Uses of Class
org.orekit.propagation.events.AbstractDetector

Packages that use AbstractDetector

fr.cnes.sirius.patrius.events
fr.cnes.sirius.patrius.events.sensor
fr.cnes.sirius.patrius.stela
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.

Uses of AbstractDetector in fr.cnes.sirius.patrius.events

Subclasses of AbstractDetector in fr.cnes.sirius.patrius.events

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	CombinedPhenomenaDetector This class finds the events resulting from the combination of two phenomena.
class	EarthZoneDetector Detects when the satellite enters a ground zone (several zones can be defined at the same time).

Uses of AbstractDetector in fr.cnes.sirius.patrius.events.sensor

Subclasses of AbstractDetector in fr.cnes.sirius.patrius.events.sensor

class	AbstractDetectorWithTropoCorrection Abstract event detector using a station elevation correction.
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	MaskingDetector Sensor masking detector.
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
class	SensorVisibilityDetector
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	TargetInFieldOfViewDetector
class	VisibilityFromStationDetector Finder for satellite apparent entering in a station's field of view.

Uses of AbstractDetector in fr.cnes.sirius.patrius.stela

Subclasses of AbstractDetector in fr.cnes.sirius.patrius.stela

class

PerigeeAltitudeDetector Finder for satellite altitude crossing events in Semi-analytical theory.

Uses of AbstractDetector in org.orekit.forces.maneuvers

Subclasses of AbstractDetector in org.orekit.forces.maneuvers

class

ImpulseManeuver Impulse maneuver model.

Uses of AbstractDetector in org.orekit.propagation.events

Subclasses of AbstractDetector in org.orekit.propagation.events

class	AlignmentDetector Finder for satellite/body alignment events.
class	AltitudeDetector Finder for satellite altitude crossing events.
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	CircularFieldOfViewDetector Finder for target entry/exit events with respect to a satellite sensor field of view.
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	EclipseDetector Finder for satellite eclipse related events.
class	ElevationDetector Finder for satellite raising/setting events.
class	EventShifter Wrapper shifting events occurrences times.
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. The local minimum or maximum is chosen through a constructor parameter, with values ExtremaElevationDetector.MIN, ExtremaElevationDetector.MAX and ExtremaElevationDetector.MIN_MAX for both.
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	ExtremaThreeBodiesAngleDetector Detects the maximal or minimal angle between three bodies is reached, the spacecraft eventually being one of the bodies.
class	GroundMaskElevationDetector Finder for satellite azimuth-elevation events with respect to a mask.
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	NadirSolarIncidenceDetector Spacecraft's nadir point solar incidence detector.
class	NodeDetector Finder for node crossing events.
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	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	ThreeBodiesAngleDetector Detects when the angle between three bodies is equal to a predetermined value.