public class AOLDetector extends AbstractDetector
The default implementation behaviour is to EventDetector.Action#STOP stop propagation when the angle θ
is reached. This can be changed by using provided constructors.
EventDetector,
Serialized FormEventDetector.ActionactionAtEntry, actionAtExit, DEFAULT_MAXCHECK, DEFAULT_MAXITER, DEFAULT_THRESHOLD, removeAtEntry, removeAtExit, shouldBeRemovedFlagDECREASING, 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 |
copy()
A copy of the detector.
|
EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handle an AOL 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 |
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.
|
filterEvent, getActionAtEntry, getActionAtExit, getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, isRemoveAtEntry, isRemoveAtExit, logEventsOverTimeInterval, resetState, setMaxCheckInterval, setMaxIter, shouldBeRemovedpublic 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 EventDetector.Action#STOP 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 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 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 getAOL()
public PositionAngle getAOLType()
public Frame getAOLFrame()
public EventDetector.Action getAction()
public EventDetector copy()
The following attributes are not deeply copied:
FrameCopyright © 2025 CNES. All rights reserved.