Uses of Class
org.orekit.orbits.PositionAngle

Packages that use PositionAngle

fr.cnes.sirius.patrius.propagation.events.multi
fr.cnes.sirius.patrius.propagation.numerical.multi
fr.cnes.sirius.patrius.propagation.precomputed.multi
fr.cnes.sirius.patrius.propagation.sampling.multi
fr.cnes.sirius.patrius.stela.orbits
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.orbits.orbitalparameters
org.orekit.propagation	This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.numerical
org.orekit.propagation.precomputed
org.orekit.propagation.sampling	This package provides interfaces and classes dealing with step handling during propagation.

Uses of PositionAngle in fr.cnes.sirius.patrius.propagation.events.multi

Constructors in fr.cnes.sirius.patrius.propagation.events.multi with parameters of type PositionAngle

AdaptedMonoEventDetector(EventDetector detector, OrbitType orbitType, PositionAngle angleType, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, AbsoluteDate referenceDate, double mu, Frame integrationFrame, MultiStateVectorInfo stateVectorInfo, String satId)
Build a wrapped event detector.

AdaptedMultiEventDetector(MultiEventDetector detector, OrbitType orbitType, PositionAngle angleType, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, AbsoluteDate referenceDate, Map<String,Double> muMap, Map<String,Frame> framesMap, MultiStateVectorInfo stateVectorInfo)
Build a wrapped multi-sat event detector.

Uses of PositionAngle in fr.cnes.sirius.patrius.propagation.numerical.multi

Methods in fr.cnes.sirius.patrius.propagation.numerical.multi that return PositionAngle

PositionAngle

MultiNumericalPropagator.getPositionAngleType() Get propagation parameter type.

Methods in fr.cnes.sirius.patrius.propagation.numerical.multi with parameters of type PositionAngle

void	MultiEphemerisModeHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attitudeProvidersForces, Map<String,AttitudeProvider> attitudeProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frame, Map<String,Double> mu) Initialize the mode handler.
void	MultiModeHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attitudeProvidersForces, Map<String,AttitudeProvider> attitudeProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frame, Map<String,Double> mu) Initialize the mode handler.
SpacecraftState	MultiStateVectorInfo.mapArrayToState(double[] y, AbsoluteDate currentDate, OrbitType orbitType, PositionAngle angleType, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, double mu, Frame integrationFrame, String satId) Extract a given SpacecraftState from the state vector.
Map<String,SpacecraftState>	MultiStateVectorInfo.mapArrayToStates(double[] y, AbsoluteDate currentDate, OrbitType orbitType, PositionAngle angleType, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, Map<String,Double> mu, Map<String,Frame> integrationFrame) Convert state vector into a Map of SpacecraftState
void	MultiStateVectorInfo.mapStatesToArray(Map<String,SpacecraftState> s, OrbitType orbitType, PositionAngle angleType, double[] y) Convert a map of SpacecraftState into a state vector.
void	MultiNumericalPropagator.setPositionAngleType(PositionAngle positionAngleType) Set position angle type.

Uses of PositionAngle in fr.cnes.sirius.patrius.propagation.precomputed.multi

Constructors in fr.cnes.sirius.patrius.propagation.precomputed.multi with parameters of type PositionAngle

MultiIntegratedEphemeris(List<AbsoluteDate> startDatesIn, List<AbsoluteDate> minDatesIn, List<AbsoluteDate> maxDatesIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, MultiStateVectorInfo stateInfos, List<ContinuousOutputModel> modelsIn, Frame referenceFrameIn, double muIn, String satIdIn)
Creates a new instance of IntegratedEphemeris.

Uses of PositionAngle in fr.cnes.sirius.patrius.propagation.sampling.multi

Methods in fr.cnes.sirius.patrius.propagation.sampling.multi with parameters of type PositionAngle

void

MultiAdaptedStepHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frameMap, Map<String,Double> muMap) Initialize the mode handler.

Uses of PositionAngle in fr.cnes.sirius.patrius.stela.orbits

Methods in fr.cnes.sirius.patrius.stela.orbits with parameters of type PositionAngle

protected void

StelaEquinoctialOrbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot)

Uses of PositionAngle in org.orekit.forces.maneuvers

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

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

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

void	Orbit.addKeplerContribution(PositionAngle type, double gm, double[] pDot) Call the method Orbit.orbitAddKeplerContribution(PositionAngle, double, double[]) implemented in inherited classes of Orbit.
protected double[][]	Orbit.createInverseJacobian(PositionAngle type) Create an inverse Jacobian.
double	CircularOrbit.getAlpha(PositionAngle type) Get the latitude argument.
double	KeplerianOrbit.getAnomaly(PositionAngle type) Get the anomaly.
double	EquatorialOrbit.getAnomaly(PositionAngle type) Get the anomaly.
double	ApsisOrbit.getAnomaly(PositionAngle type) Get the anomaly.
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.
void	EquinoctialOrbit.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.
protected void	CircularOrbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
protected void	KeplerianOrbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
protected abstract void	Orbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
protected void	EquatorialOrbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
protected void	EquinoctialOrbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
protected void	ApsisOrbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives
protected void	CartesianOrbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives

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

ApsisOrbit(double peri, double apo, double i, double pa, double raan, double anomaly, 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, Frame frame, AbsoluteDate date, double mu)
Creates a new instance.

EquatorialOrbit(double a, double e, double pomega, double ix, double iy, double anomaly, PositionAngle type, Frame frame, AbsoluteDate date, 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.orbits.orbitalparameters

Methods in org.orekit.orbits.orbitalparameters with parameters of type PositionAngle

double	CircularParameters.getAlpha(PositionAngle type) Get the latitude argument.
double	EquatorialParameters.getAnomaly(PositionAngle type) Get the anomaly.
double	KeplerianParameters.getAnomaly(PositionAngle type) Get the anomaly.
double	ApsisAltitudeParameters.getAnomaly(PositionAngle type) Get the anomaly.
double	ApsisRadiusParameters.getAnomaly(PositionAngle type) Get the anomaly.
double	EquinoctialParameters.getL(PositionAngle type) Get the longitude argument.

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

ApsisAltitudeParameters(double periapsisAltitude, double apoapsisAltitude, double i, double pa, double raan, double anomaly, PositionAngle type, double mu, double ae)
Creates a new instance.

ApsisRadiusParameters(double periapsis, double apoapsis, double i, double pa, double raan, double anomaly, PositionAngle type, double mu)
Creates a new instance.

CircularParameters(double a, double ex, double ey, double i, double raan, double alpha, PositionAngle type, double mu)
Creates a new instance.

EquatorialParameters(double a, double e, double pomega, double ix, double iy, double anomaly, PositionAngle type, double mu)
Creates a new instance.

EquinoctialParameters(double a, double ex, double ey, double hx, double hy, double l, PositionAngle type, double mu)
Creates a new instance.

KeplerianParameters(double a, double e, double i, double pa, double raan, double anomaly, PositionAngle type, double mu)
Creates a new instance.

Uses of PositionAngle in org.orekit.propagation

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

void	SpacecraftState.mapStateToArray(OrbitType orbitType, PositionAngle angleType, double[] stateVector) Convert SpacecraftState to state vector.

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

SpacecraftState(double[] y, OrbitType orbitType, PositionAngle angleType, AbsoluteDate date, double mu, Frame frame, Map<String,AdditionalStateInfo> addStatesInfo, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents)
Build a spacecraft from an array (a state vector) and an additional states informations map.

Uses of PositionAngle in org.orekit.propagation.events

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

PositionAngle	AnomalyDetector.getAnomalyType() Get the type of anomaly to detect.
PositionAngle	AOLDetector.getAOLType() Get the type of AOL to detect.

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

AdaptedEventDetector(EventDetector detector, Map<String,AdditionalStateInfo> info, OrbitType orbitType, PositionAngle angleType, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, AbsoluteDate referenceDate, double mu, Frame integrationFrame)
Build a wrapped event detector.

AnomalyDetector(PositionAngle angleType, double angle)
Constructor for an AnomalyDetector instance.

AnomalyDetector(PositionAngle angleType, double angle, double maxCheck, double threshold)
Constructor for an AnomalyDetector instance with complementary parameters.

AnomalyDetector(PositionAngle angleType, double angle, double maxCheck, double threshold, EventDetector.Action action)
Constructor for an AnomalyDetector instance with complementary parameters.

AnomalyDetector(PositionAngle angleType, double angle, double maxCheck, double threshold, EventDetector.Action action, boolean remove)
Constructor for an AnomalyDetector instance with complementary parameters.

AOLDetector(double angle, PositionAngle type, Frame equator)
Constructor for an AOLDetector instance.

AOLDetector(double angle, PositionAngle type, Frame equator, double maxCheck, double threshold)
Constructor for an AOLDetector instance with complementary parameters.

AOLDetector(double angle, PositionAngle type, Frame equator, double maxCheck, double threshold, EventDetector.Action action)
Constructor for an AOLDetector instance with complementary parameters.

AOLDetector(double angle, PositionAngle type, Frame equator, double maxCheck, double threshold, EventDetector.Action action, boolean remove)
Constructor for an AOLDetector instance with complementary parameters.

Uses of PositionAngle in org.orekit.propagation.numerical

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

PositionAngle

NumericalPropagator.getPositionAngleType() Get propagation parameter type.

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

void	ModeHandler.initialize(OrbitType orbit, PositionAngle angle, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, Map<String,AdditionalStateInfo> additionalStateInfos, boolean activateHandlers, AbsoluteDate reference, Frame frame, double mu) Initialize the mode handler.
void	NumericalPropagator.setPositionAngleType(PositionAngle positionAngleType) Set position angle type.

Uses of PositionAngle in org.orekit.propagation.precomputed

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

IntegratedEphemeris(List<AbsoluteDate> startDates, List<AbsoluteDate> minDates, List<AbsoluteDate> maxDates, OrbitType orbitType, PositionAngle angleType, AttitudeProvider attitudeForcesProvider, AttitudeProvider attitudeEventsProvider, Map<String,AdditionalStateInfo> additionalStateInfos, List<ContinuousOutputModel> models, Frame referenceFrame, double mu)
Creates a new instance of IntegratedEphemeris.

Uses of PositionAngle in org.orekit.propagation.sampling

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

void

AdaptedStepHandler.initialize(OrbitType orbit, PositionAngle angle, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, Map<String,AdditionalStateInfo> additionalStateInfos, boolean activateHandlers, AbsoluteDate reference, Frame frame, double mu) Initialize the mode handler.