public class LongitudeDetector extends AbstractDetector
The default implementation behaviour is to stop
propagation when the longitude is
reached. This can be changed by using provided constructors.
EventDetector
,
Serialized FormAbstractDetector.PropagationDelayType
EventDetector.Action
DEFAULT_MAXCHECK, DEFAULT_THRESHOLD
DECREASING, INCREASING, INCREASING_DECREASING
Constructor and Description |
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LongitudeDetector(double longitudeToDetect,
Frame bodyFrame)
Constructor for the longitude detector.
|
LongitudeDetector(double longitudeToDetect,
Frame bodyFrame,
double maxCheck,
double threshold)
Constructor for the longitude detector.
|
LongitudeDetector(double longitudeToDetect,
Frame bodyFrame,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for the longitude detector.
|
LongitudeDetector(double longitudeToDetect,
Frame bodyFrame,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for the longitude detector.
|
Modifier and Type | Method and Description |
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EventDetector |
copy()
A copy of the detector.
|
EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handle a longitude reaching event and choose what to do next.
|
double |
g(SpacecraftState s)
Compute the value of the switching function.
|
Frame |
getBodyFrame()
Returns central body frame.
|
double |
getLongitudeToDetect()
Returns longitude 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, getPropagationDelayType, getSignalEmissionDate, getSignalReceptionDate, getSlopeSelection, getThreshold, resetState, setPropagationDelayType
public LongitudeDetector(double longitudeToDetect, Frame bodyFrame)
The default implementation behavior is to stop
propagation when the expected
longitude is reached.
longitudeToDetect
- the longitude to detectbodyFrame
- the frame of the central body (take care to use a rotative frame to get the
right longitude)public LongitudeDetector(double longitudeToDetect, Frame bodyFrame, double maxCheck, double threshold)
The default implementation behavior is to stop
propagation when the expected
longitude is reached.
longitudeToDetect
- the longitude to detectbodyFrame
- the frame of the central body (take care to use a rotative frame to get the
right longitude)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)public LongitudeDetector(double longitudeToDetect, Frame bodyFrame, double maxCheck, double threshold, EventDetector.Action action)
The default implementation behavior is to stop
propagation when the expected
longitude is reached.
longitudeToDetect
- the longitude to detectbodyFrame
- the frame of the central body (take care to use a rotative frame to get the
right longitude)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at longitude detectionpublic LongitudeDetector(double longitudeToDetect, Frame bodyFrame, double maxCheck, double threshold, EventDetector.Action action, boolean remove)
The default implementation behavior is to stop
propagation when the expected
longitude is reached.
longitudeToDetect
- the longitude to detectbodyFrame
- the frame of the central body (take care to use a rotative frame to get the
right longitude)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at longitude detectionremove
- true if detector should be removedpublic 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 EventDetector.Action eventOccurred(SpacecraftState s, boolean increasing, boolean forward) throws PatriusException
The default implementation behavior is to stop
propagation when the expected
longitude is reached.
eventOccurred
in interface EventDetector
eventOccurred
in class AbstractDetector
s
- the current state information : date, kinematics, attitude.increasing
- 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 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 EventDetector
shouldBeRemoved
in class AbstractDetector
public double g(SpacecraftState s) throws PatriusException
g
in interface EventDetector
g
in class AbstractDetector
s
- the current state information: date, kinematics, attitude for forces and events
computation, mass provider, and additional statesPatriusException
- if some specific error occurspublic double getLongitudeToDetect()
public Frame getBodyFrame()
public EventDetector copy()
The following attributes are not deeply copied:
Frame
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