public class NadirSolarIncidenceDetector extends AbstractDetector
The solar incidence is the angle between the nadir-satellite vector and the nadir-sun vector.
This detector does not discriminate among increasing g events and decreasing g events: every
detected event is a solar incidence crossing event.
The default implementation is to stop
propagation when the
reference solar incidence is reached. This can be changed by using provided constructors.
EventDetector
,
Serialized FormEventDetector.Action
DEFAULT_MAXCHECK, DEFAULT_THRESHOLD
DECREASING, INCREASING, INCREASING_DECREASING
Constructor and Description |
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NadirSolarIncidenceDetector(double incidence,
BodyShape earth,
double maxCheck,
double threshold)
Constructor for the nadir point solar incidence detector
|
NadirSolarIncidenceDetector(double incidence,
BodyShape earth,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for the nadir point solar incidence detector
|
NadirSolarIncidenceDetector(double incidence,
BodyShape earth,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for the nadir point solar incidence 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 solar incidence event and choose what to do next.
|
double |
g(SpacecraftState s)
Compute the value of the switching function.
|
BodyShape |
getEarthShape()
Returns Earth shape.
|
double |
getIncidence()
Returns incidence.
|
PVCoordinatesProvider |
getSun()
Returns Sun.
|
void |
init(SpacecraftState s0,
AbsoluteDate t)
Initialize event handler at the start of a propagation.
|
void |
setSun(PVCoordinatesProvider sun)
Sets the sun
PVCoordinatesProvider |
boolean |
shouldBeRemoved()
This method is called after
EventDetector.eventOccurred(fr.cnes.sirius.patrius.propagation.SpacecraftState, boolean, boolean) has been triggered. |
getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, resetState
public NadirSolarIncidenceDetector(double incidence, BodyShape earth, double maxCheck, double threshold) throws PatriusException
The default implementation behavior is to stop
propagation
when the local time is reached.
incidence
- the incidence to detect (set 0. to detect the terminator)earth
- the earth shapemaxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)PatriusException
- error when loading the ephemeris filespublic NadirSolarIncidenceDetector(double incidence, BodyShape earth, double maxCheck, double threshold, EventDetector.Action action) throws PatriusException
incidence
- the incidence to detect (set 0. to detect the terminator)earth
- the earth shapemaxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at nadir point solar incidence detectionPatriusException
- error when loading the ephemeris filespublic NadirSolarIncidenceDetector(double incidence, BodyShape earth, double maxCheck, double threshold, EventDetector.Action action, boolean remove) throws PatriusException
incidence
- the incidence to detect (set 0. to detect the terminator)earth
- the earth shapemaxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at nadir point solar incidence detectionremove
- true if detector should be removed at nadir point solar incidence detectionPatriusException
- error when loading the ephemeris filespublic 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 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 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 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 void setSun(PVCoordinatesProvider sun)
PVCoordinatesProvider
sun
- the sunpublic PVCoordinatesProvider getSun()
public BodyShape getEarthShape()
public double getIncidence()
public EventDetector copy()
The following attributes are not deeply copied:
PVCoordinatesProvider
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