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.
EventDetector,
Serialized FormEventDetector.ActionDEFAULT_MAXCHECK, DEFAULT_THRESHOLDDECREASING, INCREASING, INCREASING_DECREASING| Constructor and Description |
|---|
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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| Modifier and Type | Method and Description |
|---|---|
EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handle a local time angle event and choose what to do next.
|
double |
g(SpacecraftState s)
Compute the value of the switching function.
|
double |
getTime()
Get local time angle to detect.
|
void |
init(SpacecraftState s0,
AbsoluteDate t)
Initialize event handler at the start of a propagation.
|
boolean |
shouldBeRemoved()
This method is called after
EventDetector.eventOccurred(fr.cnes.sirius.patrius.propagation.SpacecraftState, boolean, boolean) has been triggered. |
getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, resetStatepublic 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 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 boolean shouldBeRemoved()
EventDetector.eventOccurred(fr.cnes.sirius.patrius.propagation.SpacecraftState, boolean, boolean) has been triggered.
It returns true if the current detector should be removed after first event detection.
WARNING: this method can be called only once a event has been triggered. Before,
the value is not available.shouldBeRemoved in interface EventDetectorshouldBeRemoved in class AbstractDetectorpublic double g(SpacecraftState s) throws PatriusException
AbstractDetectorg in interface EventDetectorg in class AbstractDetectors - 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)
AbstractDetectorThis 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()
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