public class SolarTimeAngleDetector extends AbstractDetector
The default implementation is to stop
propagation when the solar time is reached.
This can be changed by using provided constructors.
This detector can takes into account signal propagation duration through
AbstractDetector.setPropagationDelayType(PropagationDelayType)
(default is signal being instantaneous).
EventDetector
,
Serialized FormAbstractDetector.PropagationDelayType
EventDetector.Action
DEFAULT_MAXCHECK, DEFAULT_THRESHOLD
DECREASING, INCREASING, INCREASING_DECREASING
Constructor and Description |
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SolarTimeAngleDetector(double solarTimeAngle)
Constructor for a SolarTimeDetector instance.
|
SolarTimeAngleDetector(double solarTimeAngle,
CelestialBody sunModel,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for a SolarTimeDetector instance with complimentary parameters.
|
SolarTimeAngleDetector(double solarTimeAngle,
double maxCheck,
double threshold)
Constructor for a SolarTimeDetector instance with complimentary parameters.
|
SolarTimeAngleDetector(double solarTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action)
Constructor for a SolarTimeDetector instance with complimentary parameters.
|
SolarTimeAngleDetector(double solarTimeAngle,
double maxCheck,
double threshold,
EventDetector.Action action,
boolean remove)
Constructor for a SolarTimeDetector instance with complimentary parameters.
|
Modifier and Type | Method and Description |
---|---|
EventDetector |
copy()
A copy of the detector.
|
EventDetector.Action |
eventOccurred(SpacecraftState s,
boolean increasing,
boolean forward)
Handle a solar time angle event and choose what to do next.
|
double |
g(SpacecraftState s)
Compute the value of the switching function.
|
double |
getTime()
Get solar time angle to detect.
|
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 SolarTimeAngleDetector(double solarTimeAngle) throws PatriusException
solarTimeAngle
- satellite solar time angle triggering the event (in the range [-Π,
Π[). Angle between the projection of the Sun in the osculator orbital plane and the
satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).PatriusException
- error when loading the ephemeris files or solar time angle not in
the range [-Π, Π[public SolarTimeAngleDetector(double solarTimeAngle, double maxCheck, double threshold) throws PatriusException
solarTimeAngle
- satellite solar time angle triggering the event (in the range [-Π,
Π[). Angle between the projection of the Sun in the osculator orbital plane and the
satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)PatriusException
- error when loading the ephemeris files or solar time angle not in
the range [-Π, Π[public SolarTimeAngleDetector(double solarTimeAngle, double maxCheck, double threshold, EventDetector.Action action) throws PatriusException
solarTimeAngle
- satellite solar time angle triggering the event (in the range [-Π,
Π[). Angle between the projection of the Sun in the osculator orbital plane and the
satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at solar time detectionPatriusException
- error when loading the ephemeris files or solar time angle not in
the range [-Π, Π[public SolarTimeAngleDetector(double solarTimeAngle, double maxCheck, double threshold, EventDetector.Action action, boolean remove) throws PatriusException
solarTimeAngle
- satellite solar time angle triggering the event (in the range [-Π,
Π[). Angle between the projection of the Sun in the osculator orbital plane and the
satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).maxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at solar time detectionremove
- true if detector should be removedPatriusException
- error when loading the ephemeris files or solar time angle not in
the range [-Π, Π[public SolarTimeAngleDetector(double solarTimeAngle, CelestialBody sunModel, double maxCheck, double threshold, EventDetector.Action action, boolean remove) throws PatriusException
solarTimeAngle
- satellite solar time angle triggering the event (in the range [-Π,
Π[). Angle between the projection of the Sun in the osculator orbital plane and the
satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).sunModel
- Sun modelmaxCheck
- maximum check (see AbstractDetector
)threshold
- threshold (see AbstractDetector
)action
- action performed at solar time detectionremove
- true if detector should be removedPatriusException
- error when loading the ephemeris files or solar time angle not in
the range [-Π, Π[public EventDetector.Action eventOccurred(SpacecraftState s, boolean increasing, boolean forward) throws PatriusException
The default implementation behavior is to stop
propagation when the solar time
is reached.
eventOccurred
in interface EventDetector
eventOccurred
in class AbstractDetector
s
- the current state information : date, kinematics, attitude.increasing
- if true, the value of the switching function increases when time increases
around event.forward
- 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 double getTime()
public EventDetector copy()
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