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java.lang.Objectorg.orekit.propagation.events.AbstractDetector
org.orekit.propagation.events.NadirSolarIncidenceDetector
public class NadirSolarIncidenceDetector
Spacecraft's nadir point solar incidence detector.
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 Form| Nested Class Summary |
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| Nested classes/interfaces inherited from interface org.orekit.propagation.events.EventDetector |
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EventDetector.Action |
| Field Summary |
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| Fields inherited from class org.orekit.propagation.events.AbstractDetector |
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DEFAULT_MAXCHECK, DEFAULT_THRESHOLD |
| Fields inherited from interface org.orekit.propagation.events.EventDetector |
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DECREASING, INCREASING, INCREASING_DECREASING |
| Constructor Summary | |
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NadirSolarIncidenceDetector(double incidence,
BodyShape earth,
double maxCheck,
double threshold)
Constructor for the nadir point solar incidence detector |
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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 |
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| Method Summary | |
|---|---|
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(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered. |
| Methods inherited from class org.orekit.propagation.events.AbstractDetector |
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getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, resetState |
| Methods inherited from class java.lang.Object |
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clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait |
| Constructor Detail |
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public NadirSolarIncidenceDetector(double incidence,
BodyShape earth,
double maxCheck,
double threshold)
throws OrekitException
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)
OrekitException - error when loading the ephemeris files
public NadirSolarIncidenceDetector(double incidence,
BodyShape earth,
double maxCheck,
double threshold,
EventDetector.Action action)
throws OrekitException
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 detection
OrekitException - error when loading the ephemeris files
public NadirSolarIncidenceDetector(double incidence,
BodyShape earth,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
throws OrekitException
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 detection
OrekitException - error when loading the ephemeris files| Method Detail |
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public double g(SpacecraftState s)
throws OrekitException
AbstractDetector
g in interface EventDetectorg in class AbstractDetectors - the current state information: date, kinematics, attitude for forces
and events computation, mass provider, and additional states
OrekitException - if some specific error occurs
public EventDetector.Action eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
throws OrekitException
eventOccurred in interface EventDetectoreventOccurred in class AbstractDetectors - 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.
OrekitException - if some specific error occurspublic boolean shouldBeRemoved()
EventDetector.eventOccurred(org.orekit.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 EventDetectorshouldBeRemoved in class AbstractDetector
public void init(SpacecraftState s0,
AbsoluteDate t)
AbstractDetectorThis 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 void setSun(PVCoordinatesProvider sun)
PVCoordinatesProvider
sun - the sunpublic PVCoordinatesProvider getSun()
public BodyShape getEarthShape()
public double getIncidence()
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