fr.cnes.sirius.patrius.events.detectors

Class CircularFieldOfViewDetector

java.lang.Object

fr.cnes.sirius.patrius.events.AbstractDetector

fr.cnes.sirius.patrius.events.detectors.AbstractSignalPropagationDetector

fr.cnes.sirius.patrius.events.detectors.CircularFieldOfViewDetector

All Implemented Interfaces:

EventDetector, Serializable

public class CircularFieldOfViewDetector
extends AbstractSignalPropagationDetector

Finder for target entry/exit events with respect to a satellite sensor field of view.

This class handle fields of view with a circular boundary.

The default implementation behavior is to continue propagation at fov entry and to stop propagation at fov exit. This can be changed by using the constructor CircularFieldOfViewDetector.

This detector can takes into account signal propagation duration through AbstractSignalPropagationDetector.setPropagationDelayType(PropagationDelayType, Frame) (default is signal being instantaneous).

Author:

Véronique Pommier-Maurussane

See Also:

Propagator.addEventDetector(EventDetector), DihedralFieldOfViewDetector, Serialized Form

Nested Class Summary

Nested classes/interfaces inherited from class fr.cnes.sirius.patrius.events.detectors.AbstractSignalPropagationDetector

AbstractSignalPropagationDetector.DatationChoice, AbstractSignalPropagationDetector.PropagationDelayType

Nested classes/interfaces inherited from interface fr.cnes.sirius.patrius.events.EventDetector

EventDetector.Action

Field Summary

Fields inherited from class fr.cnes.sirius.patrius.events.AbstractDetector

actionAtEntry, actionAtExit, DEFAULT_MAXCHECK, DEFAULT_MAXITER, removeAtEntry, removeAtExit, shouldBeRemovedFlag

Fields inherited from interface fr.cnes.sirius.patrius.events.EventDetector

DECREASING, INCREASING, INCREASING_DECREASING

Constructor Summary

Constructors

Constructor and Description
CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, double halfApertureIn, double maxCheckIn) Build a new instance.
CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, double halfApertureIn, double maxCheck, double threshold) Build a new instance.
CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, double halfApertureIn, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit) Build a new instance with defined actions at fov entry and exit.
CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, double halfApertureIn, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit, boolean removeEntry, boolean removeExit) Build a new instance with defined actions at fov entry and exit.

Method Summary

Modifier and Type	Method and Description
EventDetector	copy() A copy of the detector.
EventDetector.Action	eventOccurred(SpacecraftState s, boolean increasing, boolean forward) Handle an fov event and choose what to do next.
double	g(SpacecraftState s) Compute the value of the switching function.
Vector3D	getCenter() Get the direction of fov center.
AbstractSignalPropagationDetector.DatationChoice	getDatationChoice() Specify if the datation choice corresponds to the emitter date or the receiver date.
PVCoordinatesProvider	getEmitter(SpacecraftState s) Getter for the signal emitter.
double	getHalfAperture() Get fov half aperture angle.
PVCoordinatesProvider	getPVTarget() Get the position/velocity provider of the target .
PVCoordinatesProvider	getReceiver(SpacecraftState s) Getter for the signal receiver.
void	setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame) Setter for the propagation delay computation type.

Methods inherited from class fr.cnes.sirius.patrius.events.detectors.AbstractSignalPropagationDetector

getEpsilonSignalPropagation, getInertialFrame, getMaxIterSignalPropagation, getPropagationDelayType, getSignalEmissionDate, getSignalEmissionDate, getSignalReceptionDate, getSignalReceptionDate, setEpsilonSignalPropagation, setMaxIterSignalPropagation

Methods inherited from class fr.cnes.sirius.patrius.events.AbstractDetector

filterEvent, getActionAtEntry, getActionAtExit, getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, init, isRemoveAtEntry, isRemoveAtExit, logEventsOverTimeInterval, resetState, setMaxCheckInterval, setMaxIter, shouldBeRemoved

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Constructor Detail

CircularFieldOfViewDetector

public CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget,
                                   Vector3D centerIn,
                                   double halfApertureIn,
                                   double maxCheckIn)

Build a new instance.

The maximal interval between distance to fov boundary checks should be smaller than the half duration of the minimal pass to handle, otherwise some short passes could be missed.

The default implementation behavior is to continue propagation at fov entry and to stop propagation at fov exit.

Parameters:

pvTarget - Position/velocity provider of the considered target

centerIn - Direction of the fov center, in spacecraft frame

halfApertureIn - Fov half aperture angle

maxCheckIn - maximal interval in seconds

CircularFieldOfViewDetector

public CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget,
                                   Vector3D centerIn,
                                   double halfApertureIn,
                                   double maxCheck,
                                   double threshold)

Build a new instance.

The maximal interval between distance to fov boundary checks should be smaller than the half duration of the minimal pass to handle, otherwise some short passes could be missed.

The default implementation behavior is to continue propagation at fov entry and to stop propagation at fov exit.

Parameters:

pvTarget - Position/velocity provider of the considered target

centerIn - Direction of the fov center, in spacecraft frame

halfApertureIn - Fov half aperture angle

maxCheck - maximal interval in seconds

threshold - threshold in seconds for events date computation

CircularFieldOfViewDetector

public CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget,
                                   Vector3D centerIn,
                                   double halfApertureIn,
                                   double maxCheck,
                                   double threshold,
                                   EventDetector.Action entry,
                                   EventDetector.Action exit)

Build a new instance with defined actions at fov entry and exit.

The maximal interval between distance to fov boundary checks should be smaller than the half duration of the minimal pass to handle, otherwise some short passes could be missed.

Parameters:

pvTarget - Position/velocity provider of the considered target

centerIn - Direction of the fov center, in spacecraft frame

halfApertureIn - Fov half aperture angle

maxCheck - maximal interval in seconds

threshold - threshold in seconds for events date computation

entry - action performed at fov entry

exit - action performed at fov exit

CircularFieldOfViewDetector

public CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget,
                                   Vector3D centerIn,
                                   double halfApertureIn,
                                   double maxCheck,
                                   double threshold,
                                   EventDetector.Action entry,
                                   EventDetector.Action exit,
                                   boolean removeEntry,
                                   boolean removeExit)

Build a new instance with defined actions at fov entry and exit.

The maximal interval between distance to fov boundary checks should be smaller than the half duration of the minimal pass to handle, otherwise some short passes could be missed.

Parameters:

pvTarget - Position/velocity provider of the considered target

centerIn - Direction of the fov center, in spacecraft frame

halfApertureIn - Fov half aperture angle

maxCheck - maximal interval in seconds

threshold - threshold in seconds for events date computation

entry - action performed at fov entry

exit - action performed at fov exit

removeEntry - true if detector should be removed at fov entry

removeExit - true if detector should be removed at fov exit

Since:

3.1

Method Detail

getPVTarget

public PVCoordinatesProvider getPVTarget()

Get the position/velocity provider of the target .

Returns:

the position/velocity provider of the target

getCenter

public Vector3D getCenter()

Get the direction of fov center.

Returns:

the direction of fov center

getHalfAperture

public double getHalfAperture()

Get fov half aperture angle.

Returns:

the fov half aperture angle

eventOccurred

public EventDetector.Action eventOccurred(SpacecraftState s,
                                          boolean increasing,
                                          boolean forward)
                                   throws PatriusException

Handle an fov event and choose what to do next.

The default implementation behavior is to continue propagation at entry and to stop propagation at exit. This can be changed by using the constructor CircularFieldOfViewDetector

Specified by:

eventOccurred in interface EventDetector

Overrides:

eventOccurred in class AbstractDetector

Parameters:

s - the current state information : date, kinematics, attitude

increasing - if true, the value of the switching function increases when times increases around event, i.e. target enters the fov (note that increase is measured with respect to physical time, not with respect to propagation which may go backward in time)

forward - if true, the integration variable (time) increases during integration.

Returns:

the action performed at expected fov entry or exit.

Throws:

PatriusException - if some specific error occurs

g

public double g(SpacecraftState s)
         throws PatriusException

Compute the value of the switching function. This function must be continuous (at least in its roots neighborhood), as the integrator will need to find its roots to locate the events. g function value is the difference between fov half aperture and the absolute value of the angle between target direction and field of view center. It is positive inside the fov and negative outside.

Specified by:

g in interface EventDetector

Specified by:

g in class AbstractDetector

Parameters:

s - the current state information: date, kinematics, attitude for forces and events computation, mass provider, and additional states

Returns:

value of the switching function

Throws:

PatriusException - if some specific error occurs

setPropagationDelayType

public void setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType,
                                    Frame frame)

Description copied from class: AbstractSignalPropagationDetector

Setter for the propagation delay computation type. Warning: check Javadoc of detector to see if detector takes into account propagation time delay. if not, signals are always considered instantaneous. The provided frame is used to compute the signal propagation when delay is taken into account.

Overrides:

setPropagationDelayType in class AbstractSignalPropagationDetector

Parameters:

propagationDelayType - Propagation delay type used in events computation

frame - Frame to use for signal propagation with delay (may be null if propagation delay type is considered instantaneous). Warning: the usage of a pseudo inertial frame is tolerated, however it will lead to some inaccuracies due to the non-invariance of the frame with respect to time. For this reason, it is suggested to use the ICRF frame or a frame which is frozen with respect to the ICRF.

getEmitter

public PVCoordinatesProvider getEmitter(SpacecraftState s)

Getter for the signal emitter.

Specified by:

getEmitter in class AbstractSignalPropagationDetector

Parameters:

s - the spacecraft state used by the detector

Returns:

the signal emitter

getReceiver

public PVCoordinatesProvider getReceiver(SpacecraftState s)

Getter for the signal receiver.

Specified by:

getReceiver in class AbstractSignalPropagationDetector

Parameters:

s - the spacecraft state used by the detector

Returns:

the signal receiver

getDatationChoice

public AbstractSignalPropagationDetector.DatationChoice getDatationChoice()

Specify if the datation choice corresponds to the emitter date or the receiver date.

Specified by:

getDatationChoice in class AbstractSignalPropagationDetector

Returns:

the corresponding datation choice

copy

public EventDetector copy()

A copy of the detector. By default copy is deep. If not, detector javadoc will specify which attribute is not fully copied. In that case, the attribute reference is passed.

The following attributes are not deeply copied:

• targetPVProvider: PVCoordinatesProvider

Returns:

a copy of the detector.