Uses of Interface
org.orekit.utils.ParameterDriversProvider
Packages that use ParameterDriversProvider
Package
Description
This package provides classes to represent simple attitudes.
The measurements package defines everything that is related to orbit
determination measurements.
This package provides methods to handle GNSS measurements.
This package provides measurement modifier.
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.
This package provides models that simulate the impact of the ionosphere.
This package provides classes for implementing NeQuick ionosphere models.
This package provides models that simulate the impact of the troposphere.
This package contains class for the troposphere model OTU-4 P.834.
Top level package for analytical propagators.
This package provides classes to propagate GNSS orbits.
This package provides classes related to navigation data containing in
GNSS almanacs and navigation messages.
This package provides classes to propagate Intelsat's 11 elements.
This package provides classes to read and extrapolate tle's.
Utilities for integration-based propagators (both numerical and semi-analytical).
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 ParameterDriversProvider in org.orekit.attitudes
Subinterfaces of ParameterDriversProvider 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.interfaceInterface for (attitude) rotation models taking as inputs a spacecraft state and model parameters.interfaceThis interface is intended for attitude ephemerides valid only during a time range.Classes in org.orekit.attitudes that implement ParameterDriversProviderModifier 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 ParameterDriversProvider in org.orekit.estimation.measurements
Subinterfaces of ParameterDriversProvider in org.orekit.estimation.measurementsModifier and TypeInterfaceDescriptioninterfaceEstimationModifier<T extends ObservedMeasurement<T>>Interface for estimated measurements modifiers used for orbit determination.interfaceInterface underlying both observed and observing measurement objects.interfaceObservedMeasurement<T extends ObservedMeasurement<T>>Interface for measurements used for orbit determination.interfaceAbstract interface that contains those methods necessary for both space and ground-based satellite observers.Classes in org.orekit.estimation.measurements that implement ParameterDriversProviderModifier and TypeClassDescriptionclassAbstractMeasurement<T extends ObservedMeasurement<T>>Abstract class handling measurements boilerplate.classAbstract class underlying both observed and observing measurement objects.classAbstract class modeling one-way or two-way range-related measurement.classClass modeling an Azimuth-Elevation measurement from a ground station.classAngularMeasurement<T extends SignalBasedMeasurement<T>>Abstract class for ground-based angular measurements, when the sensor receives the signal.classClass modeling a Right Ascension - Declination measurement from an optical sensor, typically via astrometry.classClass modeling a bistatic range measurement using an emitter ground station and a receiver ground station.classClass modeling a bistatic range rate measurement using an emitter ground station and a receiver ground station.classClass modeling a Frequency Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.classClass modeling a ground station that can perform some measurements.classOne-way or two-way range measurements between two satellites.classClass multiplexing several measurements as one.classClass modeling a satellite that can be observed.classClass that accepts a PVCoordinatesProvider for a space- based measurement receiver.classClass modeling a position only measurement.classPseudoMeasurement<T extends PseudoMeasurement<T>>Abstract class modeling a position(-velocity) measurement, referred to as pseudo because it is not based on any signals.classClass modeling a position-velocity measurement.classClass modeling a range measurement received by an observer.classClass modeling one-way or two-way range rate measurement between two vehicles.classSignalBasedMeasurement<T extends ObservedMeasurement<T>>Abstract class modeling a measurement based on signal transmission.classClass modeling a Time Difference of Arrival measurement with a satellite as emitter and two observers as receivers.classClass modeling a turn-around range measurement using a primary observer and a secondary observer. -
Uses of ParameterDriversProvider in org.orekit.estimation.measurements.gnss
Classes in org.orekit.estimation.measurements.gnss that implement ParameterDriversProviderModifier and TypeClassDescriptionclassAbstractInterSatellitesMeasurement<T extends ObservedMeasurement<T>>Base class for measurement between two satellites that are both estimated.classAbstractOneWayGNSS<T extends ObservedMeasurement<T>>Abstract class for one-way GNSS measurement.classAbstractWindUp<T extends ObservedMeasurement<T>>Base class for wind-up effect computation.classOne way range-rate measurement between two satellites.classPhase measurement between two satellites.classModifier for wind-up effect in GNSSinter-satellites phase measurements.classOne-way GNSS phase measurement.classOne-way GNSS range measurement.classOne-way GNSS range rate measurement.classModifier for wind-up effect in GNSSone-way GNSS phase measurements.classClass modeling a phase measurement from a ground station.classModifier for wind-up effect in GNSSphase measurements. -
Uses of ParameterDriversProvider in org.orekit.estimation.measurements.modifiers
Classes in org.orekit.estimation.measurements.modifiers that implement ParameterDriversProviderModifier and TypeClassDescriptionclassClass modifying theoretical angular measurement with (the inverse of) stellar aberration.classClass modifying theoretical range-rate measurement with relativistic frequency deviation.classAbstractShapiroBaseModifier<T extends ObservedMeasurement<T>>Class modifying theoretical range measurement with Shapiro time delay.classAbstractShapiroPhaseModifier<T extends ObservedMeasurement<T>>Class modifying theoretical phase measurement with Shapiro time delay.classAbstractShapiroRangeModifier<T extends ObservedMeasurement<T>>Class modifying theoretical range measurement with Shapiro time delay.classClass modifying theoretical angular measurement with ionospheric delay.classClass modifying theoretical angular measurement with tropospheric radio refractive index.classBias<T extends ObservedMeasurement<T>>Class modeling a measurement bias.classClass modifying theoretical bistatic range measurement with ionospheric delay.classClass modifying theoretical bistatic range-rate measurement with ionospheric delay.classClass modifying theoretical bistatic range-rate measurements with tropospheric delay.classClass modifying theoretical bistatic range measurement with tropospheric delay.classDynamicOutlierFilter<T extends ObservedMeasurement<T>>Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.classMeasurementNoise<T extends ObservedMeasurement<T>>Class modeling a measurement noise.classOn-board antenna offset effect on inter-satellites phase measurements.classOn-board antenna offset effect on inter-satellites range measurements.classOn-board antenna offset effect on one-way GNSS phase measurements.classOn-board antenna offset effect on one-way GNSS range measurements.classOn-board antenna offset effect on turn around range measurements.classClass modifying theoretical range measurement with ionospheric delay.classOutlierFilter<T extends ObservedMeasurement<T>>Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.classGround and on-board antennas offsets effect on phase measurements.classGround and on-board antennas offsets effect on range measurements.classClass modifying theoretical phase measurement with ionospheric delay.classClass modifying theoretical phase measurement with tropospheric delay.classClass modifying theoretical range measurement with ionospheric delay.classClass modifying theoretical range-rate measurement with ionospheric delay.classClass modifying theoretical range-rate measurements with tropospheric delay.classClass modifying theoretical range measurement with tropospheric delay.classClass modifying theoretical range-rate measurement with relativistic frequency deviation.classClass modifying theoretical inter-satellites phase measurement with relativistic clock correction.classClass modifying theoretical inter-satellites range measurement with relativistic clock correction.classClass modifying theoretical one-way GNSS phase measurement with relativistic clock correction.classClass modifying theoretical one-way GNSS range measurement with relativistic clock correction.classClass modifying theoretical range-rate measurement with relativistic frequency deviation.classClass modifying theoretical phase measurement with relativistic clock correction.classClass modifying theoretical range measurement with relativistic clock correction.classClass modifying theoretical range-rate measurement with relativistic frequency deviation.classClass modifying theoretical inter-satellites phase measurements with relativistic J2 clock correction.classClass modifying theoretical inter-satellites range measurements with relativistic J2 clock correction.classClass modifying theoretical one-way phase measurements with relativistic J2 clock correction.classClass modifying one-way GNSS range theoretical measurements with relativistic J2 clock correction.classClass modifying theoretical phase measurements with relativistic J2 clock correction.classClass modifying theoretical range measurements with relativistic J2 clock correction.classClass modifying theoretical range measurement with Shapiro time delay.classClass modifying theoretical inter-satellites phase measurement with Shapiro time delay.classClass modifying theoretical range measurement with Shapiro time delay.classClass modifying theoretical one-way GNSS phase measurement with Shapiro time delay.classClass modifying theoretical range measurement with Shapiro time delay.classClass modifying theoretical phase measurement with Shapiro time delay.classClass modifying theoretical range measurement with Shapiro time delay.classClass modifying theoretical TDOA measurements with ionospheric delay.classClass modifying theoretical TDOA measurements with tropospheric delay.classClass modifying theoretical TurnAroundRange measurement with ionospheric delay.classClass modifying theoretical turn-around TurnAroundRange measurement with tropospheric delay.Methods in org.orekit.estimation.measurements.modifiers with parameters of type ParameterDriversProviderModifier and TypeMethodDescriptionstatic <T extends ObservedMeasurement<T>>
voidOneWayGNSSRangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer gnssSatellite, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement.static <T extends ObservedMeasurement<T>>
voidRangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer observer, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement.static <T extends ObservedMeasurement<T>>
voidRangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer observer, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement. -
Uses of ParameterDriversProvider in org.orekit.forces
Subinterfaces of ParameterDriversProvider in org.orekit.forcesModifier and TypeInterfaceDescriptioninterfaceThis interface represents a force modifying spacecraft motion.interfaceInterface to wrap another force model. -
Uses of ParameterDriversProvider in org.orekit.forces.drag
Classes in org.orekit.forces.drag that implement ParameterDriversProviderModifier and TypeClassDescriptionclassBase class for drag force models.classAtmospheric drag force model.classTime span atmospheric drag force model. -
Uses of ParameterDriversProvider in org.orekit.forces.empirical
Subinterfaces of ParameterDriversProvider in org.orekit.forces.empiricalModifier and TypeInterfaceDescriptioninterfaceAcceleration model used by empirical force.Classes in org.orekit.forces.empirical that implement ParameterDriversProviderModifier and TypeClassDescriptionclassAbstract class for parametric acceleration.classHarmonic acceleration model.classThis class implements a parametric acceleration.classPolynomial acceleration model.classTime span parametric acceleration model. -
Uses of ParameterDriversProvider in org.orekit.forces.gravity
Classes in org.orekit.forces.gravity that implement ParameterDriversProviderModifier 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 ParameterDriversProvider in org.orekit.forces.inertia
Classes in org.orekit.forces.inertia that implement ParameterDriversProvider -
Uses of ParameterDriversProvider in org.orekit.forces.maneuvers
Classes in org.orekit.forces.maneuvers that implement ParameterDriversProviderModifier 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 ParameterDriversProvider in org.orekit.forces.maneuvers.propulsion
Subinterfaces of ParameterDriversProvider 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 ParameterDriversProviderModifier 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 ParameterDriversProvider in org.orekit.forces.maneuvers.trigger
Subinterfaces of ParameterDriversProvider 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 ParameterDriversProviderModifier 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 ParameterDriversProvider in org.orekit.forces.radiation
Subinterfaces of ParameterDriversProvider in org.orekit.forces.radiationModifier and TypeInterfaceDescriptioninterfaceInterface for radiation-related force models.Classes in org.orekit.forces.radiation that implement ParameterDriversProviderModifier 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 ParameterDriversProvider in org.orekit.gnss.attitude
Subinterfaces of ParameterDriversProvider in org.orekit.gnss.attitudeModifier and TypeInterfaceDescriptioninterfaceAttitude providers for navigation satellites.Classes in org.orekit.gnss.attitude that implement ParameterDriversProviderModifier 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 ParameterDriversProvider in org.orekit.models.earth.ionosphere
Subinterfaces of ParameterDriversProvider in org.orekit.models.earth.ionosphereModifier and TypeInterfaceDescriptioninterfaceDefines a ionospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.Classes in org.orekit.models.earth.ionosphere that implement ParameterDriversProviderModifier and TypeClassDescriptionclassAbstract ionospheric model parent class.classAn estimated ionospheric model.classGlobal Ionosphere Map (GIM) model.classKlobuchar ionospheric delay model.classIonospheric model based on SSR IM201 message. -
Uses of ParameterDriversProvider in org.orekit.models.earth.ionosphere.nequick
Classes in org.orekit.models.earth.ionosphere.nequick that implement ParameterDriversProviderModifier and TypeClassDescriptionclassGalileo-specific version of NeQuick engine.classOriginal model from Aeronomy and Radiopropagation Laboratory of the Abdus Salam International Centre for Theoretical Physics Trieste, Italy.classNeQuick ionospheric delay model. -
Uses of ParameterDriversProvider in org.orekit.models.earth.troposphere
Subinterfaces of ParameterDriversProvider in org.orekit.models.earth.troposphereModifier and TypeInterfaceDescriptioninterfaceDefines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.Classes in org.orekit.models.earth.troposphere that implement ParameterDriversProviderModifier and TypeClassDescriptionclassThe Vienna tropospheric delay model for radio techniques.classThe Askne Nordius model.classThe canonical Saastamoinen model.classDefines a constant tropospheric model.classAn estimated tropospheric model.classA static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via theDataProvidersManager.classThe Marini-Murray tropospheric delay model for laser ranging.classThe Mendes - Pavlis tropospheric delay model for optical techniques.classThe modified Hopfield model.classThe modified Saastamoinen model.classTime span estimated tropospheric model.classThe Vienna 1 tropospheric delay model for radio techniques.classThe Vienna 3 tropospheric delay model for radio techniques. -
Uses of ParameterDriversProvider in org.orekit.models.earth.troposphere.iturp834
Classes in org.orekit.models.earth.troposphere.iturp834 that implement ParameterDriversProvider -
Uses of ParameterDriversProvider in org.orekit.propagation.analytical
Classes in org.orekit.propagation.analytical that implement ParameterDriversProviderModifier and TypeClassDescriptionclassConverter for analytical orbit propagator.classThis class propagates aSpacecraftStateusing the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).classFieldAbstractAnalyticalPropagator<T extends CalculusFieldElement<T>>Common handling ofFieldPropagatormethods for analytical propagators.classFieldBrouwerLyddanePropagator<T extends CalculusFieldElement<T>>This class propagates aFieldSpacecraftStateusing the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).classFieldEcksteinHechlerPropagator<T extends CalculusFieldElement<T>>This class propagates aFieldSpacecraftStateusing the analytical Eckstein-Hechler model.classFieldEphemeris<T extends CalculusFieldElement<T>>This class is designed to accept and handle tabulated orbital entries.classFieldKeplerianPropagator<T extends CalculusFieldElement<T>>Simple Keplerian orbit propagator. -
Uses of ParameterDriversProvider in org.orekit.propagation.analytical.gnss
Classes in org.orekit.propagation.analytical.gnss that implement ParameterDriversProviderModifier and TypeClassDescriptionclassFieldGnssPropagator<T extends CalculusFieldElement<T>>Common handling ofFieldAbstractAnalyticalPropagatormethods for GNSS propagators. -
Uses of ParameterDriversProvider in org.orekit.propagation.analytical.gnss.data
Classes in org.orekit.propagation.analytical.gnss.data that implement ParameterDriversProviderModifier and TypeClassDescriptionclassAbstractAlmanac<O extends AbstractAlmanac<O>>Base class for GNSS almanacs.classAbstractNavigationMessage<O extends AbstractNavigationMessage<O>>Base class for GNSS navigation messages.classClass for BeiDou almanac.classContainer for data contained in a Beidou civilian navigation message.classContainer for data contained in a BeiDou navigation message.classCivilianNavigationMessage<O extends CivilianNavigationMessage<O>>Container for data contained in a GPS/QZNSS civilian navigation message.classCommonGnssData<O extends CommonGnssData<O>>Container for common GNSS data contained in almanac and navigation messages.classFieldAbstractAlmanac<T extends CalculusFieldElement<T>,O extends AbstractAlmanac<O>> Base class for GNSS almanacs.classFieldAbstractNavigationMessage<T extends CalculusFieldElement<T>,O extends AbstractNavigationMessage<O>> Base class for GNSS navigation messages.classFieldBeidouAlmanac<T extends CalculusFieldElement<T>>Class for BeiDou almanac.classFieldBeidouCivilianNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in a Beidou civilian navigation message.classFieldBeidouLegacyNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in a BeiDou navigation message.classFieldCivilianNavigationMessage<T extends CalculusFieldElement<T>,O extends CivilianNavigationMessage<O>> Container for data contained in a GPS/QZNSS civilian navigation message.classFieldCommonGnssData<T extends CalculusFieldElement<T>,O extends CommonGnssData<O>> Container for common GNSS data contained in almanac and navigation messages.classFieldGalileoAlmanac<T extends CalculusFieldElement<T>>Class for Galileo almanac.classFieldGalileoNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in a Galileo navigation message.classFieldGnssOrbitalElements<T extends CalculusFieldElement<T>,O extends GNSSOrbitalElements<O>> This class provides the minimal set of orbital elements needed by theFieldGnssPropagator.classFieldGPSAlmanac<T extends CalculusFieldElement<T>>This class holds a GPS almanac as read from SEM or YUMA files.classFieldGPSCivilianNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in a GPS navigation message.classFieldGPSLegacyNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in a GPS navigation message.classFieldLegacyNavigationMessage<T extends CalculusFieldElement<T>,O extends LegacyNavigationMessage<O>> Container for data contained in a GPS/QZNSS legacy navigation message.classFieldNavICAlmanac<T extends CalculusFieldElement<T>>Class for NavIC almanac.classFieldNavicL1NvNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in a NavIC navigation message.classFieldNavicLegacyNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in an NavIC navigation message.classFieldQZSSAlmanac<T extends CalculusFieldElement<T>>This class holds a QZSS almanac as read from YUMA files.classFieldQZSSCivilianNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in a QZSS navigation message.classFieldQZSSLegacyNavigationMessage<T extends CalculusFieldElement<T>>Container for data contained in a QZSS navigation message.classClass for Galileo almanac.classContainer for data contained in a Galileo navigation message.classGNSSOrbitalElements<O extends GNSSOrbitalElements<O>>This class provides the minimal set of orbital elements needed by theGNSSPropagator.classThis class manages the non-keplerian parameter drivers forGNSSOrbitalElementsandFieldGnssOrbitalElements.classThis class holds a GPS almanac as read from SEM or YUMA files.classContainer for data contained in a GPS navigation message.classContainer for data contained in a GPS navigation message.classLegacyNavigationMessage<O extends LegacyNavigationMessage<O>>Container for data contained in a GPS/QZNSS legacy navigation message.classClass for NavIC almanac.classContainer for data contained in a NavIC navigation message.classContainer for data contained in an NavIC navigation message.classThis class holds a QZSS almanac as read from YUMA files.classContainer for data contained in a QZSS navigation message.classContainer for data contained in a QZSS navigation message. -
Uses of ParameterDriversProvider in org.orekit.propagation.analytical.intelsat
Classes in org.orekit.propagation.analytical.intelsat that implement ParameterDriversProviderModifier and TypeClassDescriptionclassFieldIntelsatElevenElementsPropagator<T extends CalculusFieldElement<T>>This class provides elements to propagate Intelsat's 11 elements. -
Uses of ParameterDriversProvider in org.orekit.propagation.analytical.tle
Classes in org.orekit.propagation.analytical.tle that implement ParameterDriversProviderModifier and TypeClassDescriptionclassFieldDeepSDP4<T extends CalculusFieldElement<T>>This class contains the methods that compute deep space perturbation terms.classFieldSGP4<T extends CalculusFieldElement<T>>This class contains methods to compute propagated coordinates with the SGP4 model.classFieldTLE<T extends CalculusFieldElement<T>>This class is a container for a single set of TLE data.classFieldTLEPropagator<T extends CalculusFieldElement<T>>This class provides elements to propagate TLE's.classThis class is a container for a single set of TLE data. -
Uses of ParameterDriversProvider in org.orekit.propagation.integration
Classes in org.orekit.propagation.integration that implement ParameterDriversProviderModifier and TypeClassDescriptionclassFieldIntegratedEphemeris<T extends CalculusFieldElement<T>>This class stores sequentially generated orbital parameters for later retrieval.Methods in org.orekit.propagation.integration with parameters of type ParameterDriversProviderModifier and TypeMethodDescriptionGradient[]AbstractGradientConverter.getParameters(FieldSpacecraftState<Gradient> state, ParameterDriversProvider parametricModel) Get the parametric model parameters, return gradient values for each span of each driver (several gradient values for each parameter).Gradient[]AbstractGradientConverter.getParametersAtStateDate(FieldSpacecraftState<Gradient> state, ParameterDriversProvider parametricModel) Get the parametric model parameters, return gradient values at state date for each driver (only 1 gradient value for each parameter).AbstractGradientConverter.getState(ParameterDriversProvider parametricModel) Get the state with the number of parameters consistent with parametric model. -
Uses of ParameterDriversProvider in org.orekit.propagation.numerical.cr3bp
Classes in org.orekit.propagation.numerical.cr3bp that implement ParameterDriversProviderModifier and TypeClassDescriptionclassClass calculating the acceleration induced by CR3BP model. -
Uses of ParameterDriversProvider in org.orekit.propagation.semianalytical.dsst.forces
Subinterfaces of ParameterDriversProvider 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 ParameterDriversProviderModifier 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.