Uses of Class
fr.cnes.sirius.patrius.events.detectors.AbstractSignalPropagationDetector.PropagationDelayType

Packages that use AbstractSignalPropagationDetector.PropagationDelayType

Package	Description
fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.bodies
fr.cnes.sirius.patrius.bodies.mesh
fr.cnes.sirius.patrius.events.detectors
fr.cnes.sirius.patrius.forces.radiation
fr.cnes.sirius.patrius.signalpropagation

Uses of AbstractSignalPropagationDetector.PropagationDelayType in fr.cnes.sirius.patrius.assembly.models

Methods in fr.cnes.sirius.patrius.assembly.models with parameters of type AbstractSignalPropagationDetector.PropagationDelayType

Modifier and Type	Method and Description
double	SensorModel.celestialBodiesMaskingDistance(AbsoluteDate spacecraftDate, AbsoluteDate targetDate, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, VisibilityFromStationDetector.LinkType linkType) Computes the minimal euclidian distance to the celestial body shapes.
static Pair<BodyShape,Double>	SensorModel.computeMinDistToMaskingBodies(AbsoluteDate spacecraftDate, PVCoordinatesProvider orbit, LinkTypeHandler.SignalPropagationRole spacecraftRole, Frame spacecraftFrame, Vector3D targetPosition, List<BodyShape> maskingBodies, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, double epsilonSignalPropagation, int maxIterSignalPropagation) Computes the minimal euclidian distance to the celestial body shapes.
double	SensorModel.getInhibitionTargetAngularRadius(AbsoluteDate inhibitionDate, AbsoluteDate sensorDate, int inhibitionFieldNumber, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType) Computes the angular radius from the sensor of the main target at a date.
double	SensorModel.spacecraftsMaskingDistance(AbsoluteDate spacecraftDate, AbsoluteDate targetDate, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, VisibilityFromStationDetector.LinkType linkType) Computes the minimal euclidian distance to the spacecraft's shapes (GEOMERTY properties).

Uses of AbstractSignalPropagationDetector.PropagationDelayType in fr.cnes.sirius.patrius.bodies

Methods in fr.cnes.sirius.patrius.bodies with parameters of type AbstractSignalPropagationDetector.PropagationDelayType

Modifier and Type	Method and Description
double	VariableRadiusProvider.getApparentRadius(PVCoordinatesProvider pvObserver, AbsoluteDate date, PVCoordinatesProvider occultedBody, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType) Compute the apparent radius (in meters) of the occulting body from the spacecraft (observer) position.
double	ConstantRadiusProvider.getApparentRadius(PVCoordinatesProvider pvObserver, AbsoluteDate date, PVCoordinatesProvider occultedBody, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType) Compute the apparent radius (in meters) of the occulting body from the spacecraft (observer) position.
double	BodyShape.getApparentRadius(PVCoordinatesProvider pvObserver, AbsoluteDate date, PVCoordinatesProvider occultedBody, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType) Compute the apparent radius (in meters) of the occulting body from the spacecraft (observer) position.
double	ApparentRadiusProvider.getApparentRadius(PVCoordinatesProvider pvObserver, AbsoluteDate date, PVCoordinatesProvider occultedBody, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType) Compute the apparent radius (in meters) of the occulting body from the spacecraft (observer) position.
double	AbstractEllipsoidBodyShape.getApparentRadius(PVCoordinatesProvider pvObserver, AbsoluteDate date, PVCoordinatesProvider occultedBody, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType) Compute the apparent radius (in meters) of the occulting body from the spacecraft (observer) position.

Uses of AbstractSignalPropagationDetector.PropagationDelayType in fr.cnes.sirius.patrius.bodies.mesh

Methods in fr.cnes.sirius.patrius.bodies.mesh with parameters of type AbstractSignalPropagationDetector.PropagationDelayType

Modifier and Type	Method and Description
double	FacetBodyShape.getApparentRadius(PVCoordinatesProvider pvObserver, AbsoluteDate date, PVCoordinatesProvider occultedBody, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType) Compute the apparent radius (in meters) of the occulting body from the spacecraft (observer) position.

Uses of AbstractSignalPropagationDetector.PropagationDelayType in fr.cnes.sirius.patrius.events.detectors

Methods in fr.cnes.sirius.patrius.events.detectors that return AbstractSignalPropagationDetector.PropagationDelayType

Modifier and Type	Method and Description
AbstractSignalPropagationDetector.PropagationDelayType	AbstractSignalPropagationDetector.getPropagationDelayType() Getter for the propagation delay type.
static AbstractSignalPropagationDetector.PropagationDelayType	AbstractSignalPropagationDetector.PropagationDelayType.valueOf(String name) Returns the enum constant of this type with the specified name.
static AbstractSignalPropagationDetector.PropagationDelayType[]	AbstractSignalPropagationDetector.PropagationDelayType.values() Returns an array containing the constants of this enum type, in the order they are declared.

Methods in fr.cnes.sirius.patrius.events.detectors with parameters of type AbstractSignalPropagationDetector.PropagationDelayType

Modifier and Type	Method and Description
void	VisibilityFromStationDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame) Setter for the propagation delay computation type.
void	TargetInFieldOfViewDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame)
void	StationToSatMutualVisibilityDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame) Setter for the propagation delay computation type.
void	SolarTimeAngleDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frameIn)
void	SensorVisibilityDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame) Setter for the propagation delay computation type.
void	BetaAngleDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame)
void	ApparentElevationDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame)
void	AbstractSignalPropagationDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayTypeIn, Frame frameIn) Setter for the propagation delay computation type.
void	AbstractEclipseDetector.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame) Setter for the propagation delay computation type.

Uses of AbstractSignalPropagationDetector.PropagationDelayType in fr.cnes.sirius.patrius.forces.radiation

Methods in fr.cnes.sirius.patrius.forces.radiation that return AbstractSignalPropagationDetector.PropagationDelayType

Modifier and Type	Method and Description
AbstractSignalPropagationDetector.PropagationDelayType	SolarRadiationPressure.getPropagationDelayType() Getter for the propagation delay type.
AbstractSignalPropagationDetector.PropagationDelayType	LightingRatio.getPropagationDelayType() Getter for the propagation delay type.

Methods in fr.cnes.sirius.patrius.forces.radiation with parameters of type AbstractSignalPropagationDetector.PropagationDelayType

Modifier and Type	Method and Description
void	SolarRadiationPressure.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayTypeIn, Frame frameIn) Setter for the propagation delay computation type.
void	LightingRatio.setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayTypeIn, Frame frameIn) Setter for the propagation delay computation type.

Uses of AbstractSignalPropagationDetector.PropagationDelayType in fr.cnes.sirius.patrius.signalpropagation

Methods in fr.cnes.sirius.patrius.signalpropagation with parameters of type AbstractSignalPropagationDetector.PropagationDelayType

Modifier and Type	Method and Description
static AbsoluteDate	VacuumSignalPropagationModel.getSignalEmissionDate(PVCoordinatesProvider emitter, PVCoordinatesProvider orbit, AbsoluteDate date, double epsilon, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame inertialFrame) Compute signal emission date which is the date at which the signal received by the spacecraft (receiver) has been emitted by the emitter depending on AbstractSignalPropagationDetector.PropagationDelayType.
static AbsoluteDate	VacuumSignalPropagationModel.getSignalEmissionDate(PVCoordinatesProvider emitter, PVCoordinatesProvider orbit, AbsoluteDate date, double epsilon, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame inertialFrame, int maxIterSignalPropagation) Compute signal emission date which is the date at which the signal received by the spacecraft (receiver) has been emitted by the emitter depending on AbstractSignalPropagationDetector.PropagationDelayType.
static AbsoluteDate	VacuumSignalPropagationModel.getSignalReceptionDate(PVCoordinatesProvider receiver, PVCoordinatesProvider orbit, AbsoluteDate date, double epsilon, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame inertialFrame) Compute signal reception date which is the date at which the signal emitted by the spacecraft (emitter) has been received by the receiver depending on AbstractSignalPropagationDetector.PropagationDelayType.
static AbsoluteDate	VacuumSignalPropagationModel.getSignalReceptionDate(PVCoordinatesProvider receiver, PVCoordinatesProvider orbit, AbsoluteDate date, double epsilon, AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame inertialFrame, int maxIterSignalPropagation) Compute signal reception date which is the date at which the signal emitted by the spacecraft (emitter) has been received by the receiver depending on AbstractSignalPropagationDetector.PropagationDelayType.