Uses of Class
fr.cnes.sirius.patrius.orbits.PositionAngle

Packages that use PositionAngle

Package	Description
fr.cnes.sirius.patrius.covariance
fr.cnes.sirius.patrius.forces.maneuvers
fr.cnes.sirius.patrius.math.parameter
fr.cnes.sirius.patrius.orbits
fr.cnes.sirius.patrius.orbits.orbitalparameters
fr.cnes.sirius.patrius.propagation
fr.cnes.sirius.patrius.propagation.events
fr.cnes.sirius.patrius.propagation.events.multi
fr.cnes.sirius.patrius.propagation.numerical
fr.cnes.sirius.patrius.propagation.numerical.multi
fr.cnes.sirius.patrius.propagation.precomputed
fr.cnes.sirius.patrius.propagation.precomputed.multi
fr.cnes.sirius.patrius.propagation.sampling
fr.cnes.sirius.patrius.propagation.sampling.multi
fr.cnes.sirius.patrius.stela.orbits

Uses of PositionAngle in fr.cnes.sirius.patrius.covariance

Methods in fr.cnes.sirius.patrius.covariance that return PositionAngle

Modifier and Type	Method and Description
PositionAngle	AbstractOrbitalCovariance.getPositionAngle() Gets the position angle type of the covariance.

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

Modifier and Type	Method and Description
protected static List<ParameterDescriptor>	AbstractOrbitalCovariance.convertParameterDescriptors(Collection<ParameterDescriptor> parameterDescriptors, OrbitType destOrbitType, PositionAngle destPositionAngle) Returns an updated list of parameter descriptors where the orbital coordinates mapped to the orbital coordinate descriptors were all converted to the specified orbit type and position angle type.
abstract T	AbstractOrbitalCovariance.transformTo(Frame destFrame, OrbitType destOrbitType, PositionAngle destPositionAngle) Transforms this orbital covariance to the specified frame, orbit type and position angle type.
OrbitalCovariance	OrbitalCovariance.transformTo(Frame destFrame, OrbitType destOrbitType, PositionAngle destPositionAngle) Transforms this orbital covariance to the specified frame, orbit type and position angle type.
MultiOrbitalCovariance	MultiOrbitalCovariance.transformTo(Frame destFrame, OrbitType destOrbitType, PositionAngle destPositionAngle) Transforms this orbital covariance to the specified frame, orbit type and position angle type.
T	AbstractOrbitalCovariance.transformTo(OrbitType destOrbitType, PositionAngle destPositionAngle) Transforms this orbital covariance to the specified orbit type and position angle type.
T	AbstractOrbitalCovariance.transformTo(PositionAngle destPositionAngle) Transforms this orbital covariance to the specified position angle type.

Constructors in fr.cnes.sirius.patrius.covariance with parameters of type PositionAngle

Constructor and Description
AbstractOrbitalCovariance(Covariance covarianceIn, Frame frameIn, OrbitType orbitTypeIn, PositionAngle positionAngleIn) Creates a new instance from the supplied covariance, frame, orbit type and position angle type.
AbstractOrbitalCovariance(SymmetricPositiveMatrix covarianceIn, Frame frameIn, OrbitType orbitTypeIn, PositionAngle positionAngleIn) Creates a new instance from the supplied covariance matrix, frame, orbit type and position angle type.
MultiOrbitalCovariance(Covariance covariance, Collection<Orbit> orbits, int[] nbAdditionalParametersIn, Frame frame, OrbitType orbitType, PositionAngle positionAngle) Creates a new instance that associates a covariance matrix with multiple orbits, the covariance being defined in the specified frame, orbit type and position angle type.
MultiOrbitalCovariance(SymmetricPositiveMatrix covarianceMatrix, Collection<Orbit> orbits, int[] nbAdditionalParametersIn, Frame frame, OrbitType orbitType, PositionAngle positionAngle) Creates a new instance that associates a covariance matrix with multiple orbits, the covariance being defined in the specified frame, orbit type and position angle type.
OrbitalCovariance(Covariance covariance, Orbit orbit, Frame frame, OrbitType orbitType, PositionAngle positionAngle) Creates a new instance that associates a covariance matrix with a given orbit, the covariance being defined in the specified frame, orbit type and position angle type.
OrbitalCovariance(Covariance covariance, Orbit orbit, PositionAngle positionAngle) Creates a new instance that associates a covariance matrix with a given orbit, the covariance being defined in the orbit's frame and type, and the specified position angle type.
OrbitalCovariance(SymmetricPositiveMatrix covarianceMatrix, Orbit orbit, Frame frame, OrbitType orbitType, PositionAngle positionAngle) Creates a new instance that associates a covariance matrix with a given orbit, the covariance being defined in the specified frame, orbit type and position angle type.
OrbitalCovariance(SymmetricPositiveMatrix covarianceMatrix, Orbit orbit, PositionAngle positionAngle) Creates a new instance that associates a covariance matrix with a given orbit, the covariance being defined in the orbit's frame and type, and the specified position angle type.

Uses of PositionAngle in fr.cnes.sirius.patrius.forces.maneuvers

Methods in fr.cnes.sirius.patrius.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 fr.cnes.sirius.patrius.math.parameter

Methods in fr.cnes.sirius.patrius.math.parameter with parameters of type PositionAngle

Modifier and Type	Method and Description
static List<ParameterDescriptor>	ParameterUtils.buildOrbitalParameterDescriptors(OrbitType orbitType, PositionAngle positionAngle) Builds the parameter descriptors associated with a given orbit type and position angle type, each representing one of the orbital coordinates.
static List<Parameter>	ParameterUtils.buildOrbitalParameters(OrbitType orbitType, PositionAngle positionAngle) Builds the parameters associated with a given orbit type and position angle type, each one representing one of the orbital coordinates.

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

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

Modifier and Type	Method and Description
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.
abstract OrbitalCoordinate	OrbitType.getCoordinateType(int stateVectorIndex, PositionAngle positionAngle) Gets the coordinate type associated with a given state vector index.
RealMatrix	Orbit.getJacobian(double dt, Frame initFrame, Frame destFrame, OrbitType initOrbitType, OrbitType destOrbitType, PositionAngle initAngleType, PositionAngle destAngleType) Computes the Jacobian of the transformation between the specified frames, orbit types and position angle types with respect to this orbit and specified time shift.
RealMatrix	Orbit.getJacobian(Frame initFrame, Frame destFrame, OrbitType initOrbitType, OrbitType destOrbitType, PositionAngle initAngleType, PositionAngle destAngleType) Computes the Jacobian of the transformation between the specified frames, orbit types and position angle types with respect to this orbit.
RealMatrix	Orbit.getJacobian(OrbitType numerator, OrbitType denominator, PositionAngle positionAngle) Get coordinate conversion jacobian.
void	Orbit.getJacobianWrtCartesian(PositionAngle type, double[][] jacobian) Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
void	EquinoctialOrbit.getJacobianWrtParameters(PositionAngle type, double[][] jacobian) Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
void	AlternateEquinoctialOrbit.getJacobianWrtParameters(PositionAngle type, double[][] jacobian) Compute the Jacobian of the Cartesian parameters with respect to the orbital 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.
double	AlternateEquinoctialOrbit.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 fr.cnes.sirius.patrius.orbits with parameters of type PositionAngle

Constructor and Description
AlternateEquinoctialOrbit(double n, double ex, double ey, double hx, double hy, double l, PositionAngle type, Frame frame, AbsoluteDate date, double mu) Creates a new instance.
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 fr.cnes.sirius.patrius.orbits.orbitalparameters

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

Modifier and Type	Method and Description
default OrbitalCoordinate	OrbitalCoordinate.convertTo(OrbitType orbitType, PositionAngle positionAngle) Gets the coordinate type associated with the same state vector index in a given orbit type and position angle type.
double	CircularParameters.getAlpha(PositionAngle type) Get the latitude argument.
double	KeplerianParameters.getAnomaly(PositionAngle type) Get the anomaly.
double	ApsisAltitudeParameters.getAnomaly(PositionAngle type) Get the anomaly.
double	EquatorialParameters.getAnomaly(PositionAngle type) Get the anomaly.
double	ApsisRadiusParameters.getAnomaly(PositionAngle type) Get the anomaly.
double	EquinoctialParameters.getL(PositionAngle type) Get the longitude argument.
double	AlternateEquinoctialParameters.getL(PositionAngle type) Get the longitude argument.
static ApsisAltitudeCoordinate	ApsisAltitudeCoordinate.valueOf(int stateVectorIndex, PositionAngle positionAngle) Gets the coordinate type associated with a given state vector index.
static CircularCoordinate	CircularCoordinate.valueOf(int stateVectorIndex, PositionAngle positionAngle) Gets the coordinate type associated with a given state vector index.
static ApsisRadiusCoordinate	ApsisRadiusCoordinate.valueOf(int stateVectorIndex, PositionAngle positionAngle) Gets the coordinate type associated with a given state vector index.
static AlternateEquinoctialCoordinate	AlternateEquinoctialCoordinate.valueOf(int stateVectorIndex, PositionAngle positionAngle) Gets the coordinate type associated with a given state vector index.
static EquatorialCoordinate	EquatorialCoordinate.valueOf(int stateVectorIndex, PositionAngle positionAngle) Gets the coordinate type associated with a given state vector index.
static KeplerianCoordinate	KeplerianCoordinate.valueOf(int stateVectorIndex, PositionAngle positionAngle) Gets the coordinate type associated with a given state vector index.
static EquinoctialCoordinate	EquinoctialCoordinate.valueOf(int stateVectorIndex, PositionAngle positionAngle) Gets the coordinate type associated with a given state vector index.

Constructors in fr.cnes.sirius.patrius.orbits.orbitalparameters with parameters of type PositionAngle

Constructor and Description
AlternateEquinoctialParameters(double nIn, double exIn, double eyIn, double hxIn, double hyIn, double l, PositionAngle type, double mu) Creates a new instance.
ApsisAltitudeParameters(double periapsisAltitudeIn, double apoapsisAltitudeIn, double i, double pa, double raan, double anomaly, PositionAngle type, double mu, double aeIn) Creates a new instance.
ApsisRadiusParameters(double periapsisIn, double apoapsisIn, double i, double pa, double raan, double anomaly, PositionAngle type, double mu) Creates a new instance.
CircularParameters(double aIn, double exIn, double eyIn, double iIn, double raanIn, double alpha, PositionAngle type, double mu) Creates a new instance.
EquatorialParameters(double aIn, double eIn, double pomegaIn, double ixIn, double iyIn, double anomaly, PositionAngle type, double mu) Creates a new instance.
EquinoctialParameters(double aIn, double exIn, double eyIn, double hxIn, double hyIn, double l, PositionAngle type, double mu) Creates a new instance.
KeplerianParameters(double aIn, double eIn, double iIn, double paIn, double raanIn, double anomaly, PositionAngle type, double mu) Creates a new instance.

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

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

Modifier and Type	Method and Description
void	SpacecraftState.mapStateToArray(OrbitType orbitType, PositionAngle angleType, double[] stateVector) Convert SpacecraftState to state vector.

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

Constructor and Description
SpacecraftState(double[] y, OrbitType orbitType, PositionAngle angleType, AbsoluteDate date, double mu, Frame frame, Map<String,AdditionalStateInfo> addStatesInfo, Attitude attForces, Attitude attEvents) Build a spacecraft from an array (a state vector) and an additional states informations map.
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 fr.cnes.sirius.patrius.propagation.events

Methods in fr.cnes.sirius.patrius.propagation.events that return PositionAngle

Modifier and Type	Method and Description
PositionAngle	AnomalyDetector.getAnomalyType() Get the type of anomaly to detect.
PositionAngle	AOLDetector.getAOLType() Get the type of AOL to detect.

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

Modifier and Type	Method and Description
void	AdaptedEventDetector.reinitialize(Map<String,AdditionalStateInfo> info, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, AbsoluteDate referenceDateIn, double muIn, Frame integrationFrameIn) Reinitialize reference data.

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

Constructor and Description
AdaptedEventDetector(EventDetector detectorIn, Map<String,AdditionalStateInfo> info, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, AbsoluteDate referenceDateIn, double muIn, Frame integrationFrameIn) 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.
CenteredAolPassageDetector(double aol, PositionAngle positionAngle, MeanOsculatingElementsProvider provider, Frame frame) Constructor
CenteredAolPassageDetector(double aol, PositionAngle positionAngle, MeanOsculatingElementsProvider provider, Frame frame, double maxCheck, double threshold) Constructor with complementary parameters
CenteredAolPassageDetector(double aol, PositionAngle positionAngle, MeanOsculatingElementsProvider provider, Frame frame, double maxCheck, double threshold, EventDetector.Action action) Constructor with complementary parameters

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

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

Modifier and Type	Method and Description
void	AdaptedMultiEventDetector.reinitialize(OrbitType orbitType, PositionAngle angleType, Map<String,MultiAttitudeProvider> attProvidersForces, Map<String,MultiAttitudeProvider> attProvidersEvents, AbsoluteDate referenceDate, Map<String,Double> muMap, Map<String,Frame> framesMap, MultiStateVectorInfo stateVectorInfo) Reinitialize data.
void	AdaptedMonoEventDetector.reinitialize(OrbitType orbitType, PositionAngle angleType, MultiAttitudeProvider attProviderForces, MultiAttitudeProvider attProviderEvents, AbsoluteDate referenceDate, MultiStateVectorInfo stateVectorInfo, String satId) Reinitialize data.

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

Constructor and Description
AdaptedMonoEventDetector(EventDetector detector, OrbitType orbitType, PositionAngle angleType, MultiAttitudeProvider attProviderForces, MultiAttitudeProvider attProviderEvents, AbsoluteDate referenceDate, MultiStateVectorInfo stateVectorInfo, String satId) Build a wrapped event detector.
AdaptedMultiEventDetector(MultiEventDetector detector, OrbitType orbitType, PositionAngle angleType, Map<String,MultiAttitudeProvider> attProvidersForces, Map<String,MultiAttitudeProvider> 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

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

Modifier and Type	Method and Description
PositionAngle	JacobiansMapper.getAngleType() Getter for the position angle type.
protected PositionAngle	PartialDerivativesEquations.getPositionAngle() Returns the propagator position angle.
protected abstract PositionAngle	AbstractPartialDerivativesEquations.getPositionAngle() Returns the propagator position angle.
PositionAngle	NumericalPropagator.getPositionAngleType() Get propagation parameter type.

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

Modifier and Type	Method and Description
void	JacobiansMapper.getParametersJacobian(Parameter parameter, SpacecraftState state, double[] dYdP, OrbitType orbitTypeIn, PositionAngle angleTypeIn, Frame frameIn) Get the Jacobian with respect to provided parameter parameter.
double[]	JacobiansMapper.getParametersJacobian(Parameter parameter, SpacecraftState state, OrbitType orbitTypeIn, PositionAngle angleTypeIn, Frame frameIn) Get the Jacobian with respect to provided parameter parameter.
void	JacobiansMapper.getParametersJacobian(SpacecraftState state, double[][] dYdP, OrbitType orbitTypeIn, PositionAngle angleTypeIn, Frame frameIn) Get the Jacobian with respect to parameters.
double[][]	JacobiansMapper.getParametersJacobian(SpacecraftState state, OrbitType orbitTypeOut, PositionAngle angleTypeOut, Frame frameOut) Get the Jacobian with respect to parameters.
void	JacobiansMapper.getStateJacobian(SpacecraftState state, double[][] dYdY0, OrbitType orbitTypeIn, PositionAngle angleTypeIn, Frame frameIn) Get the Jacobian with respect to state.
double[][]	JacobiansMapper.getStateJacobian(SpacecraftState state, OrbitType orbitTypeOut, PositionAngle angleTypeOut, Frame frameOut) Get the Jacobian with respect to state.
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.

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

Constructor and Description
JacobiansMapper(String nameIn, List<Parameter> list, OrbitType orbitTypeIn, PositionAngle angleTypeIn, Frame frame) Simple constructor.
NumericalPropagator(FirstOrderIntegrator integratorIn, Frame propagationFrameIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn) Create a new instance of NumericalPropagator, based on orbit definition mu.

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

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

Modifier and Type	Method and Description
protected PositionAngle	MultiPartialDerivativesEquations.getPositionAngle() Returns the propagator position angle.
PositionAngle	MultiNumericalPropagator.getPositionAngleType() Get propagation parameter type.

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

Modifier and Type	Method and Description
void	MultiEphemerisModeHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,MultiAttitudeProvider> attitudeProvidersForces, Map<String,MultiAttitudeProvider> 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,MultiAttitudeProvider> attitudeProvidersForces, Map<String,MultiAttitudeProvider> 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, MultiAttitudeProvider attProviderForces, MultiAttitudeProvider attProviderEvents, String id) Extract a given SpacecraftState from the state vector.
Map<String,SpacecraftState>	MultiStateVectorInfo.mapArrayToStates(double[] y, AbsoluteDate currentDate, OrbitType orbitType, PositionAngle angleType, Map<String,MultiAttitudeProvider> attProvidersForces, Map<String,MultiAttitudeProvider> 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.

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

Constructor and Description
MultiNumericalPropagator(FirstOrderIntegrator integratorIn, Map<String,Frame> propagationFrameMapIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn) Create a new instance of MultiNumericalPropagator.

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

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

Constructor and Description
IntegratedEphemeris(List<AbsoluteDate> startDatesIn, List<AbsoluteDate> minDatesIn, List<AbsoluteDate> maxDatesIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attitudeForcesProvider, AttitudeProvider attitudeEventsProvider, Map<String,AdditionalStateInfo> additionalStateInfos, List<ContinuousOutputModel> modelsIn, Frame referenceFrameIn, double muIn) Creates a new instance of IntegratedEphemeris.
IntegratedEphemeris(List<AbsoluteDate> startDatesIn, List<AbsoluteDate> minDatesIn, List<AbsoluteDate> maxDatesIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attitudeProvider, Map<String,AdditionalStateInfo> additionalStateInfos, List<ContinuousOutputModel> modelsIn, Frame referenceFrameIn, double muIn) Creates a new instance of IntegratedEphemeris.

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

Constructor and Description

MultiIntegratedEphemeris(List<AbsoluteDate> startDatesIn, List<AbsoluteDate> minDatesIn, List<AbsoluteDate> maxDatesIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn, MultiAttitudeProvider multiAttitudeProviderForcesIn, MultiAttitudeProvider multiAttitudeProviderEventsIn, MultiStateVectorInfo stateInfos, List<ContinuousOutputModel> modelsIn, Frame referenceFrameIn, String satIdIn) Creates a new instance of IntegratedEphemeris.

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

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

Modifier and Type	Method and Description
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.

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

Modifier and Type	Method and Description
void	MultiAdaptedStepHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,MultiAttitudeProvider> attProvidersForces, Map<String,MultiAttitudeProvider> 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

Modifier and Type	Method and Description
void	StelaEquinoctialOrbit.addKeplerContribution(PositionAngle type, double gm, double[] pDot) Call the method StelaEquinoctialOrbit.orbitAddKeplerContribution(PositionAngle, double, double[]) implemented in inherited classes of Orbit.
protected void	StelaEquinoctialOrbit.orbitAddKeplerContribution(PositionAngle type, double gm, double[] pDot) Add the contribution of the Keplerian motion to parameters derivatives