Uses of Interface
org.orekit.propagation.events.EventDetectorsProvider
Packages that use EventDetectorsProvider
Package
Description
This package provides classes to represent simple attitudes.
This package provides the interface for force models that will be used by the
NumericalPropagator, as well as
some classical spacecraft models for surface forces (spherical, box and solar array ...).This package provides all drag-related forces.
This package provides empirical forces.
This package provides all gravity-related forces.
This package provides inertial force model.
This package provides models of simple maneuvers.
This package provides propulsion models intended to be used with class
Maneuver.This package provides maneuver triggers' models intended to be used with class
Maneuver.This package provides all radiation pressure related forces.
This package provides classes related to navigation satellites attitude modeling.
Top level package for CR3BP Models used with a numerical propagator.
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
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Uses of EventDetectorsProvider in org.orekit.attitudes
Subinterfaces of EventDetectorsProvider in org.orekit.attitudesModifier and TypeInterfaceDescriptioninterfaceThis interface represents an attitude provider model set.interfaceThis interface represents an attitude provider that modifies/wraps another underlying provider.interfaceThis interface is intended for attitude ephemerides valid only during a time range.Classes in org.orekit.attitudes that implement EventDetectorsProviderModifier and TypeClassDescriptionclassABoundedAttitudeProviderthat covers a larger time span from several constituent attitude providers that cover shorter time spans.classAttitude provider with one satellite vector aligned and another one constrained to two targets.classThis classes manages a sequence of different attitude providers that are activated in turn according to switching events.classThis classes manages a sequence of different attitude providers that are activated in turn according to switching events.classThis class handles body center pointing attitude provider.classThis class handles a celestial body pointed attitude provider.classThis class handles a simple attitude provider at constant rate around a fixed axis.classThis class handles an attitude provider aligned with a frame or a fixed offset to it.classBase class for ground pointing attitude providers.classAbstract class for attitude provider modifiers using an underlying ground pointing law.classAttitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.classThis class provides a default attitude provider.classThis class handles nadir pointing attitude provider.classThis class handles a spin stabilized attitude provider.classThis class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.classThis class handles an attitude provider interpolating from a predefined table.classThis class handles target pointing attitude provider.classThis class handles torque-free motion of a general (non-symmetrical) body.classThis class handles yaw compensation attitude provider.classThis class handles yaw steering law. -
Uses of EventDetectorsProvider in org.orekit.forces
Subinterfaces of EventDetectorsProvider in org.orekit.forcesModifier and TypeInterfaceDescriptioninterfaceThis interface represents a force modifying spacecraft motion.interfaceInterface to wrap another force model. -
Uses of EventDetectorsProvider in org.orekit.forces.drag
Classes in org.orekit.forces.drag that implement EventDetectorsProviderModifier and TypeClassDescriptionclassBase class for drag force models.classAtmospheric drag force model.classTime span atmospheric drag force model. -
Uses of EventDetectorsProvider in org.orekit.forces.empirical
Classes in org.orekit.forces.empirical that implement EventDetectorsProviderModifier and TypeClassDescriptionclassAbstract class for parametric acceleration.classThis class implements a parametric acceleration.classTime span parametric acceleration model. -
Uses of EventDetectorsProvider in org.orekit.forces.gravity
Classes in org.orekit.forces.gravity that implement EventDetectorsProviderModifier and TypeClassDescriptionclassAbstract class for non-central body attraction force model.classDe Sitter post-Newtonian correction force due to general relativity.classThis class represents the gravitational field of a celestial body.classJ2-only force model.classLense-Thirring post-Newtonian correction force due to general relativity.classForce model for Newtonian central body attraction.classOcean tides force model.classPost-Newtonian correction force due to general relativity.classBody attraction force model computed as absolute acceleration towards a body.classBody attraction force model computed as relative acceleration towards frame center.classSolid tides force model.classThird body attraction force model.classThird body attraction force model. -
Uses of EventDetectorsProvider in org.orekit.forces.inertia
Classes in org.orekit.forces.inertia that implement EventDetectorsProvider -
Uses of EventDetectorsProvider in org.orekit.forces.maneuvers
Classes in org.orekit.forces.maneuvers that implement EventDetectorsProviderModifier and TypeClassDescriptionclassThis class implements a simple maneuver with constant thrust.classA generic model for maneuvers with finite-valued acceleration magnitude, as opposed to instantaneous changes in the velocity vector which are defined via detectors (inImpulseManeuverandFieldImpulseManeuver). -
Uses of EventDetectorsProvider in org.orekit.forces.maneuvers.propulsion
Subinterfaces of EventDetectorsProvider in org.orekit.forces.maneuvers.propulsionModifier and TypeInterfaceDescriptioninterfaceGeneric interface for a propulsion model used in aManeuver.interfaceInterface for a thrust-based propulsion model.Classes in org.orekit.forces.maneuvers.propulsion that implement EventDetectorsProviderModifier and TypeClassDescriptionclassThis abstract class simply serve as a container for a constant thrust maneuver.classConstant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust norm or the flow rate.classThrust propulsion model based on segmented profile.classThrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.classConstant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust vector in spherical coordinates. -
Uses of EventDetectorsProvider in org.orekit.forces.maneuvers.trigger
Subinterfaces of EventDetectorsProvider in org.orekit.forces.maneuvers.triggerModifier and TypeInterfaceDescriptioninterfaceGeneric interface for the maneuver triggers used in aManeuver.interfaceInterface for maneuver triggers with resetters.Classes in org.orekit.forces.maneuvers.trigger that implement EventDetectorsProviderModifier and TypeClassDescriptionclassBase class for triggers.classManeuver triggers based on a start and end date.classIntervalEventTrigger<T extends EventDetector>Maneuver triggers based on a single event detector that defines firing intervals.classStartStopEventsTrigger<A extends EventDetector,O extends EventDetector> Maneuver triggers based on a pair of event detectors that defines firing start and stop.classManeuver trigger based on time intervals. -
Uses of EventDetectorsProvider in org.orekit.forces.radiation
Subinterfaces of EventDetectorsProvider in org.orekit.forces.radiationModifier and TypeInterfaceDescriptioninterfaceInterface for radiation-related force models.Classes in org.orekit.forces.radiation that implement EventDetectorsProviderModifier and TypeClassDescriptionclassBase class for radiation force models.classThe Empirical CODE Orbit Model 2 (ECOM2) of the Center for Orbit Determination in Europe (CODE).classThe Knocke Earth Albedo and IR emission force model.classClass representing a light-induced radiation pressure force, by leveraging on a given flux model.classSolar radiation pressure force model. -
Uses of EventDetectorsProvider in org.orekit.gnss.attitude
Subinterfaces of EventDetectorsProvider in org.orekit.gnss.attitudeModifier and TypeInterfaceDescriptioninterfaceAttitude providers for navigation satellites.Classes in org.orekit.gnss.attitude that implement EventDetectorsProviderModifier and TypeClassDescriptionclassAttitude providers for Beidou geostationary orbit navigation satellites.classAttitude providers for Beidou inclined geosynchronous orbit navigation satellites.classAttitude providers for Beidou Medium Earth Orbit navigation satellites.classAttitude providers for Galileo navigation satellites.classAttitude providers for navigation satellites for which no specialized model is known.classAttitude providers for Glonass navigation satellites.classAttitude providers for GPS block IIA navigation satellites.classAttitude providers for GPS block IIF navigation satellites.classAttitude providers for GPS block IIR navigation satellites. -
Uses of EventDetectorsProvider in org.orekit.propagation.numerical.cr3bp
Classes in org.orekit.propagation.numerical.cr3bp that implement EventDetectorsProviderModifier and TypeClassDescriptionclassClass calculating the acceleration induced by CR3BP model. -
Uses of EventDetectorsProvider in org.orekit.propagation.semianalytical.dsst.forces
Subinterfaces of EventDetectorsProvider in org.orekit.propagation.semianalytical.dsst.forcesModifier and TypeInterfaceDescriptioninterfaceThis interface represents a force modifying spacecraft motion for aDSSTPropagator.Classes in org.orekit.propagation.semianalytical.dsst.forces that implement EventDetectorsProviderModifier and TypeClassDescriptionclassCommon handling ofDSSTForceModelmethods for Gaussian contributions to DSST propagation.classAtmospheric drag contribution to theDSSTPropagator.classSecond order J2-squared force model.classForce model for Newtonian central body attraction for theDSST propagator.classSolar radiation pressure contribution to theDSSTPropagator.classTesseral contribution to the central body gravitational perturbation.classThird body attraction perturbation to theDSSTPropagator.classZonal contribution to the central body gravitational perturbation.