public class LocalTimeAngleDetector extends AbstractDetector
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
AbstractDetector.setPropagationDelayType(PropagationDelayType, fr.cnes.sirius.patrius.frames.Frame)
(default is signal being instantaneous).
EventDetector,
Serialized FormAbstractDetector.PropagationDelayTypeEventDetector.ActionactionAtEntry, actionAtExit, DEFAULT_MAXCHECK, 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,
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,
CelestialBody sun)
Constructor for a LocalTimeDetector instance with complimentary parameters including Sun choice.
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| Modifier and Type | Method and Description |
|---|---|
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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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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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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void |
setPropagationDelayType(AbstractDetector.PropagationDelayType propagationDelayType,
Frame frame)
Setter for propagation delay computation type.
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getActionAtEntry, getActionAtExit, getInertialFrame, getMaxCheckInterval, getMaxIterationCount, getPropagationDelayType, getSignalEmissionDate, getSignalReceptionDate, getSlopeSelection, getThreshold, isRemoveAtEntry, isRemoveAtExit, logEventsOverTimeInterval, resetState, setMaxCheckInterval, shouldBeRemovedpublic LocalTimeAngleDetector(double localTimeAngle)
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)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.
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,
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 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,
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 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,
EventDetector.Action action,
boolean remove,
CelestialBody 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 - SunPatriusException - error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public 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 double getTime()
public EventDetector.Action getAction()
public void setPropagationDelayType(AbstractDetector.PropagationDelayType propagationDelayType, Frame frame)
AbstractDetectorsetPropagationDelayType in class AbstractDetectorpropagationDelayType - propagation delay type used in events computationframe - 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.public EventDetector copy()
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