public class ExtremaLatitudeDetector extends AbstractDetector
MIN,
MAX and MIN_MAX for both.
The default implementation behaviour is to stop propagation when the
minimum/maximum latitude is reached. This can be changed by using provided constructors.
EventDetector,
Serialized FormAbstractDetector.PropagationDelayTypeEventDetector.Action| Modifier and Type | Field and Description |
|---|---|
static int |
MAX
Flag for local maximum latitude detection (g decreasing).
|
static int |
MIN
Flag for local minimum latitude detection (g increasing).
|
static int |
MIN_MAX
Flag for both local minimum and maximum distance detection.
|
DEFAULT_MAXCHECK, DEFAULT_THRESHOLDDECREASING, INCREASING, INCREASING_DECREASING| Constructor and Description |
|---|
ExtremaLatitudeDetector(int extremumType,
Frame bodyFrame)
Constructor for a ExtremaLatitudeDetector instance.
|
ExtremaLatitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold)
Constructor for a ExtremaLatitudeDetector instance.
|
ExtremaLatitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for a ExtremaLatitudeDetector instance.
|
ExtremaLatitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for a ExtremaLatitudeDetector instance.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector |
copy()
A copy of the detector.
|
EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handle an extrema latitude event and choose what to do next.
|
double |
g(SpacecraftState s)
Compute the value of the switching function.
|
Frame |
getBodyFrame()
Returns the body frame.
|
void |
init(SpacecraftState s0,
AbsoluteDate t)
Initialize event handler at the start of a propagation.
|
boolean |
shouldBeRemoved()
This method is called after
EventDetector.eventOccurred(fr.cnes.sirius.patrius.propagation.SpacecraftState, boolean, boolean) has been triggered. |
getMaxCheckInterval, getMaxIterationCount, getPropagationDelayType, getSignalEmissionDate, getSignalReceptionDate, getSlopeSelection, getThreshold, resetState, setPropagationDelayTypepublic static final int MIN
public static final int MAX
public static final int MIN_MAX
public ExtremaLatitudeDetector(int extremumType,
Frame bodyFrame)
public ExtremaLatitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold)
The default implementation behavior is to stop propagation when the expected
extremum is reached.
extremumType - MIN for minimal latitude detection,
MAX for maximal latitude detection or
MIN_MAX for both minimal and maximal latitude
detectionbodyFrame - the body attached frame (in witch the latitude is defined)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)public ExtremaLatitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold,
EventDetector.Action action)
extremumType - MIN for minimal latitude detection,
MAX for maximal latitude detection or
MIN_MAX for both minimal and maximal latitude
detectionbodyFrame - the body attached frame (in witch the latitude is defined)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at extrema latitude detectionpublic ExtremaLatitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
extremumType - MIN for minimal latitude detection,
MAX for maximal latitude detection or
MIN_MAX for both minimal and maximal latitude
detectionbodyFrame - the body attached frame (in witch the latitude is defined)maxCheck - maximum check (see AbstractDetector)threshold - threshold (see AbstractDetector)action - action performed at extrema latitude detectionremove - true if detector should be removed at extrema latitude detectionpublic EventDetector.Action eventOccurred(SpacecraftState s, boolean increasing, boolean forward) throws PatriusException
eventOccurred in interface EventDetectoreventOccurred in class AbstractDetectors - the current state information : date, kinematics, attitudeincreasing - if true, the value of the switching function increases when times 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 EventDetectorshouldBeRemoved in class AbstractDetectorpublic double g(SpacecraftState s) throws PatriusException
g in interface EventDetectorg in class AbstractDetectors - 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 EventDetectorinit in class AbstractDetectors0 - initial statet - target time for the integrationpublic Frame getBodyFrame()
public EventDetector copy()
The following attributes are not deeply copied:
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