public class LocalTimeAngleDetector extends AbstractSignalPropagationDetector
The default implementation is to stop
propagation when the local time 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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LocalTimeAngleDetector(double localTimeAngle)
Constructor for a LocalTimeDetector instance.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold)
Constructor for a LocalTimeDetector instance with complimentary parameters.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame)
Constructor for a LocalTimeDetector instance with complimentary parameters.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action)
Constructor for a LocalTimeDetector instance with complimentary parameters.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove)
Constructor for a LocalTimeDetector instance with complimentary parameters.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove,
CelestialPoint sun)
Constructor for a LocalTimeDetector instance with complimentary parameters including Sun choice.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
CelestialBodyFrame frame,
EventDetector.Action action,
boolean remove,
CelestialPoint sun,
int slopeSelection)
Constructor for a LocalTimeDetector instance with complimentary parameters including Sun choice.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for a LocalTimeDetector instance with complimentary parameters.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for a LocalTimeDetector instance with complimentary parameters.
|
LocalTimeAngleDetector(double localTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove,
CelestialPoint sun)
Constructor for a LocalTimeDetector 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)
Handle a local time angle event and choose what to do next.
|
boolean |
filterEvent(SpacecraftState state,
boolean increasing,
boolean forward)
Filter last event: returns true if the last event is a false detection, false otherwise.
|
double |
g(SpacecraftState state)
Compute the value of the switching function.
|
EventDetector.Action |
getAction()
Return the action at detection.
|
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.
|
CelestialBodyFrame |
getFrame()
Returns the frame used for solar time computation.
|
PVCoordinatesProvider |
getReceiver(SpacecraftState s)
Getter for the signal receiver.
|
double |
getTime()
Get local time angle to detect.
|
void |
init(SpacecraftState s0,
AbsoluteDate t)
Initialize event handler at the start of a propagation.
|
void |
setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType,
Frame frameIn)
Setter for the propagation delay computation type.
|
getEpsilonSignalPropagation, getInertialFrame, getMaxIterSignalPropagation, getPropagationDelayType, getSignalEmissionDate, getSignalEmissionDate, getSignalReceptionDate, getSignalReceptionDate, setEpsilonSignalPropagation, setMaxIterSignalPropagation
getActionAtEntry, getActionAtExit, getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, isRemoveAtEntry, isRemoveAtExit, logEventsOverTimeInterval, resetState, setMaxCheckInterval, setMaxIter, shouldBeRemoved
public LocalTimeAngleDetector(double localTimeAngle) throws PatriusException
Local time will be computed in satellite orbit frame.
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)PatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold) throws PatriusException
The default implementation behavior is to stop
propagation when the local time
is reached.
Local time will be computed in satellite orbit frame.
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)PatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold, CelestialBodyFrame frame) throws PatriusException
The default implementation behavior is to stop
propagation when the local time
is reached.
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)frame
- in relation to which the calculations are madePatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold, EventDetector.Action action) throws PatriusException
Local time will be computed in satellite orbit frame.
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at local time detectionPatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold, CelestialBodyFrame frame, EventDetector.Action action) throws PatriusException
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at local time detectionframe
- in relation to which the calculations are madePatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold, EventDetector.Action action, boolean remove) throws PatriusException
Local time will be computed in satellite orbit frame.
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at local time detectionremove
- true if detector should be removedPatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold, CelestialBodyFrame frame, EventDetector.Action action, boolean remove) throws PatriusException
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at local time detectionremove
- true if detector should be removedframe
- in relation to which the calculations are madePatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold, EventDetector.Action action, boolean remove, CelestialPoint sun) throws PatriusException
Local time will be computed in satellite orbit frame.
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at local time detectionremove
- true if detector should be removedsun
- SunPatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[public LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold, CelestialBodyFrame frame, EventDetector.Action action, boolean remove, CelestialPoint sun) throws PatriusException
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at local time detectionremove
- true if detector should be removedsun
- Sunframe
- in relation to which the calculations are madePatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic LocalTimeAngleDetector(double localTimeAngle, double maxCheck, double threshold, CelestialBodyFrame frame, EventDetector.Action action, boolean remove, CelestialPoint sun, int slopeSelection) throws PatriusException
localTimeAngle
- satellite local time angle triggering the event (in the range [-Π,
Π[). Angle between the projections of the Sun and the satellite in the equatorial
plane (Local Time In Hours = 12.00h + localTimeAngle * 12 / Π)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at local time detectionremove
- true if detector should be removedsun
- Sunframe
- in relation to which the calculations are madeslopeSelection
- NodeDetector.ASCENDING
for ascending node detection,NodeDetector.DESCENDING
for descending node detection,NodeDetector.ASCENDING_DESCENDING
for both ascending and descending node
detection.PatriusException
- error when loading the ephemeris files or local time angle not in
the range [-Π, Π[ or frame not null and not inertialpublic 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 time 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 boolean filterEvent(SpacecraftState state, boolean increasing, boolean forward) throws PatriusException
This method is called right before EventDetector.eventOccurred(SpacecraftState, boolean, boolean)
method.
This may be useful in order to filter some events in particular when angles are at stake (see for example
LocalTimeAngleDetector
).
filterEvent
in interface EventDetector
filterEvent
in class AbstractDetector
state
- state at last event occurrenceincreasing
- if true, the value of the switching function increases when times increases
around event (note that increase is measured with respect to physical time, not with
respect to propagation which may go backward in time)forward
- if true, the integration variable (time) increases during integration.PatriusException
- thrown if computation failed for some reasonspublic double getTime()
public EventDetector.Action getAction()
public CelestialBodyFrame getFrame()
public void setPropagationDelayType(AbstractSignalPropagationDetector.PropagationDelayType propagationDelayType, Frame frameIn)
AbstractSignalPropagationDetector
setPropagationDelayType
in class AbstractSignalPropagationDetector
propagationDelayType
- Propagation delay type used in events computationframeIn
- 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()
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