| Modifier and Type | Method and Description |
|---|---|
void |
AttitudesSequence.addSwitchingCondition(AttitudeLaw before,
EventDetector switchEvent,
boolean switchOnIncrease,
boolean switchOnDecrease,
AttitudeLaw after)
Add a switching condition between two attitude providers.
|
| Modifier and Type | Class and Description |
|---|---|
class |
AbstractDetector
Common parts shared by several events finders.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector |
EventDetector.copy()
A copy of the detector.
|
| Modifier and Type | Class and Description |
|---|---|
class |
ExtremaGenericDetector<D extends EventDetector>
Detector for extrema of the switching value of
ExtremaGenericDetector.underlyingDetector. |
| Modifier and Type | Class and Description |
|---|---|
class |
AbstractSignalPropagationDetector
Common parts shared by several events finders related to signal propagation concept.
A default implementation of most of the methods of EventDetector Interface. Make it easier to create a new detector. |
class |
AbstractStationToSatDetector
Abstract event detector using a station elevation correction.
|
class |
AlignmentDetector
Finder for satellite/body alignment events.
|
class |
AltitudeDetector
Finder for satellite altitude crossing events.
|
class |
AngularMomentumExcessDetector
Detector triggered when the angular momentum reaches a maximal threshold
|
class |
AnomalyDetector
Detects when the anomaly of the spacecraft reaches a predetermined value, θ.
Anomaly is not defined for all kinds of orbits: this detector will detect anomaly events only if the corresponding orbit is not a circular orbit, otherwise it may trigger events randomly. |
class |
AOLDetector
Detects when the Argument of Latitude of the spacecraft reaches a predetermined value, θ.
|
class |
ApparentElevationDetector
Finder for satellite apparent elevation events.
|
class |
ApsideDetector
Finder for apside crossing events.
|
class |
BetaAngleDetector
Detects when the beta angle of the spacecraft reaches a predetermined value.
The beta angle is the angle between the orbit plane and the vector from the central body to the sun. |
class |
CenteredAolPassageDetector
Centered argument of latitude detector
|
class |
CentralBodyMaskCircularFOVDetector
Finder for target entry/exit events with respect to a satellite sensor FOV defined by a vector3D
giving the direction in satellite frame and taking into account masking from the central body
|
class |
CircularFieldOfViewDetector
Finder for target entry/exit events with respect to a satellite sensor field of view.
|
class |
CombinedPhenomenaDetector
This class finds the events resulting from the combination of two phenomena.
|
class |
DateDetector
Finder for date events.
|
class |
DihedralFieldOfViewDetector
Finder for body entering/exiting dihedral fov events.
|
class |
DistanceDetector
Detects when the distance from the spacecraft to a given body reaches a predetermined value.
|
class |
DotProductDetector
Detects when the dot product value between a spacecraft and a target PV coordinates reaches a
threshold value.
|
class |
EarthZoneDetector
Detects when the satellite enters a ground zone (several zones can be defined at the same time).
|
class |
EclipseDetector
Finder for satellite eclipse related events.
|
class |
ElevationDetector
Finder for satellite raising/setting events.
|
class |
ExtremaDistanceDetector
Detects when the distance from the spacecraft to a given body reaches either a local minimum or a
local maximum.
|
class |
ExtremaElevationDetector
Detects the time when the spacecraft reaches the elevation extrema in a given topocentric
frame.
ExtremaElevationDetector.MIN, ExtremaElevationDetector.MAX and
ExtremaElevationDetector.MIN_MAX for both. |
class |
ExtremaGenericDetector<D extends EventDetector>
Detector for extrema of the switching value of
ExtremaGenericDetector.underlyingDetector. |
class |
ExtremaLatitudeDetector
Detects when the spacecraft reaches the maximal or minimal local latitude.
|
class |
ExtremaLongitudeDetector
Detects when the spacecraft reaches the maximal or minimal local longitude.
|
class |
ExtremaSightAxisDetector
Detects the minimum angle between a sight view line and a PVCoordinateProvider target view from a
Frame which origin is on the line.
|
class |
ExtremaThreeBodiesAngleDetector
Detects the maximal or minimal angle between three bodies is reached, the spacecraft eventually
being one of the bodies.
|
class |
FlightDomainExcessDetector |
class |
GroundMaskElevationDetector
Finder for satellite azimuth-elevation events with respect to a mask.
|
class |
IntervalOccurrenceDetector
This event detector detects the occurrences "i" of an underlying event detector matching the 2 following condition:
i belong to [n, m]
i - n % p = 0
n being the first occurrence to detect, m the last occurrence to detect and p the occurrence step of detection.
|
class |
LatitudeDetector
Detects when the spacecraft reaches a given local latitude.
|
class |
LocalTimeAngleDetector
Detects when the local time angle of a spacecraft is equal to a predetermined value.
The local time is represented by the angle between the projections of the Sun and the satellite in the equatorial plane; therefore this angle is equal to zero when the local time is 12.00h and Π when the local time is 0.00h (Local Time In Hours = 12.00h + local time angle * 12 / Π). |
class |
LongitudeDetector
Detects when the spacecraft reaches a given local longitude.
|
class |
MaskingDetector
Sensor masking detector.
|
class |
NadirSolarIncidenceDetector
Spacecraft's nadir point solar incidence detector.
|
class |
NodeDetector
Finder for node crossing events.
|
class |
NthOccurrenceDetector
This event detector detects the nth occurrence of an underlying event detector.
|
class |
NullMassDetector
This class creates an event detector that detects when the global mass of the satellite becomes
null.
|
class |
NullMassPartDetector
This class creates an event detector that detects when the mass of the element becomes null.
|
class |
RelativeDateDetector
Date detector defined by relative date.
|
class |
RFVisibilityDetector
Finder for ground station / satellite RF visibility events.
|
class |
SatToSatMutualVisibilityDetector
Mutual spacecraft visibility detector : the g function is positive only if each spacecraft is in the main field of
view of the other one's sensor.
|
class |
SensorInhibitionDetector
Event detector for the inhibition of a sensor.
|
class |
SensorVisibilityDetector
Event detector for the visibility of a sensor.
|
class |
SolarTimeAngleDetector
Detects when the solar time angle of a spacecraft is equal to a predetermined value.
The solar time is represented by the angle between the projections of the Sun in the osculator orbital plane and the satellite position; therefore this angle is equal to zero when the solar time is 12.00h and Π when the solar time is 0.00h (Solar Time In Hours = 12.00h + solar time angle * 12 / Π). |
class |
StationToSatMutualVisibilityDetector
Mutual station to spacecraft visibility detector : the g function is positive only if the station's sensor sees the
spacecraft's sensor AND the spacecraft's sensor sees the station's sensor.
|
class |
SurfaceDistanceDetector
Detects when the distance from the spacecraft to the surface of a given body reaches a predetermined value.
|
class |
TargetInFieldOfViewDetector
Event detector for the main target visibility of a sensor.
|
class |
ThreeBodiesAngleDetector
Detects when the angle between three bodies is equal to a predetermined value.
|
class |
VisibilityFromStationDetector
Finder for satellite apparent entering in a station's field of view.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector |
TargetInFieldOfViewDetector.copy()
A copy of the detector.
|
EventDetector |
DotProductDetector.copy()
A copy of the detector.
|
EventDetector |
ExtremaLongitudeDetector.copy()
A copy of the detector.
|
EventDetector |
SatToSatMutualVisibilityDetector.copy()
A copy of the detector.
|
EventDetector |
StationToSatMutualVisibilityDetector.copy()
A copy of the detector.
|
EventDetector |
CentralBodyMaskCircularFOVDetector.copy()
A copy of the detector.
|
EventDetector |
BetaAngleDetector.copy()
A copy of the detector.
|
EventDetector |
EclipseDetector.copy()
A copy of the detector.
|
EventDetector |
NodeDetector.copy()
A copy of the detector.
|
EventDetector |
AngularMomentumExcessDetector.copy()
A copy of the detector.
|
EventDetector |
DateDetector.copy()
A copy of the detector.
|
EventDetector |
AlignmentDetector.copy()
A copy of the detector.
|
EventDetector |
DistanceDetector.copy()
A copy of the detector.
|
EventDetector |
MaskingDetector.copy()
A copy of the detector.
|
EventDetector |
CombinedPhenomenaDetector.copy()
A copy of the detector.
|
EventDetector |
AOLDetector.copy()
A copy of the detector.
|
EventDetector |
AltitudeDetector.copy()
A copy of the detector.
|
EventDetector |
RFVisibilityDetector.copy()
A copy of the detector.
|
EventDetector |
ExtremaThreeBodiesAngleDetector.copy()
A copy of the detector.
|
EventDetector |
SolarTimeAngleDetector.copy()
A copy of the detector.
|
EventDetector |
NullMassDetector.copy()
A copy of the detector.
|
EventDetector |
NullMassPartDetector.copy()
A copy of the detector.
|
EventDetector |
EarthZoneDetector.copy()
A copy of the detector.
|
EventDetector |
ElevationDetector.copy()
A copy of the detector.
|
EventDetector |
CircularFieldOfViewDetector.copy()
A copy of the detector.
|
EventDetector |
SurfaceDistanceDetector.copy()
A copy of the detector.
|
EventDetector |
VisibilityFromStationDetector.copy()
A copy of the detector.
|
EventDetector |
NadirSolarIncidenceDetector.copy()
A copy of the detector.
|
EventDetector |
ExtremaLatitudeDetector.copy()
A copy of the detector.
|
EventDetector |
CenteredAolPassageDetector.copy()
A copy of the detector.
|
EventDetector |
DihedralFieldOfViewDetector.copy()
A copy of the detector.
|
EventDetector |
ThreeBodiesAngleDetector.copy()
A copy of the detector.
|
EventDetector |
IntervalOccurrenceDetector.copy()
A copy of the detector.
|
EventDetector |
LongitudeDetector.copy()
A copy of the detector.
|
EventDetector |
FlightDomainExcessDetector.copy()
A copy of the detector.
|
EventDetector |
RelativeDateDetector.copy()
A copy of the detector.
|
EventDetector |
ExtremaDistanceDetector.copy()
A copy of the detector.
|
EventDetector |
SensorInhibitionDetector.copy()
A copy of the detector.
|
EventDetector |
ApparentElevationDetector.copy()
A copy of the detector.
|
EventDetector |
GroundMaskElevationDetector.copy()
A copy of the detector.
|
EventDetector |
AnomalyDetector.copy()
A copy of the detector.
|
EventDetector |
ApsideDetector.copy()
A copy of the detector.
|
EventDetector |
ExtremaElevationDetector.copy()
A copy of the detector.
|
EventDetector |
SensorVisibilityDetector.copy()
A copy of the detector.
|
EventDetector |
LocalTimeAngleDetector.copy()
A copy of the detector.
|
EventDetector |
ExtremaSightAxisDetector.copy()
A copy of the detector.
|
EventDetector |
LatitudeDetector.copy()
A copy of the detector.
|
EventDetector |
CombinedPhenomenaDetector.getDetector1()
Returns first detector.
|
EventDetector |
CombinedPhenomenaDetector.getDetector2()
Returns second detector.
|
EventDetector |
IntervalOccurrenceDetector.getEvent()
Get event to detect.
|
| Constructor and Description |
|---|
CombinedPhenomenaDetector(EventDetector d1,
boolean d1IncreasingIsStart,
EventDetector d2,
boolean d2IncreasingIsStart,
boolean togetherIn)
Constructor for the detector of the combination of two phenomena.
|
CombinedPhenomenaDetector(EventDetector d1,
boolean d1IncreasingIsStart,
EventDetector d2,
boolean d2IncreasingIsStart,
boolean togetherIn,
EventDetector.Action action)
Constructor for the detector of the combination of two phenomena.
|
IntervalOccurrenceDetector(EventDetector eventToDetect,
int firstOccurrenceIn,
int lastOccurrenceIn,
int stepIn,
EventDetector.Action actionAtOccurrence)
Constructor.
|
IntervalOccurrenceDetector(EventDetector eventToDetect,
int firstOccurrenceIn,
int lastOccurrenceIn,
int stepIn,
EventDetector.Action actionAtOccurrence,
boolean remove)
Constructor.
|
NthOccurrenceDetector(EventDetector eventToDetect,
int occurrence,
EventDetector.Action actionAtOccurrence)
Constructor.
|
NthOccurrenceDetector(EventDetector eventToDetect,
int occurrence,
EventDetector.Action actionAtOccurrence,
boolean remove)
Constructor.
|
| Modifier and Type | Interface and Description |
|---|---|
interface |
CodingEventDetector
This interface represents an event detector that is able to build a
CodedEvent object. |
| Modifier and Type | Class and Description |
|---|---|
class |
GenericCodingEventDetector
This class represents an all-purpose implementation of the
CodingEventDetector interface. |
| Modifier and Type | Method and Description |
|---|---|
EventDetector |
GenericCodingEventDetector.copy()
A copy of the detector.
|
EventDetector |
EventsLogger.LoggedEvent.getEventDetector()
Get the event detector triggered.
|
EventDetector |
CodedEventsLogger.monitorDetector(CodingEventDetector detector)
Takes a
CodingEventDetector instance and returns an EventDetector instance that will trigger this
CodedEventsLogger every time eventOccurred is called. |
EventDetector |
EventsLogger.monitorDetector(EventDetector monitoredDetector)
Monitor an event detector.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector |
EventsLogger.monitorDetector(EventDetector monitoredDetector)
Monitor an event detector.
|
| Constructor and Description |
|---|
GenericCodingEventDetector(EventDetector eventDetectorIn,
String increasingCodeIn,
String decreasingCodeIn)
Constructor for a
GenericCodingEventDetector that does not support a Phenomenon. |
GenericCodingEventDetector(EventDetector eventDetectorIn,
String increasingCodeIn,
String decreasingCodeIn,
boolean increasingIsStartIn,
String phenomenonCodeIn)
Constructor for a
GenericCodingEventDetector that supports a Phenomenon.No delays and no occurrence numbers are associated to the events detected by this detector. |
GenericCodingEventDetector(EventDetector eventDetectorIn,
String increasingCodeIn,
String decreasingCodeIn,
boolean increasingIsStartIn,
String phenomenonCodeIn,
double delayIn,
int occurrenceIn)
Constructor for a
GenericCodingEventDetector that supports a Phenomenon.A delay and/or an occurrence number can be associated to the events detected by this detector. When a delay is added to the detected events, two kinds of events will be coded: - the original events, with their original codes; - the delayed events, whose codes will be "DELAYED_" followed by the original code. |
GenericCodingEventDetector(EventDetector eventDetectorIn,
String increasingCodeIn,
String decreasingCodeIn,
double delayIn,
int occurrenceIn)
Constructor for a
GenericCodingEventDetector that does not support a Phenomenon.When a delay is added to the detected events, two kinds of events will be coded: - the original events, with their original codes; - the delayed events, whose codes will be "DELAYED_" followed by the original code. |
| Modifier and Type | Class and Description |
|---|---|
class |
EventShifter
Wrapper shifting events occurrences times.
|
class |
SignalPropagationWrapperDetector
Wrap a
signal propagation event detector and compute the emitter & receiver
dates of the occurred events. |
| Modifier and Type | Method and Description |
|---|---|
EventDetector |
SignalPropagationWrapperDetector.copy()
A copy of the detector.
|
EventDetector |
EventShifter.copy()
A copy of the detector.
|
EventDetector |
AdaptedEventDetector.getDetector()
Get the detector object.
|
EventDetector |
EventState.getEventDetector()
Get the underlying event detector.
|
| Constructor and Description |
|---|
AdaptedEventDetector(EventDetector detectorIn,
Map<String,AdditionalStateInfo> info,
OrbitType orbitTypeIn,
PositionAngle angleTypeIn,
AttitudeProvider attProviderForces,
AttitudeProvider attProviderEvents,
AbsoluteDate referenceDateIn,
double muIn,
Frame integrationFrameIn)
Build a wrapped event detector.
|
AdaptedMonoEventDetector(EventDetector detector,
OrbitType orbitType,
PositionAngle angleType,
MultiAttitudeProvider attProviderForces,
MultiAttitudeProvider attProviderEvents,
AbsoluteDate referenceDate,
MultiStateVectorInfo stateVectorInfo,
String satId)
Build a wrapped event detector.
|
EventShifter(EventDetector detectorIn,
boolean useShiftedStatesIn,
double increasingTimeShift,
double decreasingTimeShift)
Build a new instance.
|
EventState(EventDetector detectorIn)
Simple constructor.
|
EventState(EventDetector detectorIn,
UnivariateSolver solverIn)
Constructor allowing the user to provide
the solver used in switch detection.
|
OneSatEventDetectorWrapper(EventDetector detector,
String satId)
Simple constructor.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector[] |
EmpiricalForce.getEventsDetectors()
Get the discrete events related to the model.
|
EventDetector[] |
ForceModel.getEventsDetectors()
Get the discrete events related to the model.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector[] |
DragForce.getEventsDetectors()
There are no discrete events for this model.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector[] |
AbstractBodyAttraction.getEventsDetectors()
Get the discrete events related to the model.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector[] |
AbstractTides.getEventsDetectors()
Get the discrete events related to the model.
|
| Modifier and Type | Class and Description |
|---|---|
class |
ImpulseManeuver
Impulse maneuver model.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector[] |
ContinuousThrustManeuver.getEventsDetectors()
Get the discrete events related to the model.
|
EventDetector[] |
ConstantThrustError.getEventsDetectors()
Get the discrete events related to the model.
|
EventDetector |
ImpulseManeuver.getTrigger()
Get the triggering event.
|
| Constructor and Description |
|---|
ConstantThrustError(EventDetector startEventDetector,
EventDetector stopEventDetector,
Frame frame,
IParamDiffFunction fx,
IParamDiffFunction fy,
IParamDiffFunction fz)
Create a constant thrust error model whose x, y and z components are constant functions:
fx = cx fy = cy fz = cz |
ConstantThrustError(EventDetector startEventDetector,
EventDetector stopEventDetector,
Frame frame,
Parameter cx,
Parameter cy,
Parameter cz)
Create a constant thrust error model whose x, y and z components are constant functions:
fx = cx fy = cy fz = cz |
ConstantThrustError(EventDetector startEventDetector,
EventDetector stopEventDetector,
IParamDiffFunction fx,
IParamDiffFunction fy,
IParamDiffFunction fz)
Create a constant thrust error model whose x, y and z components are constant functions:
fx = cx fy = cy fz = cz |
ConstantThrustError(EventDetector startEventDetector,
EventDetector stopEventDetector,
LOFType lofType,
IParamDiffFunction fx,
IParamDiffFunction fy,
IParamDiffFunction fz)
Create a constant thrust error model whose x, y and z components are constant functions:
fx = cx fy = cy fz = cz |
ConstantThrustError(EventDetector startEventDetector,
EventDetector stopEventDetector,
LOFType lofType,
Parameter cx,
Parameter cy,
Parameter cz)
Create a constant thrust error model whose x, y and z components are constant functions:
fx = cx fy = cy fz = cz |
ConstantThrustError(EventDetector startEventDetector,
EventDetector stopEventDetector,
Parameter cx,
Parameter cy,
Parameter cz)
Create a constant thrust error model whose x, y and z components are constant functions:
fx = cx fy = cy fz = cz |
ContinuousThrustManeuver(EventDetector startEventDetector,
EventDetector stopEventDetector,
PropulsiveProperty engine,
IDependentVectorVariable<SpacecraftState> inDirection,
MassProvider massProvider,
TankProperty tank)
Constructor for a variable direction in satellite frame.
|
ContinuousThrustManeuver(EventDetector startEventDetector,
EventDetector stopEventDetector,
PropulsiveProperty engine,
IDependentVectorVariable<SpacecraftState> inDirection,
MassProvider massProvider,
TankProperty tank,
Frame frameIn)
Constructor for a variable direction in provided frame.
|
ContinuousThrustManeuver(EventDetector startEventDetector,
EventDetector stopEventDetector,
PropulsiveProperty engine,
IDependentVectorVariable<SpacecraftState> inDirection,
MassProvider massProvider,
TankProperty tank,
LOFType lofTyp)
Constructor for a variable direction in local orbital frame.
|
ContinuousThrustManeuver(EventDetector startEventDetector,
EventDetector stopEventDetector,
PropulsiveProperty engine,
Vector3D inDirection,
MassProvider massProvider,
TankProperty tank)
Constructor for a constant direction in satellite frame.
|
ContinuousThrustManeuver(EventDetector startEventDetector,
EventDetector stopEventDetector,
PropulsiveProperty engine,
Vector3D inDirection,
MassProvider massProvider,
TankProperty tank,
Frame frameIn)
Constructor for a constant direction in provided frame.
|
ContinuousThrustManeuver(EventDetector startEventDetector,
EventDetector stopEventDetector,
PropulsiveProperty engine,
Vector3D inDirection,
MassProvider massProvider,
TankProperty tank,
LOFType lofTyp)
Constructor for a constant direction in local orbital frame.
|
ImpulseManeuver(EventDetector inTrigger,
Vector3D inDeltaVSat,
double isp,
MassProvider massModel,
String part)
Build a new instance.
|
ImpulseManeuver(EventDetector inTrigger,
Vector3D inDeltaVSat,
double isp,
MassProvider massModel,
String part,
LOFType inLofType)
Build a new instance with a LocalOrbitalFrame.
|
ImpulseManeuver(EventDetector inTrigger,
Vector3D inDeltaVSat,
Frame inFrame,
double isp,
MassProvider massModel,
String part)
Build a new instance.
|
ImpulseManeuver(EventDetector inTrigger,
Vector3D inDeltaVSat,
Frame inFrame,
PropulsiveProperty engine,
MassProvider massModel,
TankProperty tank)
Build a new instance using propulsive and engine property.
|
ImpulseManeuver(EventDetector inTrigger,
Vector3D inDeltaVSat,
PropulsiveProperty engine,
MassProvider massModel,
TankProperty tank)
Build a new instance using propulsive and engine property.
|
ImpulseManeuver(EventDetector inTrigger,
Vector3D inDeltaVSat,
PropulsiveProperty engine,
MassProvider massModel,
TankProperty tank,
LOFType inLofType)
Build a new instance with a LocalOrbitalFrame and using propulsive and engine property.
|
| Modifier and Type | Class and Description |
|---|---|
class |
ImpulseDaManeuver
Class defining an impulsive maneuver with a semi-major axis increment as input.
|
class |
ImpulseDeManeuver
Class defining an impulsive maneuver with an eccentricity and a semi major axis increment as input.
|
class |
ImpulseDiManeuver
Class defining an impulsive maneuver with a inclination and eventually a semi major axis increment as input.
|
| Constructor and Description |
|---|
ImpulseDaManeuver(EventDetector inTrigger,
double da,
double isp,
MassProvider massModel,
String part)
Build a new instance.
|
ImpulseDaManeuver(EventDetector inTrigger,
double da,
PropulsiveProperty engine,
MassProvider massModel,
TankProperty tank)
Build a new instance using propulsive and engine property.
|
ImpulseDeManeuver(EventDetector inTrigger,
double de,
double da,
double isp,
MassProvider massModel,
String part,
boolean throwExceptionIfNotSolution)
Build a new instance.
|
ImpulseDeManeuver(EventDetector inTrigger,
double de,
double da,
PropulsiveProperty engine,
MassProvider massModel,
TankProperty tank,
boolean throwExceptionIfNotSolution)
Build a new instance using propulsive and engine property.
|
ImpulseDiManeuver(EventDetector inTrigger,
double di,
double da,
double isp,
MassProvider massModel,
String part,
boolean throwExceptionIfNotSolution)
Build a new instance.
|
ImpulseDiManeuver(EventDetector inTrigger,
double di,
double isp,
MassProvider massModel,
String part,
boolean throwExceptionIfNotSolution)
Build a new instance.
|
ImpulseDiManeuver(EventDetector inTrigger,
double di,
double da,
PropulsiveProperty engine,
MassProvider massModel,
TankProperty tank,
boolean throwExceptionIfNotSolution)
Build a new instance using propulsive and engine property.
|
ImpulseDiManeuver(EventDetector inTrigger,
double di,
PropulsiveProperty engine,
MassProvider massModel,
TankProperty tank,
boolean throwExceptionIfNotSolution)
Build a new instance using propulsive and engine property.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector[] |
RediffusedRadiationPressure.getEventsDetectors()
Get the discrete events related to the model.
|
EventDetector[] |
SolarRadiationPressure.getEventsDetectors()
Get the discrete events related to the model.
|
| Modifier and Type | Method and Description |
|---|---|
EventDetector[] |
LenseThirringRelativisticEffect.getEventsDetectors()
Get the discrete events related to the model.
|
EventDetector[] |
SchwarzschildRelativisticEffect.getEventsDetectors()
Get the discrete events related to the model.
|
EventDetector[] |
CoriolisRelativisticEffect.getEventsDetectors()
Get the discrete events related to the model.
|
| Modifier and Type | Method and Description |
|---|---|
Collection<EventDetector> |
AbstractPropagator.getEventsDetectors()
Get all the events detectors that have been added.
|
Collection<EventDetector> |
Propagator.getEventsDetectors()
Get all the events detectors that have been added.
|
| Modifier and Type | Method and Description |
|---|---|
void |
AbstractPropagator.addEventDetector(EventDetector detector)
Add an event detector.
|
void |
Propagator.addEventDetector(EventDetector detector)
Add an event detector.
|
void |
MultiPropagator.addEventDetector(EventDetector detector,
String satId)
Add an event detector to a specific spacecraft.
|
| Modifier and Type | Method and Description |
|---|---|
Collection<EventDetector> |
NumericalPropagator.getEventsDetectors()
Get all the events detectors that have been added.
|
| Modifier and Type | Method and Description |
|---|---|
void |
NumericalPropagator.addEventDetector(EventDetector detector)
Add an event detector.
|
protected void |
NumericalPropagator.setUpEventDetector(EventDetector osf)
Wrap an Orekit event detector and register it to the integrator.
|
| Modifier and Type | Method and Description |
|---|---|
void |
MultiNumericalPropagator.addEventDetector(EventDetector detector,
String satId)
Add an event detector to a specific spacecraft.
|
protected void |
MultiNumericalPropagator.setUpEventDetector(EventDetector osf,
Map<String,MultiAttitudeProvider> localAttProvForces,
Map<String,MultiAttitudeProvider> localAttProvEvents,
String satId)
Wrap an Orekit event detector and register it to the integrator.
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| Modifier and Type | Class and Description |
|---|---|
class |
PerigeeAltitudeDetector
Finder for satellite altitude crossing events in Semi-analytical theory.
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| Modifier and Type | Method and Description |
|---|---|
EventDetector |
PerigeeAltitudeDetector.copy()
A copy of the detector.
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| Modifier and Type | Method and Description |
|---|---|
Collection<EventDetector> |
StelaAbstractPropagator.getEventsDetectors()
Get all the events detectors that have been added.
|
| Modifier and Type | Method and Description |
|---|---|
void |
StelaAbstractPropagator.addEventDetector(EventDetector detector)
Add an event detector.
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