Uses of Class org.orekit.orbits.PositionAngleType (OREKIT 12.2.1 API)

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.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
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`.
`static PositionAngleType`	PositionAngleType.`valueOf(String name)`	Returns the enum constant of this type with the specified name.
`static PositionAngleType[]`	PositionAngleType.`values()`	Returns an array containing the constants of this enum type, 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.

Constructors in org.orekit.orbits with parameters of type PositionAngleType
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(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, PositionAngleType type, 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, 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.
`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, PositionAngleType cachedPositionAngleType, Frame frame, FieldAbsoluteDate<T> date, T mu)`	Creates a new instance.
`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, double aDot, double eDot, double iDot, double paDot, double raanDot, double anomalyDot, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, AbsoluteDate date, double mu)`	Creates a new instance.
`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(double a, double e, double i, double pa, double raan, double anomaly, PositionAngleType type, PositionAngleType cachedPositionAngleType, Frame frame, AbsoluteDate date, double mu)`	Creates a new instance.

Uses of PositionAngleType in org.orekit.propagation

Fields in org.orekit.propagation declared as PositionAngleType
Modifier and Type	Field	Description
`static PositionAngleType`	AbstractStateCovarianceInterpolator.`DEFAULT_POSITION_ANGLE`	Default position angle for covariance expressed in Cartesian elements.

Methods in org.orekit.propagation 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`	MatricesHarvester.`getPositionAngleType()`	Get the position angle used for the matrix computation.
`PositionAngleType`	StateCovariance.`getPositionAngleType()`	Get the covariance angle type.

Methods in org.orekit.propagation 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 with parameters of type PositionAngleType
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 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[])`.

Constructors in org.orekit.propagation.conversion with parameters of type PositionAngleType
Constructor	Description
`AbstractAnalyticalPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider, double initialMass)`	Build a new instance.
`AbstractPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction)`	Build a new instance.
`AbstractPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider)`	Build a new instance.
`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.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
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 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.
`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.`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
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 PositionAngleType in org.orekit.propagation.numerical

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.
`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.`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.
`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 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.

Uses of Classorg.orekit.orbits.PositionAngleType

Uses of PositionAngleType in org.orekit.estimation.sequential

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

Uses of PositionAngleType in org.orekit.forces.maneuvers

Uses of PositionAngleType in org.orekit.orbits

Uses of PositionAngleType in org.orekit.propagation

Uses of PositionAngleType in org.orekit.propagation.analytical

Uses of PositionAngleType in org.orekit.propagation.conversion

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

Uses of PositionAngleType in org.orekit.propagation.events

Uses of PositionAngleType in org.orekit.propagation.integration

Uses of PositionAngleType in org.orekit.propagation.numerical

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

Uses of PositionAngleType in org.orekit.utils

Uses of Class
org.orekit.orbits.PositionAngleType