Uses of 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.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 and Description
PositionAngleType	UnivariateProcessNoise.getPositionAngleType() Getter for the positionAngle.

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

Constructor and Description
UnivariateProcessNoise(org.hipparchus.linear.RealMatrix initialCovarianceMatrix, LOFType lofType, PositionAngleType positionAngleType, org.hipparchus.analysis.UnivariateFunction[] lofCartesianOrbitalParametersEvolution, org.hipparchus.analysis.UnivariateFunction[] propagationParametersEvolution) Simple constructor.
UnivariateProcessNoise(org.hipparchus.linear.RealMatrix initialCovarianceMatrix, LOFType lofType, PositionAngleType positionAngleType, org.hipparchus.analysis.UnivariateFunction[] lofCartesianOrbitalParametersEvolution, org.hipparchus.analysis.UnivariateFunction[] propagationParametersEvolution, org.hipparchus.analysis.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 and 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 and 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 and 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 and Description
PositionAngleType	FieldKeplerianOrbit.getCachedPositionAngleType() Get the cached PositionAngleType.
PositionAngleType	FieldCircularOrbit.getCachedPositionAngleType() Get the cached PositionAngleType.
PositionAngleType	EquinoctialOrbit.getCachedPositionAngleType() Get the cached PositionAngleType.
PositionAngleType	KeplerianOrbit.getCachedPositionAngleType() Get the cached PositionAngleType.
PositionAngleType	CircularOrbit.getCachedPositionAngleType() Get the cached PositionAngleType.
PositionAngleType	FieldEquinoctialOrbit.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 and Description
void	EquinoctialOrbit.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
void	KeplerianOrbit.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	CartesianOrbit.addKeplerContribution(PositionAngleType type, double gm, double[] 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
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	FieldCartesianOrbit.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
T	FieldCircularOrbit.getAlpha(PositionAngleType type) Get the latitude argument.
double	CircularOrbit.getAlpha(PositionAngleType type) Get the latitude argument.
T	FieldCircularOrbit.getAlphaDot(PositionAngleType type) Get the latitude argument derivative.
double	CircularOrbit.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	Orbit.getJacobianWrtCartesian(PositionAngleType type, double[][] jacobian) Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
void	FieldOrbit.getJacobianWrtCartesian(PositionAngleType type, T[][] jacobian) Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
void	Orbit.getJacobianWrtParameters(PositionAngleType type, double[][] jacobian) Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
void	FieldOrbit.getJacobianWrtParameters(PositionAngleType type, T[][] 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 org.hipparchus.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 org.hipparchus.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 and 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.
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.
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.
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.
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.
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.
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, 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.
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.
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.
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.

Uses of PositionAngleType in org.orekit.propagation

Fields in org.orekit.propagation declared as PositionAngleType

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

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

Constructor and Description
AbstractStateCovarianceInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType) Constructor.
FieldStateCovariance(org.hipparchus.linear.FieldMatrix<T> orbitalCovariance, FieldAbsoluteDate<T> epoch, Frame covarianceFrame, OrbitType orbitType, PositionAngleType angleType) Constructor.
StateCovariance(org.hipparchus.linear.RealMatrix orbitalCovariance, AbsoluteDate epoch, Frame covarianceFrame, OrbitType orbitType, PositionAngleType angleType) Constructor.
StateCovarianceBlender(org.hipparchus.analysis.polynomials.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, 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(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(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 and 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 and 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 and Description
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.
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, AttitudeProvider attitudeProvider, double M2) Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, 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.
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, TleGenerationAlgorithm generationAlgorithm) Build a new instance.

Uses of PositionAngleType in org.orekit.propagation.events

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

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

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

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

Uses of PositionAngleType in org.orekit.propagation.integration

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

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

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

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

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

Modifier and Type	Method and Description
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.
protected StateMapper	GLONASSNumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)
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.
void	NumericalPropagator.setPositionAngleType(PositionAngleType positionAngleType) Set position angle type.
void	FieldNumericalPropagator.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 and Description
PositionAngleType	FieldDSSTPropagator.getPositionAngleType() Get propagation parameter type.
PositionAngleType	DSSTPropagator.getPositionAngleType() Get propagation parameter type.
PositionAngleType	DSSTHarvester.getPositionAngleType() Get the position angle used for the matrix computation.

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

Modifier and Type	Method and 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 and 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.