Uses of Class
org.orekit.orbits.PositionAngle

Packages that use PositionAngle

Package	Description
org.orekit.files.ccsds	This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.orbits	This package provides classes to represent orbits.
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).

Uses of PositionAngle in org.orekit.files.ccsds

Methods in org.orekit.files.ccsds that return PositionAngle

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

Uses of PositionAngle in org.orekit.forces.maneuvers

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

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

Uses of PositionAngle in org.orekit.orbits

Methods in org.orekit.orbits that return PositionAngle

Modifier and Type	Method and Description
static PositionAngle	PositionAngle.valueOf(String name) Returns the enum constant of this type with the specified name.
static PositionAngle[]	PositionAngle.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 PositionAngle

Modifier and Type	Method and Description
void	CircularOrbit.addKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
void	CartesianOrbit.addKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
void	EquinoctialOrbit.addKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
abstract void	Orbit.addKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
void	KeplerianOrbit.addKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
double	CircularOrbit.getAlpha(PositionAngle type) Get the latitude argument.
double	KeplerianOrbit.getAnomaly(PositionAngle type) Get the anomaly.
void	CartesianOrbit.getJacobianWrtCartesian(PositionAngle type, double[][] jacobian)
void	Orbit.getJacobianWrtCartesian(PositionAngle type, double[][] jacobian) Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
void	Orbit.getJacobianWrtParameters(PositionAngle type, double[][] jacobian) Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
double	EquinoctialOrbit.getL(PositionAngle type) Get the longitude argument.
abstract Orbit	OrbitType.mapArrayToOrbit(double[] array, PositionAngle type, AbsoluteDate date, double mu, Frame frame) Convert state array to orbital parameters.
abstract void	OrbitType.mapOrbitToArray(Orbit orbit, PositionAngle type, double[] stateVector) Convert orbit to state array.

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

Constructor and Description
CircularOrbit(double a, double ex, double ey, double i, double raan, double alpha, PositionAngle type, Frame frame, AbsoluteDate date, double mu) Creates a new instance.
CircularOrbit(double a, double ex, double ey, double i, double raan, double alpha, PositionAngle type, TimeStampedPVCoordinates pvCoordinates, Frame frame, double mu) Creates a new instance.
EquinoctialOrbit(double a, double ex, double ey, double hx, double hy, double l, PositionAngle type, Frame frame, AbsoluteDate date, double mu) Creates a new instance.
KeplerianOrbit(double a, double e, double i, double pa, double raan, double anomaly, PositionAngle type, Frame frame, AbsoluteDate date, double mu) Creates a new instance.

Uses of PositionAngle in org.orekit.propagation.conversion

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

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

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

Constructor and Description
AbstractPropagatorBuilder(Frame frame, double mu, OrbitType orbitType, PositionAngle positionAngle) Build a new instance.
EcksteinHechlerPropagatorBuilder(Frame frame, double referenceRadius, double mu, TideSystem tideSystem, double c20, double c30, double c40, double c50, double c60, OrbitType orbitType, PositionAngle positionAngle) Build a new instance.
EcksteinHechlerPropagatorBuilder(Frame frame, UnnormalizedSphericalHarmonicsProvider provider, OrbitType orbitType, PositionAngle positionAngle) Build a new instance.
KeplerianPropagatorBuilder(double mu, Frame frame, OrbitType orbitType, PositionAngle positionAngle) Build a new instance.
NumericalPropagatorBuilder(double mu, Frame frame, FirstOrderIntegratorBuilder builder, OrbitType orbitType, PositionAngle positionAngle) Build a new instance.
TLEPropagatorBuilder(int satelliteNumber, char classification, int launchYear, int launchNumber, String launchPiece, int elementNumber, int revolutionNumberAtEpoch, OrbitType orbitType, PositionAngle positionAngle) Build a new instance.

Uses of PositionAngle in org.orekit.propagation.events

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

Modifier and Type	Method and Description
PositionAngle	PositionAngleDetector.getPositionAngle() Get the type of position angle.

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

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

Uses of PositionAngle in org.orekit.propagation.integration

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

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

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

Modifier and Type	Method and Description
protected abstract StateMapper	AbstractIntegratedPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
protected void	AbstractIntegratedPropagator.setPositionAngleType(PositionAngle positionAngleType) Set position angle type.

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

Constructor and Description
StateMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Simple constructor.

Uses of PositionAngle in org.orekit.propagation.numerical

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

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

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

Modifier and Type	Method and Description
protected StateMapper	NumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
void	NumericalPropagator.setPositionAngleType(PositionAngle positionAngleType) Set position angle type.

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

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

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