public class ExtremaLongitudeDetector extends AbstractDetector
MIN
,
MAX
and MIN_MAX
for both.
The default implementation behaviour is to stop
propagation when the
minimum/maximum longitude is reached. This can be changed by using provided constructors.
EventDetector
,
Serialized FormAbstractDetector.PropagationDelayType
EventDetector.Action
Modifier and Type | Field and Description |
---|---|
static int |
MAX
Flag for local maximum longitude detection (g decreasing).
|
static int |
MIN
Flag for local minimum longitude detection (g increasing).
|
static int |
MIN_MAX
Flag for both local minimum and maximum distance detection.
|
DEFAULT_MAXCHECK, DEFAULT_THRESHOLD
DECREASING, INCREASING, INCREASING_DECREASING
Constructor and Description |
---|
ExtremaLongitudeDetector(int extremumType,
Frame bodyFrame)
Constructor for a ExtremaLongitudeDetector instance.
|
ExtremaLongitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold)
Constructor for a ExtremaLongitudeDetector instance.
|
ExtremaLongitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for a ExtremaLongitudeDetector instance.
|
ExtremaLongitudeDetector(int extremumType,
Frame bodyFrame,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for a ExtremaLongitudeDetector 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 distance 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, setPropagationDelayType
public static final int MIN
public static final int MAX
public static final int MIN_MAX
public ExtremaLongitudeDetector(int extremumType, Frame bodyFrame)
public ExtremaLongitudeDetector(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 longitude detection,
MAX
for maximal longitude detection or
MIN_MAX
for both minimal and maximal longitude
detectionbodyFrame
- the body attached frame (in witch the longitude is defined)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)public ExtremaLongitudeDetector(int extremumType, Frame bodyFrame, double maxCheck, double threshold, EventDetector.Action action)
extremumType
- MIN
for minimal longitude detection,
MAX
for maximal longitude detection or
MIN_MAX
for both minimal and maximal longitude
detectionbodyFrame
- the body attached frame (in witch the longitude is defined)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at extrema longitude detectionpublic ExtremaLongitudeDetector(int extremumType, Frame bodyFrame, double maxCheck, double threshold, EventDetector.Action action, boolean remove)
extremumType
- MIN
for minimal longitude detection,
MAX
for maximal longitude detection or
MIN_MAX
for both minimal and maximal longitude
detectionbodyFrame
- the body attached frame (in witch the longitude is defined)maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at extrema longitude detectionremove
- true if detector should be removed at extrema longitude detectionpublic 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 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 EventDetector
shouldBeRemoved
in class AbstractDetector
public 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 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 Frame getBodyFrame()
public EventDetector copy()
The following attributes are not deeply copied:
Frame
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