positionAngleType()	Returns the value of the positionAngleType record component.
static PositionAngleType	PositionAngleType.valueOf(String name)	Returns the enum constant of this class with the specified name.
static PositionAngleType[]	PositionAngleType.values()	Returns an array containing the constants of this enum class, in the order they are declared.

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

Modifier and Type	Method	Description
void	CartesianOrbit.addKeplerContribution(PositionAngleType type, double gm, double[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
void	CircularOrbit.addKeplerContribution(PositionAngleType type, double gm, double[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
void	EquinoctialOrbit.addKeplerContribution(PositionAngleType type, double gm, double[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
void	FieldCartesianOrbit.addKeplerContribution(PositionAngleType type, T gm, T[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
void	FieldCircularOrbit.addKeplerContribution(PositionAngleType type, T gm, T[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
void	FieldEquinoctialOrbit.addKeplerContribution(PositionAngleType type, T gm, T[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
void	FieldKeplerianOrbit.addKeplerContribution(PositionAngleType type, T gm, T[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
abstract void	FieldOrbit.addKeplerContribution(PositionAngleType type, T gm, T[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
void	KeplerianOrbit.addKeplerContribution(PositionAngleType type, double gm, double[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
abstract void	Orbit.addKeplerContribution(PositionAngleType type, double gm, double[] pDot)	Add the contribution of the Keplerian motion to parameters derivatives
static double	CircularLatitudeArgumentUtility.convertAlpha(PositionAngleType oldType, double alpha, double ex, double ey, PositionAngleType newType)	Convert argument of latitude.
static <T extends CalculusFieldElement<T>> T	FieldCircularLatitudeArgumentUtility.convertAlpha(PositionAngleType oldType, T alpha, T ex, T ey, PositionAngleType newType)	Convert argument of latitude.
static <T extends CalculusFieldElement<T>> T	FieldKeplerianAnomalyUtility.convertAnomaly(PositionAngleType oldType, T anomaly, T e, PositionAngleType newType)	Convert anomaly.
static double	KeplerianAnomalyUtility.convertAnomaly(PositionAngleType oldType, double anomaly, double e, PositionAngleType newType)	Convert anomaly.
static double	EquinoctialLongitudeArgumentUtility.convertL(PositionAngleType oldType, double l, double ex, double ey, PositionAngleType newType)	Convert argument of longitude.
static <T extends CalculusFieldElement<T>> T	FieldEquinoctialLongitudeArgumentUtility.convertL(PositionAngleType oldType, T l, T ex, T ey, PositionAngleType newType)	Convert argument of longitude.
double	CircularOrbit.getAlpha(PositionAngleType type)	Get the latitude argument.
T	FieldCircularOrbit.getAlpha(PositionAngleType type)	Get the latitude argument.
double	CircularOrbit.getAlphaDot(PositionAngleType type)	Get the latitude argument derivative.
T	FieldCircularOrbit.getAlphaDot(PositionAngleType type)	Get the latitude argument derivative.
T	FieldKeplerianOrbit.getAnomaly(PositionAngleType type)	Get the anomaly.
double	KeplerianOrbit.getAnomaly(PositionAngleType type)	Get the anomaly.
T	FieldKeplerianOrbit.getAnomalyDot(PositionAngleType type)	Get the anomaly derivative.
double	KeplerianOrbit.getAnomalyDot(PositionAngleType type)	Get the anomaly derivative.
abstract ParameterDriversList	OrbitType.getDrivers(double dP, Orbit orbit, PositionAngleType type)	Get parameters drivers initialized from a reference orbit.
void	FieldOrbit.getJacobianWrtCartesian(PositionAngleType type, T[][] jacobian)	Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
void	Orbit.getJacobianWrtCartesian(PositionAngleType type, double[][] jacobian)	Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
void	FieldOrbit.getJacobianWrtParameters(PositionAngleType type, T[][] jacobian)	Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
void	Orbit.getJacobianWrtParameters(PositionAngleType type, double[][] jacobian)	Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
double	EquinoctialOrbit.getL(PositionAngleType type)	Get the longitude argument.
T	FieldEquinoctialOrbit.getL(PositionAngleType type)	Get the longitude argument.
double	EquinoctialOrbit.getLDot(PositionAngleType type)	Get the longitude argument derivative.
T	FieldEquinoctialOrbit.getLDot(PositionAngleType type)	Get the longitude argument derivative.
abstract Orbit	OrbitType.mapArrayToOrbit(double[] array, double[] arrayDot, PositionAngleType type, AbsoluteDate date, double mu, Frame frame)	Convert state array to orbital parameters.
abstract <T extends CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.mapArrayToOrbit(T[] array, T[] arrayDot, PositionAngleType type, FieldAbsoluteDate<T> date, T mu, Frame frame)	Convert state array to orbital parameters.
abstract <T extends CalculusFieldElement<T>> void	OrbitType.mapOrbitToArray(FieldOrbit<T> orbit, PositionAngleType type, T[] stateVector, T[] stateVectorDot)	Convert orbit to state array.
abstract void	OrbitType.mapOrbitToArray(Orbit orbit, PositionAngleType type, double[] stateVector, double[] stateVectorDot)	Convert orbit to state array.
FieldKeplerianParameters<T>	FieldKeplerianParametersConverter.toParameters(FieldPVCoordinates<T> cartesian, PositionAngleType positionAngleType)	Convert Cartesian coordinates to Keplerian elements.
KeplerianParameters	KeplerianParametersConverter.toParameters(PVCoordinates cartesian, PositionAngleType positionAngleType)	Convert Cartesian coordinates to Keplerian elements.
CircularOrbit	CircularOrbit.withCachedPositionAngleType(PositionAngleType positionAngleType)	Creates a new instance with the provided type used for caching.
EquinoctialOrbit	EquinoctialOrbit.withCachedPositionAngleType(PositionAngleType positionAngleType)	Creates a new instance with the provided type used for caching.
FieldCircularOrbit<T>	FieldCircularOrbit.withCachedPositionAngleType(PositionAngleType positionAngleType)	Creates a new instance with the provided type used for caching.
FieldEquinoctialOrbit<T>	FieldEquinoctialOrbit.withCachedPositionAngleType(PositionAngleType positionAngleType)	Creates a new instance with the provided type used for caching.
FieldKeplerianOrbit<T>	FieldKeplerianOrbit.withCachedPositionAngleType(PositionAngleType positionAngleType)	Creates a new instance with the provided type used for caching.
KeplerianOrbit	KeplerianOrbit.withCachedPositionAngleType(PositionAngleType positionAngleType)	Creates a new instance with the provided type used for caching.
T	PositionAngleBased.withCachedPositionAngleType(PositionAngleType positionAngleType)	Creates a new instance with the provided type used for caching.
FieldKeplerianParameters<T>	FieldKeplerianParameters.withPositionAngleType(PositionAngleType angleType)	Builds a new instance with the specified position angle type.
KeplerianParameters	KeplerianParameters.withPositionAngleType(PositionAngleType angleType)	Builds a new instance with the specified position angle type.

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

Modifier	Constructor	Description
	CircularOrbit(double a, double ex, double ey, double i, double raan, double alpha, double aDot, double exDot, double eyDot, double iDot, double raanDot, double alphaDot, PositionAngleType type, Frame frame, AbsoluteDate date, double mu)	Creates a new instance with derivatives and with cached position angle same as value inputted.
	CircularOrbit(double a, double ex, double ey, double i, double raan, double alpha, double aDot, double exDot, double eyDot, double iDot, double raanDot, double alphaDot, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, AbsoluteDate date, double mu)	Creates a new instance.
	CircularOrbit(double a, double ex, double ey, double i, double raan, double alpha, PositionAngleType type, Frame frame, AbsoluteDate date, double mu)	Creates a new instance without derivatives and with cached position angle same as value inputted.
	CircularOrbit(double a, double ex, double ey, double i, double raan, double alpha, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, AbsoluteDate date, double mu)	Creates a new instance.
	EquinoctialOrbit(double a, double ex, double ey, double hx, double hy, double l, double aDot, double exDot, double eyDot, double hxDot, double hyDot, double lDot, PositionAngleType type, Frame frame, AbsoluteDate date, double mu)	Creates a new instance with derivatives and with cached position angle same as value inputted.
	EquinoctialOrbit(double a, double ex, double ey, double hx, double hy, double l, double aDot, double exDot, double eyDot, double hxDot, double hyDot, double lDot, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, AbsoluteDate date, double mu)	Creates a new instance.
	EquinoctialOrbit(double a, double ex, double ey, double hx, double hy, double l, PositionAngleType type, Frame frame, AbsoluteDate date, double mu)	Creates a new instance without derivatives and with cached position angle same as value inputted.
	EquinoctialOrbit(double a, double ex, double ey, double hx, double hy, double l, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, AbsoluteDate date, double mu)	Creates a new instance.
	FieldCircularOrbit(T a, T ex, T ey, T i, T raan, T alpha, PositionAngleType type, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance without derivatives and with cached position angle same as value inputted.
	FieldCircularOrbit(T a, T ex, T ey, T i, T raan, T alpha, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldCircularOrbit(T a, T ex, T ey, T i, T raan, T alpha, T aDot, T exDot, T eyDot, T iDot, T raanDot, T alphaDot, PositionAngleType type, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldCircularOrbit(T a, T ex, T ey, T i, T raan, T alpha, T aDot, T exDot, T eyDot, T iDot, T raanDot, T alphaDot, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldEquinoctialOrbit(T a, T ex, T ey, T hx, T hy, T l, PositionAngleType type, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldEquinoctialOrbit(T a, T ex, T ey, T hx, T hy, T l, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldEquinoctialOrbit(T a, T ex, T ey, T hx, T hy, T l, T aDot, T exDot, T eyDot, T hxDot, T hyDot, T lDot, PositionAngleType type, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldEquinoctialOrbit(T a, T ex, T ey, T hx, T hy, T l, T aDot, T exDot, T eyDot, T hxDot, T hyDot, T lDot, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldKeplerianOrbit(FieldKeplerianParameters<T> elements, T aDot, T eDot, T iDot, T paDot, T raanDot, T anomalyDot, PositionAngleType cachedPositionAngleType, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldKeplerianOrbit(T a, T e, T i, T pa, T raan, T anomaly, PositionAngleType type, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldKeplerianOrbit(T a, T e, T i, T pa, T raan, T anomaly, T aDot, T eDot, T iDot, T paDot, T raanDot, T anomalyDot, PositionAngleType type, Frame frame, FieldAbsoluteDate<T> date, T mu)	Creates a new instance.
	FieldKeplerianParameters(T a, T e, T i, T pa, T raan, T anomaly, PositionAngleType positionAngleType)	Creates an instance of a FieldKeplerianParameters record class.
	KeplerianOrbit(double a, double e, double i, double pa, double raan, double anomaly, double aDot, double eDot, double iDot, double paDot, double raanDot, double anomalyDot, PositionAngleType type, Frame frame, AbsoluteDate date, double mu)	Creates a new instance with cached position angle same as value inputted.
	KeplerianOrbit(double a, double e, double i, double pa, double raan, double anomaly, PositionAngleType type, Frame frame, AbsoluteDate date, double mu)	Creates a new instance without derivatives and with cached position angle same as value inputted.
	KeplerianOrbit(KeplerianParameters keplerianParameters, double aDot, double eDot, double iDot, double paDot, double raanDot, double anomalyDot, PositionAngleType cachedPositionAngleType, Frame frame, AbsoluteDate date, double mu)	Creates a new instance.
	KeplerianParameters(double a, double e, double i, double pa, double raan, double anomaly, PositionAngleType positionAngleType)	Creates an instance of a KeplerianParameters record class.

Uses of PositionAngleType in org.orekit.propagation

Methods in org.orekit.propagation that return PositionAngleType

Modifier and Type	Method	Description
PositionAngleType	MatricesHarvester.getPositionAngleType()	Get the position angle used for the matrix computation.

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

Modifier and Type	Method	Description
double[][]	SimpleToleranceProvider.getTolerances(Orbit referenceOrbit, OrbitType propagationOrbitType, PositionAngleType positionAngleType)
default <T extends CalculusFieldElement<T>> double[][]	ToleranceProvider.getTolerances(FieldOrbit<T> referenceOrbit, OrbitType propagationOrbitType, PositionAngleType positionAngleType)	Retrieve the integration tolerances given a reference Field orbit.
double[][]	ToleranceProvider.getTolerances(Orbit referenceOrbit, OrbitType propagationOrbitType, PositionAngleType positionAngleType)	Retrieve the integration tolerances given a reference orbit.

Uses of PositionAngleType in org.orekit.propagation.analytical

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

Modifier and Type	Method	Description
PositionAngleType	AbstractAnalyticalMatricesHarvester.getPositionAngleType()	Get the position angle used for the matrix computation.

Uses of PositionAngleType in org.orekit.propagation.conversion

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

Modifier and Type	Method	Description
PositionAngleType	AbstractPropagatorBuilder.getPositionAngleType()	Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
PositionAngleType	PropagatorBuilder.getPositionAngleType()	Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

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

Modifier and Type	Method	Description
abstract T	AbstractIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)
W	AbstractVariableStepFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
T	AbstractVariableStepIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ClassicalRungeKuttaFieldIntegrator<T>	ClassicalRungeKuttaFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ClassicalRungeKuttaIntegrator	ClassicalRungeKuttaIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
EulerFieldIntegrator<T>	EulerFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
EulerIntegrator	EulerIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ExplicitRungeKuttaIntegrator	ExplicitRungeKuttaIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
abstract W	FieldAbstractIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
FieldExplicitRungeKuttaIntegrator<T>	FieldExplicitRungeKuttaIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
FieldODEIntegrator<T>	FieldODEIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
GillFieldIntegrator<T>	GillFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
GillIntegrator	GillIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
LutherFieldIntegrator<T>	LutherFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType positionAngleType)	Build a first order integrator.
LutherIntegrator	LutherIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
MidpointFieldIntegrator<T>	MidpointFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
MidpointIntegrator	MidpointIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ODEIntegrator	ODEIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ThreeEighthesFieldIntegrator<T>	ThreeEighthesFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ThreeEighthesIntegrator	ThreeEighthesIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
protected double[][]	AbstractVariableStepFieldIntegratorBuilder.getTolerances(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Computes tolerances.

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

Modifier	Constructor	Description
protected	AbstractAnalyticalPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider, double initialMass)	Build a new instance.
protected	AbstractIntegratedPropagatorBuilder(Orbit templateOrbit, ODEIntegratorBuilder builder, PositionAngleType positionAngleType, double positionScale, PropagationType propagationType, AttitudeProvider attitudeProvider, double mass)	Build a new instance.
protected	AbstractPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction)	Build a new instance.
protected	AbstractPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider)	Build a new instance.
protected	AbstractPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider, double initialMass)	Build a new instance.
	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.
	BrouwerLyddanePropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, PositionAngleType positionAngleType, double positionScale, double M2)	Build a new instance.
	BrouwerLyddanePropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider, 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.
	EcksteinHechlerPropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, PositionAngleType positionAngleType, double positionScale)	Build a new instance.
	EcksteinHechlerPropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider)	Build a new instance.
	KeplerianPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale)	Build a new instance.
	KeplerianPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider)	Build a new instance.
	NumericalPropagatorBuilder(Orbit referenceOrbit, ODEIntegratorBuilder builder, PositionAngleType positionAngleType, double positionScale)	Build a new instance.
	NumericalPropagatorBuilder(Orbit referenceOrbit, ODEIntegratorBuilder builder, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider)	Build a new instance.
	TLEPropagatorBuilder(TLE templateTLE, PositionAngleType positionAngleType, double positionScale, DataContext dataContext, TleGenerationAlgorithm generationAlgorithm)	Build a new instance.
	TLEPropagatorBuilder(TLE templateTLE, PositionAngleType positionAngleType, double positionScale, DataContext dataContext, TleGenerationAlgorithm generationAlgorithm, AttitudeProvider attitudeProvider)	Build a new instance.
	TLEPropagatorBuilder(TLE templateTLE, PositionAngleType positionAngleType, double positionScale, TleGenerationAlgorithm generationAlgorithm)	Build a new instance.

Uses of PositionAngleType in org.orekit.propagation.conversion.averaging

Methods in org.orekit.propagation.conversion.averaging that return PositionAngleType

Modifier and Type	Method	Description
PositionAngleType	AveragedOrbitalState.getPositionAngleType()	Getter for the averaged position angle.
PositionAngleType	BrouwerLyddaneOrbitalState.getPositionAngleType()	Getter for the averaged position angle.
PositionAngleType	DSST6X0OrbitalState.getPositionAngleType()	Getter for the averaged position angle.
PositionAngleType	EcksteinHechlerOrbitalState.getPositionAngleType()	Getter for the averaged position angle.
PositionAngleType	SGP4OrbitalState.getPositionAngleType()	Getter for the averaged position angle.

Uses of PositionAngleType in org.orekit.propagation.covariance

Fields in org.orekit.propagation.covariance declared as PositionAngleType

Modifier and Type	Field	Description
static final PositionAngleType	AbstractStateCovarianceInterpolator.DEFAULT_POSITION_ANGLE	Default position angle for covariance expressed in Cartesian elements.

Methods in org.orekit.propagation.covariance that return PositionAngleType

Modifier and Type	Method	Description
PositionAngleType	AbstractStateCovarianceInterpolator.getOutPositionAngleType()	Get output position angle type.
PositionAngleType	FieldStateCovariance.getPositionAngleType()	Get the covariance angle type.
PositionAngleType	StateCovariance.getPositionAngleType()	Get the covariance angle type.

Methods in org.orekit.propagation.covariance with parameters of type PositionAngleType

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.
StateCovariance	StateCovarianceMatrixProvider.getStateCovariance(SpacecraftState state, OrbitType orbitType, PositionAngleType angleType)	Get the state covariance expressed in a given orbit type.
static boolean	StateCovariance.inputAndOutputAreIdentical(OrbitType inOrbitType, PositionAngleType inAngleType, OrbitType outOrbitType, PositionAngleType outAngleType)	Checks if input/output orbit and angle types are identical.

Constructors in org.orekit.propagation.covariance with parameters of type PositionAngleType

Modifier	Constructor	Description
protected	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 PositionAngleType in org.orekit.propagation.events

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

Modifier and Type	Method	Description
PositionAngleType	PositionAngleDetector.getPositionAngleType()	Get the type of position angle.

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

Modifier	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.
protected	PositionAngleDetector(EventDetectionSettings detectionSettings, EventHandler handler, OrbitType orbitType, PositionAngleType positionAngleType, double angle)	Protected constructor with full parameters.

Uses of PositionAngleType in org.orekit.propagation.integration

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

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

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

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. /** Simple constructor.
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. /** Simple constructor.
protected void	AbstractIntegratedPropagator.setPositionAngleType(PositionAngleType positionAngleType)	Set position angle type.
protected void	FieldAbstractIntegratedPropagator.setPositionAngleType(PositionAngleType positionAngleType)	Set position angle type.

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

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

Uses of PositionAngleType in org.orekit.propagation.numerical

Fields in org.orekit.propagation.numerical declared as PositionAngleType

Modifier and Type	Field	Description
static final PositionAngleType	NumericalPropagator.DEFAULT_POSITION_ANGLE_TYPE	Default position angle type.

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

Modifier and Type	Method	Description
PositionAngleType	FieldNumericalPropagator.getPositionAngleType()	Get propagation parameter type.
PositionAngleType	NumericalPropagator.getPositionAngleType()	Get propagation parameter type.

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

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. /** Simple constructor.
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. /** Simple constructor.
void	FieldNumericalPropagator.setPositionAngleType(PositionAngleType positionAngleType)	Set position angle type.
void	NumericalPropagator.setPositionAngleType(PositionAngleType positionAngleType)	Set position angle type.

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

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

Modifier and Type	Method	Description
PositionAngleType	DSSTHarvester.getPositionAngleType()	Get the position angle used for the matrix computation.
PositionAngleType	DSSTPropagator.getPositionAngleType()	Get propagation parameter type.
PositionAngleType	FieldDSSTPropagator.getPositionAngleType()	Get propagation parameter type.

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

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. /** Simple constructor.
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. /** Simple constructor.

Uses of PositionAngleType in org.orekit.utils

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

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.