public class LocalTimeAngleDetector extends AbstractSignalPropagationDetector
The default implementation is to stop propagation when the local time is reached.
This can be changed by using provided constructors.
This detector can takes into account signal propagation duration through
AbstractSignalPropagationDetector.setPropagationDelayType(PropagationDelayType, Frame) (default is signal being instantaneous).
EventDetector,
Serialized FormAbstractSignalPropagationDetector.EventDatationType, AbstractSignalPropagationDetector.PropagationDelayTypeEventDetector.ActionactionAtEntry, actionAtExit, DEFAULT_MAXCHECK, DEFAULT_MAXITER, DEFAULT_THRESHOLD, removeAtEntry, removeAtExit, shouldBeRemovedFlagDECREASING, INCREASING, INCREASING_DECREASING| Constructor and Description |
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LocalTimeAngleDetector(double localTimeAngle)
Constructor for a LocalTimeDetector instance.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold)
Constructor for a LocalTimeDetector instance with complimentary parameters.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame)
Constructor for a LocalTimeDetector instance with complimentary parameters.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action)
Constructor for a LocalTimeDetector instance with complimentary parameters.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove)
Constructor for a LocalTimeDetector instance with complimentary parameters.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove,
PVCoordinatesProvider sun)
Constructor for a LocalTimeDetector instance with complimentary parameters including Sun choice.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove,
PVCoordinatesProvider sun,
int slopeSelection)
Constructor for a LocalTimeDetector instance with complimentary parameters including Sun choice.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for a LocalTimeDetector instance with complimentary parameters.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for a LocalTimeDetector instance with complimentary parameters.
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LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove,
PVCoordinatesProvider sun)
Constructor for a LocalTimeDetector instance with complimentary parameters including Sun choice.
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| Modifier and Type | Method and Description |
|---|---|
protected double |
computeLocalTime(SpacecraftState state)
Compute the local time.
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protected double |
computeSunSatAngle(Vector3D satPos,
Vector3D sunPos)
Compute the angle between the sun and the satellite projections over the equatiorial plane
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EventDetector |
copy()
A copy of the detector.
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EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handle a local time angle event and choose what to do next.
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boolean |
filterEvent(SpacecraftState state,
boolean increasing,
boolean forward)
Filter last event: returns true if the last event is a false detection, false otherwise.
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double |
g(SpacecraftState state)
Compute the value of the switching function.
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EventDetector.Action |
getAction()
Return the action at detection.
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CelestialBodyFrame |
getFrame()
Returns the frame used for solar time computation.
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PVCoordinatesProvider |
getSun()
Return the sun
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double |
getTime()
Get local time angle to detect.
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void |
init(SpacecraftState s0,
AbsoluteDate t)
Initialize event handler at the start of a propagation.
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getEmitter, getEpsilonSignalPropagation, getEventDatationType, getInertialFrame, getLinkTypeHandler, getMaxIterSignalPropagation, getOtherDate, getPropagationDelayType, getReceiver, getSignalEmissionDate, getSignalEmissionDate, getSignalReceptionDate, getSignalReceptionDate, setEpsilonSignalPropagation, setMaxIterSignalPropagation, setPropagationDelayTypegetActionAtEntry, getActionAtExit, getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, isRemoveAtEntry, isRemoveAtExit, logEventsOverTimeInterval, resetState, setMaxCheckInterval, setMaxIter, shouldBeRemovedpublic LocalTimeAngleDetector(double localTimeAngle)
throws PatriusException
Local time will be computed in satellite orbit frame.
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)PatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold)
throws PatriusException
The default implementation behavior is to stop propagation when the local time
is reached.
Local time will be computed in satellite orbit frame.
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)PatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame)
throws PatriusException
The default implementation behavior is to stop propagation when the local time
is reached.
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)frame - in relation to which the calculations are madePatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action)
throws PatriusException
Local time will be computed in satellite orbit frame.
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at local time detectionPatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action)
throws PatriusException
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at local time detectionframe - in relation to which the calculations are madePatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
throws PatriusException
Local time will be computed in satellite orbit frame.
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at local time detectionremove - true if detector should be removedPatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove)
throws PatriusException
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at local time detectionremove - true if detector should be removedframe - in relation to which the calculations are madePatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove,
PVCoordinatesProvider sun)
throws PatriusException
Local time will be computed in satellite orbit frame.
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at local time detectionremove - true if detector should be removedsun - SunPatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove,
PVCoordinatesProvider sun)
throws PatriusException
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at local time detectionremove - true if detector should be removedsun - Sunframe - in relation to which the calculations are madePatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove,
PVCoordinatesProvider sun,
int slopeSelection)
throws PatriusException
localTimeAngle - satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at local time detectionremove - true if detector should be removedsun - Sunframe - in relation to which the calculations are madeslopeSelection - NodeDetector.ASCENDING for ascending node detection,NodeDetector.DESCENDING for descending node detection,NodeDetector.ASCENDING_DESCENDING for both ascending and descending node
detection.PatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic EventDetector.Action eventOccurred(SpacecraftState s, boolean increasing, boolean forward) throws PatriusException
eventOccurred in interface EventDetectoreventOccurred in class AbstractDetectors - the current state information : date, kinematics, attitudeincreasing - if true, the value of the switching function increases when time increases
around eventforward - if true, the integration variable (time) increases during integration.PatriusException - if some specific error occurspublic double g(SpacecraftState state) throws PatriusException
g in interface EventDetectorg in class AbstractDetectorstate - the current state information: date, kinematics, attitude for forces and events
computation, mass provider, and additional statesPatriusException - if some specific error occurspublic void init(SpacecraftState s0, AbsoluteDate t)
This method is called once at the start of the propagation. It may be used by the event handler to initialize some internal data if needed.
init in interface EventDetectorinit in class AbstractDetectors0 - initial statet - target time for the integrationpublic boolean filterEvent(SpacecraftState state, boolean increasing, boolean forward) throws PatriusException
This method is called right before EventDetector.eventOccurred(SpacecraftState, boolean, boolean) method.
This may be useful in order to filter some events in particular when angles are at stake (see for example
LocalTimeAngleDetector).
filterEvent in interface EventDetectorfilterEvent in class AbstractDetectorstate - state at last event occurrenceincreasing - if true, the value of the switching function increases when times increases
around event (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.PatriusException - thrown if computation failed for some reasonsprotected double computeLocalTime(SpacecraftState state) throws PatriusException
state - current statePatriusException - thrown if computation failedprotected double computeSunSatAngle(Vector3D satPos, Vector3D sunPos)
satPos - satellite positionsunPos - sun positionpublic double getTime()
public EventDetector.Action getAction()
public CelestialBodyFrame getFrame()
public PVCoordinatesProvider getSun()
public EventDetector copy()
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