public class BetaAngleDetector extends AbstractSignalPropagationDetector
The default implementation behaviour is to stop
propagation when the beta angle is
reached. This can be changed by using provided constructors.
This detector can takes into account signal propagation duration through
AbstractSignalPropagationDetector.setPropagationDelayType(PropagationDelayType, Frame)
(default is signal being instantaneous).
EventDetector
,
Serialized FormAbstractSignalPropagationDetector.DatationChoice, AbstractSignalPropagationDetector.PropagationDelayType
EventDetector.Action
actionAtEntry, actionAtExit, DEFAULT_MAXCHECK, DEFAULT_MAXITER, DEFAULT_THRESHOLD, removeAtEntry, removeAtExit, shouldBeRemovedFlag
DECREASING, INCREASING, INCREASING_DECREASING
Constructor and Description |
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BetaAngleDetector(double ang)
Constructor for a BetaAngleDetector instance.
|
BetaAngleDetector(double ang,
double maxCheck,
double threshold)
Constructor for a BetaAngleDetector instance with complimentary parameters.
|
BetaAngleDetector(double ang,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for a BetaAngleDetector instance with complimentary parameters.
|
BetaAngleDetector(double ang,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for a BetaAngleDetector instance with complimentary parameters.
|
BetaAngleDetector(double ang,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove,
CelestialPoint sun)
Constructor for a BetaAngleDetector instance with complimentary parameters including Sun choice.
|
Modifier and Type | Method and Description |
---|---|
EventDetector |
copy()
A copy of the detector.
|
EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handles a beta angle event and chooses what to do next.
|
double |
g(SpacecraftState state)
Compute the value of the switching function.
|
double |
getAngle()
Returns beta angle triggering the event.
|
AbstractSignalPropagationDetector.DatationChoice |
getDatationChoice()
Specify if the datation choice corresponds to the emitter date or the receiver date.
|
PVCoordinatesProvider |
getEmitter(SpacecraftState s)
Getter for the signal emitter.
|
PVCoordinatesProvider |
getReceiver(SpacecraftState s)
Getter for the signal receiver.
|
void |
init(SpacecraftState s0,
AbsoluteDate t)
Initialize event handler at the start of a propagation.
|
void |
setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType,
Frame frame)
Setter for the propagation delay computation type.
|
getEpsilonSignalPropagation, getInertialFrame, getMaxIterSignalPropagation, getPropagationDelayType, getSignalEmissionDate, getSignalEmissionDate, getSignalReceptionDate, getSignalReceptionDate, setEpsilonSignalPropagation, setMaxIterSignalPropagation
filterEvent, getActionAtEntry, getActionAtExit, getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, isRemoveAtEntry, isRemoveAtExit, logEventsOverTimeInterval, resetState, setMaxCheckInterval, setMaxIter, shouldBeRemoved
public BetaAngleDetector(double ang) throws PatriusException
ang
- angle in radians triggering the event.PatriusException
- thrown if Sun could not be retrievedpublic BetaAngleDetector(double ang, double maxCheck, double threshold) throws PatriusException
The default implementation behavior is to stop
propagation when the angle is
reached.
ang
- angle in radians triggering the event.maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)PatriusException
- thrown if Sun could not be retrievedIllegalArgumentException
- if angle is out of range [-Pi / 2 , Pi / 2]public BetaAngleDetector(double ang, double maxCheck, double threshold, EventDetector.Action action) throws PatriusException
ang
- angle in radians triggering the event.maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at beta angle detectionPatriusException
- thrown if Sun could not be retrievedIllegalArgumentException
- if angle is out of range [-Pi / 2 , Pi / 2]public BetaAngleDetector(double ang, double maxCheck, double threshold, EventDetector.Action action, boolean remove) throws PatriusException
ang
- angle in radians triggering the event.maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at beta angle detectionremove
- if the detector should be removedPatriusException
- thrown if Sun could not be retrievedIllegalArgumentException
- if angle is out of range [-Pi / 2 , Pi / 2]public BetaAngleDetector(double ang, double maxCheck, double threshold, EventDetector.Action action, boolean remove, CelestialPoint sun)
ang
- angle in radians triggering the event.maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at beta angle detectionremove
- if the detector should be removedsun
- sunIllegalArgumentException
- if angle is out of range [-Pi / 2 , Pi / 2]public 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, attitude.increasing
- if true, the value of the switching function increases when time increases
around event.forward
- 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 getAngle()
public void setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frame)
AbstractSignalPropagationDetector
setPropagationDelayType
in class AbstractSignalPropagationDetector
propagationDelayType
- Propagation delay type used in events computationframe
- Frame to use for signal propagation with delay (may be null if propagation delay type is
considered instantaneous). Warning: the usage of a pseudo inertial frame is tolerated, however it will
lead to some inaccuracies due to the non-invariance of the frame with respect to time. For this reason,
it is suggested to use the ICRF frame or a frame which is frozen with respect to the ICRF.public PVCoordinatesProvider getEmitter(SpacecraftState s)
getEmitter
in class AbstractSignalPropagationDetector
s
- the spacecraft state used by the detectorpublic PVCoordinatesProvider getReceiver(SpacecraftState s)
getReceiver
in class AbstractSignalPropagationDetector
s
- the spacecraft state used by the detectorpublic AbstractSignalPropagationDetector.DatationChoice getDatationChoice()
getDatationChoice
in class AbstractSignalPropagationDetector
public EventDetector copy()
The following attributes are not deeply copied:
CelestialPoint
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