Class PositionAngleDetector
- java.lang.Object
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- org.orekit.propagation.events.AbstractDetector<PositionAngleDetector>
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- org.orekit.propagation.events.PositionAngleDetector
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- All Implemented Interfaces:
EventDetector
public class PositionAngleDetector extends AbstractDetector<PositionAngleDetector>
Detector for in-orbit position angle.The detector is based on anomaly for
Keplerianorbits, latitude argument forcircularorbits, or longitude argument forequinoctialorbits. It does not supportCartesianorbits. The angles can be eithertrue,meanoreccentricangles.- Since:
- 7.1
- Author:
- Luc Maisonobe
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Field Summary
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Fields inherited from class org.orekit.propagation.events.AbstractDetector
DEFAULT_MAX_CHECK, DEFAULT_MAX_ITER, DEFAULT_THRESHOLD
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Constructor Summary
Constructors Modifier Constructor Description PositionAngleDetector(double maxCheck, double threshold, OrbitType orbitType, PositionAngleType positionAngleType, double angle)Build a detector.PositionAngleDetector(OrbitType orbitType, PositionAngleType positionAngleType, double angle)Build a new detector.protectedPositionAngleDetector(EventDetectionSettings detectionSettings, EventHandler handler, OrbitType orbitType, PositionAngleType positionAngleType, double angle)Protected constructor with full parameters.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description protected PositionAngleDetectorcreate(EventDetectionSettings detectionSettings, EventHandler newHandler)Build a new instance.doubleg(SpacecraftState s)Compute the value of the detection function.doublegetAngle()Get the fixed angle to be crossed (radians).OrbitTypegetOrbitType()Get the orbit type defining the angle type.PositionAngleTypegetPositionAngleType()Get the type of position angle.voidinit(SpacecraftState s0, AbsoluteDate t)Initialize event detector at the start of a propagation.-
Methods inherited from class org.orekit.propagation.events.AbstractDetector
checkIfForward, getDetectionSettings, getHandler, isForward, withDetectionSettings, withHandler, withMaxCheck, withMaxCheck, withMaxIter, withThreshold
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Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
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Methods inherited from interface org.orekit.propagation.events.EventDetector
dependsOnTimeOnly, finish, getMaxCheckInterval, getMaxIterationCount, getThreshold, reset
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Constructor Detail
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PositionAngleDetector
public PositionAngleDetector(OrbitType orbitType, PositionAngleType positionAngleType, double angle) throws OrekitIllegalArgumentException
Build a new detector.The new instance uses default values for maximal checking interval (
AbstractDetector.DEFAULT_MAX_CHECK) and convergence threshold (AbstractDetector.DEFAULT_THRESHOLD).- Parameters:
orbitType- orbit type defining the angle typepositionAngleType- type of position angleangle- fixed angle to be crossed- Throws:
OrekitIllegalArgumentException- if orbit type isOrbitType.CARTESIAN
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PositionAngleDetector
public PositionAngleDetector(double maxCheck, double threshold, OrbitType orbitType, PositionAngleType positionAngleType, double angle) throws OrekitIllegalArgumentExceptionBuild a detector.This instance uses by default the
StopOnEventhandler- Parameters:
maxCheck- maximal checking interval (s)threshold- convergence threshold (s)orbitType- orbit type defining the angle typepositionAngleType- type of position angleangle- fixed angle to be crossed- Throws:
OrekitIllegalArgumentException- if orbit type isOrbitType.CARTESIAN
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PositionAngleDetector
protected PositionAngleDetector(EventDetectionSettings detectionSettings, EventHandler handler, OrbitType orbitType, PositionAngleType positionAngleType, double angle) throws OrekitIllegalArgumentException
Protected constructor with full parameters.This constructor is not public as users are expected to use the builder API with the various
withXxx()methods to set up the instance in a readable manner without using a huge amount of parameters.- Parameters:
detectionSettings- event detection settingshandler- event handler to call at event occurrencesorbitType- orbit type defining the angle typepositionAngleType- type of position angleangle- fixed angle to be crossed- Throws:
OrekitIllegalArgumentException- if orbit type isOrbitType.CARTESIAN- Since:
- 13.0
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Method Detail
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create
protected PositionAngleDetector create(EventDetectionSettings detectionSettings, EventHandler newHandler)
Build a new instance.- Specified by:
createin classAbstractDetector<PositionAngleDetector>- Parameters:
detectionSettings- detection settingsnewHandler- event handler to call at event occurrences- Returns:
- a new instance of the appropriate sub-type
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getOrbitType
public OrbitType getOrbitType()
Get the orbit type defining the angle type.- Returns:
- orbit type defining the angle type
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getPositionAngleType
public PositionAngleType getPositionAngleType()
Get the type of position angle.- Returns:
- type of position angle
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getAngle
public double getAngle()
Get the fixed angle to be crossed (radians).- Returns:
- fixed angle to be crossed (radians)
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init
public void init(SpacecraftState s0, AbsoluteDate t)
Initialize event detector at the start of a propagation.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.
The default implementation initializes the handler.
This implementation sets the direction of propagation and initializes the event handler. If a subclass overrides this method it should call
super.init(s0, t).- Specified by:
initin interfaceEventDetector- Overrides:
initin classAbstractDetector<PositionAngleDetector>- Parameters:
s0- initial statet- target time for the integration
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g
public double g(SpacecraftState s)
Compute the value of the detection function.The value is the angle difference between the spacecraft and the fixed angle to be crossed, with some sign tweaks to ensure continuity. These tweaks imply the
increasingflag in events detection becomes irrelevant here! As an example, the angle always increase in a Keplerian orbit, but this g function will increase and decrease so it will cross the zero value once per orbit, in increasing and decreasing directions on alternate orbits..- Parameters:
s- the current state information: date, kinematics, attitude- Returns:
- angle difference between the spacecraft and the fixed angle, with some sign tweaks to ensure continuity
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