public class AOLDetector extends AbstractDetector
The default implementation behaviour is to stop propagation when the angle θ
is reached. This can be changed by using provided constructors.
EventDetector,
Serialized FormEventDetector.ActionDEFAULT_MAXCHECK, DEFAULT_THRESHOLDDECREASING, INCREASING, INCREASING_DECREASING| Constructor and Description |
|---|
AOLDetector(double angle,
PositionAngle type,
Frame equator)
Constructor for an AOLDetector instance.
|
AOLDetector(double angle,
PositionAngle type,
Frame equator,
double maxCheck,
double threshold)
Constructor for an AOLDetector instance with complementary parameters.
|
AOLDetector(double angle,
PositionAngle type,
Frame equator,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for an AOLDetector instance with complementary parameters.
|
AOLDetector(double angle,
PositionAngle type,
Frame equator,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for an AOLDetector instance with complementary parameters.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handle an AOL event and choose what to do next.
|
double |
g(SpacecraftState s)
Compute the value of the switching function.
|
double |
getAOL()
Get the AOL to detect.
|
Frame |
getAOLFrame()
Get the reference frame.
|
PositionAngle |
getAOLType()
Get the type of AOL 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 AOLDetector(double angle,
PositionAngle type,
Frame equator)
angle - AOL value triggering the event.type - type of AOL to detect, one of TRUE, MEAN and ECCENTRIC.equator - equator with respect to which the AOL is to be computedPositionAnglepublic AOLDetector(double angle,
PositionAngle type,
Frame equator,
double maxCheck,
double threshold)
The default implementation behaviour is to stop propagation when the AOL angle
is reached.
angle - AOL value triggering the event.type - type of AOL to detect, one of TRUE, MEAN and ECCENTRIC.equator - equator with respect to which the AOL is to be computedmaxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)public AOLDetector(double angle,
PositionAngle type,
Frame equator,
double maxCheck,
double threshold,
EventDetector.Action action)
angle - AOL value triggering the event.type - type of AOL to detect, one of TRUE, MEAN and ECCENTRIC.equator - equator with respect to which the AOL is to be computedmaxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at AOL detectionpublic AOLDetector(double angle,
PositionAngle type,
Frame equator,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
angle - AOL value triggering the event.type - type of AOL to detect, one of TRUE, MEAN and ECCENTRIC.equator - equator with respect to which the AOL is to be computedmaxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at AOL detectionremove - true if detector should be removedpublic boolean shouldBeRemoved()
AbstractDetectorEventDetector.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 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 times increases around eventforward - if true, the integration variable (time) increases during integration.PatriusException - if some specific error occurspublic 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 getAOL()
public PositionAngle getAOLType()
public Frame getAOLFrame()
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