Serializable, EventDetectorpublic class PositionAngleDetector extends AbstractDetector<PositionAngleDetector>
The detector is based on anomaly for Keplerian
orbits, latitude argument for circular orbits,
or longitude argument for equinoctial orbits.
It does not support Cartesian orbits. The
angles can be either true, {link mean or eccentric angles.
DEFAULT_MAX_ITER, DEFAULT_MAXCHECK, DEFAULT_THRESHOLD| Constructor | Description |
|---|---|
PositionAngleDetector(double maxCheck,
double threshold,
OrbitType orbitType,
PositionAngle positionAngle,
double angle) |
Build a detector.
|
PositionAngleDetector(OrbitType orbitType,
PositionAngle positionAngle,
double angle) |
Build a new detector.
|
| Modifier and Type | Method | Description |
|---|---|---|
protected PositionAngleDetector |
create(double newMaxCheck,
double newThreshold,
int newMaxIter,
EventHandler<? super PositionAngleDetector> newHandler) |
Build a new instance.
|
double |
g(SpacecraftState s) |
Compute the value of the detection function.
|
double |
getAngle() |
Get the fixed angle to be crossed (radians).
|
OrbitType |
getOrbitType() |
Get the orbit type defining the angle type.
|
PositionAngle |
getPositionAngle() |
Get the type of position angle.
|
void |
init(SpacecraftState s0,
AbsoluteDate t) |
Initialize event handler at the start of a propagation.
|
eventOccurred, getHandler, getMaxCheckInterval, getMaxIterationCount, getThreshold, isForward, resetState, withHandler, withMaxCheck, withMaxIter, withThresholdpublic PositionAngleDetector(OrbitType orbitType, PositionAngle positionAngle, double angle) throws OrekitIllegalArgumentException
The new instance uses default values for maximal checking interval
(AbstractDetector.DEFAULT_MAXCHECK) and convergence threshold (AbstractDetector.DEFAULT_THRESHOLD).
orbitType - orbit type defining the angle typepositionAngle - type of position angleangle - fixed angle to be crossedOrekitIllegalArgumentException - if orbit type is OrbitType.CARTESIANpublic PositionAngleDetector(double maxCheck,
double threshold,
OrbitType orbitType,
PositionAngle positionAngle,
double angle)
throws OrekitIllegalArgumentException
maxCheck - maximal checking interval (s)threshold - convergence threshold (s)orbitType - orbit type defining the angle typepositionAngle - type of position angleangle - fixed angle to be crossedOrekitIllegalArgumentException - if orbit type is OrbitType.CARTESIANprotected PositionAngleDetector create(double newMaxCheck, double newThreshold, int newMaxIter, EventHandler<? super PositionAngleDetector> newHandler)
create in class AbstractDetector<PositionAngleDetector>newMaxCheck - maximum checking interval (s)newThreshold - convergence threshold (s)newMaxIter - maximum number of iterations in the event time searchnewHandler - event handler to call at event occurrencespublic OrbitType getOrbitType()
public PositionAngle getPositionAngle()
public double getAngle()
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.
The default implementation does nothing
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).
init in interface EventDetectorinit in class AbstractDetector<PositionAngleDetector>s0 - initial statet - target time for the integrationpublic double g(SpacecraftState s)
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 increasing flag 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..
g in interface EventDetectorg in class AbstractDetector<PositionAngleDetector>s - the current state information: date, kinematics, attitudeCopyright © 2002-2019 CS Systèmes d'information. All rights reserved.