public class AnomalyDetector extends AbstractDetector
The default implementation behaviour is to stop
propagation when the anomaly
θ is reached. This can be changed by using provided constructors.
EventDetector
,
Serialized FormAbstractDetector.PropagationDelayType
EventDetector.Action
actionAtEntry, actionAtExit, DEFAULT_MAXCHECK, DEFAULT_THRESHOLD, removeAtEntry, removeAtExit, shouldBeRemovedFlag
DECREASING, INCREASING, INCREASING_DECREASING
Constructor and Description |
---|
AnomalyDetector(PositionAngle angleType,
double angle)
Constructor for an AnomalyDetector instance.
|
AnomalyDetector(PositionAngle angleType,
double angle,
double maxCheck,
double threshold)
Constructor for an AnomalyDetector instance with complementary parameters.
|
AnomalyDetector(PositionAngle angleType,
double angle,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for an AnomalyDetector instance with complementary parameters.
|
AnomalyDetector(PositionAngle angleType,
double angle,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for an AnomalyDetector instance with complementary parameters.
|
Modifier and Type | Method and Description |
---|---|
EventDetector |
copy()
A copy of the detector.
|
EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handle an anomaly event and choose what to do next.
|
double |
g(SpacecraftState state)
Compute the value of the switching function.
|
EventDetector.Action |
getAction()
Return the action at detection.
|
double |
getAnomaly()
Get the anomaly to detect.
|
PositionAngle |
getAnomalyType()
Get the type of anomaly to detect.
|
void |
init(SpacecraftState s0,
AbsoluteDate t)
Initialize event handler at the start of a propagation.
|
getActionAtEntry, getActionAtExit, getInertialFrame, getMaxCheckInterval, getMaxIterationCount, getPropagationDelayType, getSignalEmissionDate, getSignalReceptionDate, getSlopeSelection, getThreshold, isRemoveAtEntry, isRemoveAtExit, logEventsOverTimeInterval, resetState, setEpsilonSignalPropagation, setMaxCheckInterval, setMaxIterSignalPropagation, setPropagationDelayType, shouldBeRemoved
public AnomalyDetector(PositionAngle angleType, double angle)
angleType
- true, eccentric or mean anomaly.angle
- anomaly value triggering the event.public AnomalyDetector(PositionAngle angleType, double angle, double maxCheck, double threshold)
The default implementation behaviour is to stop
propagation when the anomaly is
reached.
angleType
- true, eccentric or mean anomaly.angle
- anomaly value triggering the event.maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)public AnomalyDetector(PositionAngle angleType, double angle, double maxCheck, double threshold, EventDetector.Action action)
angleType
- true, eccentric or mean anomaly.angle
- anomaly value triggering the event.maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at anomaly detectionpublic AnomalyDetector(PositionAngle angleType, double angle, double maxCheck, double threshold, EventDetector.Action action, boolean remove)
angleType
- true, eccentric or mean anomaly.angle
- anomaly value triggering the event.maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at anomaly detectionremove
- if detector should be removedpublic EventDetector.Action eventOccurred(SpacecraftState s, boolean increasing, boolean forward) throws PatriusException
eventOccurred
in interface EventDetector
eventOccurred
in class AbstractDetector
s
- 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 state) throws PatriusException
g
in interface EventDetector
g
in class AbstractDetector
state
- 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 EventDetector
init
in class AbstractDetector
s0
- initial statet
- target time for the integrationpublic double getAnomaly()
public PositionAngle getAnomalyType()
public EventDetector.Action getAction()
public EventDetector copy()
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