Uses of Interface
org.orekit.utils.ParameterDriversProvider

Packages that use ParameterDriversProvider

Package	Description
org.orekit.estimation.measurements	The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.gnss	This package provides methods to handle GNSS measurements.
org.orekit.estimation.measurements.modifiers	This package provides measurement modifier.
org.orekit.forces	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 ...).
org.orekit.forces.drag	This package provides all drag-related forces.
org.orekit.forces.empirical	This package provides empirical forces.
org.orekit.forces.gravity	This package provides all gravity-related forces.
org.orekit.forces.inertia	This package provides inertial force model.
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.forces.maneuvers.propulsion	This package provides propulsion models intended to be used with class Maneuver.
org.orekit.forces.maneuvers.trigger	This package provides maneuver triggers' models intended to be used with class Maneuver.
org.orekit.forces.radiation	This package provides all radiation pressure related forces.
org.orekit.models.earth.ionosphere	This package provides models that simulate the impact of the ionosphere.
org.orekit.models.earth.troposphere	This package provides models that simulate the impact of the troposphere.
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.analytical.intelsat	This package provides classes to propagate Intelsat's 11 elements.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical.cr3bp	Top level package for CR3BP Models used with a numerical propagator.
org.orekit.propagation.semianalytical.dsst.forces	This package provides force models for Draper Semi-analytical Satellite Theory (DSST).

Uses of ParameterDriversProvider in org.orekit.estimation.measurements

Subinterfaces of ParameterDriversProvider in org.orekit.estimation.measurements

Modifier and Type	Interface	Description
interface	EstimationModifier<T extends ObservedMeasurement<T>>	Interface for estimated measurements modifiers used for orbit determination.
interface	ObservedMeasurement<T extends ObservedMeasurement<T>>	Interface for measurements used for orbit determination.

Classes in org.orekit.estimation.measurements that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractMeasurement<T extends ObservedMeasurement<T>>	Abstract class handling measurements boilerplate.
class	AngularAzEl	Class modeling an Azimuth-Elevation measurement from a ground station.
class	AngularRaDec	Class modeling a Right Ascension - Declination measurement from a ground point (station, telescope).
class	BistaticRange	Class modeling a bistatic range measurement using an emitter ground station and a receiver ground station.
class	BistaticRangeRate	Class modeling a bistatic range rate measurement using an emitter ground station and a receiver ground station.
class	FDOA	Class modeling a Frequency Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.
class	GroundReceiverMeasurement<T extends GroundReceiverMeasurement<T>>	Base class modeling a measurement where receiver is a ground station.
class	InterSatellitesRange	One-way or two-way range measurements between two satellites.
class	MultiplexedMeasurement	Class multiplexing several measurements as one.
class	Position	Class modeling a position only measurement.
class	PV	Class modeling a position-velocity measurement.
class	Range	Class modeling a range measurement from a ground station.
class	RangeRate	Class modeling one-way or two-way range rate measurement between two vehicles.
class	TDOA	Class modeling a Time Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.
class	TurnAroundRange	Class modeling a turn-around range measurement using a primary ground station and a secondary ground station.

Uses of ParameterDriversProvider in org.orekit.estimation.measurements.gnss

Classes in org.orekit.estimation.measurements.gnss that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractInterSatellitesMeasurement<T extends ObservedMeasurement<T>>	Base class for measurement between two satellites that are both estimated.
class	AbstractOnBoardMeasurement<T extends ObservedMeasurement<T>>	Base class modeling a measurement where receiver is a satellite.
class	AbstractOneWayGNSSMeasurement<T extends ObservedMeasurement<T>>	Base class for one-way GNSS measurement.
class	AbstractWindUp<T extends ObservedMeasurement<T>>	Base class for wind-up effect computation.
class	InterSatellitesOneWayRangeRate	One way range-rate measurement between two satellites.
class	InterSatellitesPhase	Phase measurement between two satellites.
class	InterSatellitesWindUp	Modifier for wind-up effect in GNSS inter-satellites phase measurements.
class	OneWayGNSSPhase	One-way GNSS phase measurement.
class	OneWayGNSSRange	One-way GNSS range measurement.
class	OneWayGNSSRangeRate	One-way GNSS range rate measurement.
class	Phase	Class modeling a phase measurement from a ground station.
class	WindUp	Modifier for wind-up effect in GNSS phase measurements.

Uses of ParameterDriversProvider in org.orekit.estimation.measurements.modifiers

Classes in org.orekit.estimation.measurements.modifiers that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AberrationModifier	Class modifying theoretical angular measurement with (the inverse of) stellar aberration.
class	AbstractRelativisticClockOnBoardRangeRateModifier<T extends ObservedMeasurement<T>>	Class modifying theoretical range-rate measurement with relativistic frequency deviation.
class	AngularIonosphericDelayModifier	Class modifying theoretical angular measurement with ionospheric delay.
class	AngularRadioRefractionModifier	Class modifying theoretical angular measurement with tropospheric radio refractive index.
class	AngularTroposphericDelayModifier	Deprecated. as of 12.1, AngularRadioRefractionModifier shall be used to handle tropospheric effect on angular measurements
class	Bias<T extends ObservedMeasurement<T>>	Class modeling a measurement bias.
class	BistaticRangeIonosphericDelayModifier	Class modifying theoretical bistatic range measurement with ionospheric delay.
class	BistaticRangeRateIonosphericDelayModifier	Class modifying theoretical bistatic range-rate measurement with ionospheric delay.
class	BistaticRangeRateTroposphericDelayModifier	Class modifying theoretical bistatic range-rate measurements with tropospheric delay.
class	BistaticRangeTroposphericDelayModifier	Class modifying theoretical bistatic range measurement with tropospheric delay.
class	DynamicOutlierFilter<T extends ObservedMeasurement<T>>	Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
class	InterSatellitesPhaseAmbiguityModifier	Deprecated. as of 12.1 ambiguity is managed directly by raw measurements InterSatellitesPhase
class	OnBoardAntennaInterSatellitesPhaseModifier	On-board antenna offset effect on inter-satellites phase measurements.
class	OnBoardAntennaInterSatellitesRangeModifier	On-board antenna offset effect on inter-satellites range measurements.
class	OnBoardAntennaOneWayGNSSPhaseModifier	On-board antenna offset effect on one-way GNSS phase measurements.
class	OnBoardAntennaOneWayGNSSRangeModifier	On-board antenna offset effect on one-way GNSS range measurements.
class	OnBoardAntennaTurnAroundRangeModifier	On-board antenna offset effect on turn around range measurements.
class	OneWayGNSSPhaseAmbiguityModifier	Deprecated. as of 12.1 ambiguity is managed directly by raw measurements OneWayGNSSPhase
class	OutlierFilter<T extends ObservedMeasurement<T>>	Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
class	PhaseAmbiguityModifier	Deprecated. as of 12.1 ambiguity is managed directly by raw measurements Phase
class	PhaseCentersPhaseModifier	Ground and on-board antennas offsets effect on phase measurements.
class	PhaseCentersRangeModifier	Ground and on-board antennas offsets effect on range measurements.
class	PhaseIonosphericDelayModifier	Class modifying theoretical phase measurement with ionospheric delay.
class	PhaseTroposphericDelayModifier	Class modifying theoretical phase measurement with tropospheric delay.
class	RangeIonosphericDelayModifier	Class modifying theoretical range measurement with ionospheric delay.
class	RangeRateIonosphericDelayModifier	Class modifying theoretical range-rate measurement with ionospheric delay.
class	RangeRateTroposphericDelayModifier	Class modifying theoretical range-rate measurements with tropospheric delay.
class	RangeTroposphericDelayModifier	Class modifying theoretical range measurement with tropospheric delay.
class	RelativisticClockInterSatellitesOneWayRangeRateModifier	Class modifying theoretical range-rate measurement with relativistic frequency deviation.
class	RelativisticClockInterSatellitesPhaseModifier	Class modifying theoretical inter-satellites phase measurement with relativistic clock correction.
class	RelativisticClockInterSatellitesRangeModifier	Class modifying theoretical inter-satellites range measurement with relativistic clock correction.
class	RelativisticClockOneWayGNSSPhaseModifier	Class modifying theoretical one-way GNSS phase measurement with relativistic clock correction.
class	RelativisticClockOneWayGNSSRangeModifier	Class modifying theoretical one-way GNSS range measurement with relativistic clock correction.
class	RelativisticClockOneWayGNSSRangeRateModifier	Class modifying theoretical range-rate measurement with relativistic frequency deviation.
class	RelativisticClockPhaseModifier	Class modifying theoretical phase measurement with relativistic clock correction.
class	RelativisticClockRangeModifier	Class modifying theoretical range measurement with relativistic clock correction.
class	RelativisticClockRangeRateModifier	Class modifying theoretical range-rate measurement with relativistic frequency deviation.
class	RelativisticJ2ClockInterSatellitesPhaseModifier	Class modifying theoretical inter-satellites phase measurements with relativistic J2 clock correction.
class	RelativisticJ2ClockInterSatellitesRangeModifier	Class modifying theoretical inter-satellites range measurements with relativistic J2 clock correction.
class	RelativisticJ2ClockOneWayGNSSPhaseModifier	Class modifying theoretical one-way phase measurements with relativistic J2 clock correction.
class	RelativisticJ2ClockOneWayGNSSRangeModifier	Class modifying one-way GNSS range theoretical measurements with relativistic J2 clock correction.
class	RelativisticJ2ClockPhaseModifier	Class modifying theoretical phase measurements with relativistic J2 clock correction.
class	RelativisticJ2ClockRangeModifier	Class modifying theoretical range measurements with relativistic J2 clock correction.
class	ShapiroInterSatellitePhaseModifier	Class modifying theoretical inter-satellites phase measurement with Shapiro time delay.
class	ShapiroInterSatelliteRangeModifier	Class modifying theoretical range measurement with Shapiro time delay.
class	ShapiroOneWayGNSSPhaseModifier	Class modifying theoretical one-way GNSS phase measurement with Shapiro time delay.
class	ShapiroOneWayGNSSRangeModifier	Class modifying theoretical range measurement with Shapiro time delay.
class	ShapiroPhaseModifier	Class modifying theoretical phase measurement with Shapiro time delay.
class	ShapiroRangeModifier	Class modifying theoretical range measurement with Shapiro time delay.
class	TDOAIonosphericDelayModifier	Class modifying theoretical TDOA measurements with ionospheric delay.
class	TDOATroposphericDelayModifier	Class modifying theoretical TDOA measurements with tropospheric delay.
class	TurnAroundRangeIonosphericDelayModifier	Class modifying theoretical TurnAroundRange measurement with ionospheric delay.
class	TurnAroundRangeTroposphericDelayModifier	Class modifying theoretical turn-around TurnAroundRange measurement with tropospheric delay.

Methods in org.orekit.estimation.measurements.modifiers with parameters of type ParameterDriversProvider

Modifier and Type	Method	Description
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, GroundStation station, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient)	Deprecated. as of 12.1, replaced by RangeModifierUtil.modify(EstimatedMeasurement, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient, EstimationModifier)
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, GroundStation station, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	RangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, GroundStation station, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient)	Deprecated. as of 12.1, replaced by RangeRateModifierUtil.modify(EstimatedMeasurement, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient, EstimationModifier)
static <T extends ObservedMeasurement<T>> void	RangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, GroundStation station, 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.forces

Modifier and Type	Interface	Description
interface	ForceModel	This interface represents a force modifying spacecraft motion.

Uses of ParameterDriversProvider in org.orekit.forces.drag

Classes in org.orekit.forces.drag that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractDragForceModel	Base class for drag force models.
class	DragForce	Atmospheric drag force model.
class	TimeSpanDragForce	Deprecated. as of 12.1

Uses of ParameterDriversProvider in org.orekit.forces.empirical

Subinterfaces of ParameterDriversProvider in org.orekit.forces.empirical

Modifier and Type	Interface	Description
interface	AccelerationModel	Acceleration model used by empirical force.

Classes in org.orekit.forces.empirical that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	HarmonicAccelerationModel	Harmonic acceleration model.
class	ParametricAcceleration	This class implements a parametric acceleration.
class	PolynomialAccelerationModel	Polynomial acceleration model.
class	TimeSpanParametricAcceleration	Time span parametric acceleration model.

Uses of ParameterDriversProvider in org.orekit.forces.gravity

Classes in org.orekit.forces.gravity that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractBodyAttraction	Abstract class for non-central body attraction force model.
class	DeSitterRelativity	De Sitter post-Newtonian correction force due to general relativity.
class	HolmesFeatherstoneAttractionModel	This class represents the gravitational field of a celestial body.
class	J2OnlyPerturbation	J2-only force model.
class	LenseThirringRelativity	Lense-Thirring post-Newtonian correction force due to general relativity.
class	NewtonianAttraction	Force model for Newtonian central body attraction.
class	OceanTides	Ocean tides force model.
class	Relativity	Post-Newtonian correction force due to general relativity.
class	SingleBodyAbsoluteAttraction	Body attraction force model computed as absolute acceleration towards a body.
class	SingleBodyRelativeAttraction	Body attraction force model computed as relative acceleration towards frame center.
class	SolidTides	Solid tides force model.
class	ThirdBodyAttraction	Third body attraction force model.
class	ThirdBodyAttractionEpoch	Third body attraction force model.

Uses of ParameterDriversProvider in org.orekit.forces.inertia

Classes in org.orekit.forces.inertia that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	InertialForces	Inertial force model.

Uses of ParameterDriversProvider in org.orekit.forces.maneuvers

Classes in org.orekit.forces.maneuvers that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	ConfigurableLowThrustManeuver	This class implements a configurable low thrust maneuver.
class	ConstantThrustManeuver	This class implements a simple maneuver with constant thrust.
class	Maneuver	A generic model for maneuvers with finite-valued acceleration magnitude, as opposed to instantaneous changes in the velocity vector which are defined via detectors (in ImpulseManeuver and FieldImpulseManeuver).

Uses of ParameterDriversProvider in org.orekit.forces.maneuvers.propulsion

Subinterfaces of ParameterDriversProvider in org.orekit.forces.maneuvers.propulsion

Modifier and Type	Interface	Description
interface	PropulsionModel	Generic interface for a propulsion model used in a Maneuver.
interface	ThrustPropulsionModel	Interface for a thrust-based propulsion model.

Classes in org.orekit.forces.maneuvers.propulsion that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractConstantThrustPropulsionModel	This abstract class simply serve as a container for a constant thrust maneuver.
class	BasicConstantThrustPropulsionModel	Constant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust norm or the flow rate.
class	ProfileThrustPropulsionModel	Thrust propulsion model based on segmented profile.
class	ScaledConstantThrustPropulsionModel	Thrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.

Uses of ParameterDriversProvider in org.orekit.forces.maneuvers.trigger

Subinterfaces of ParameterDriversProvider in org.orekit.forces.maneuvers.trigger

Modifier and Type	Interface	Description
interface	ManeuverTriggers	Generic interface for the maneuver triggers used in a Maneuver.

Classes in org.orekit.forces.maneuvers.trigger that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractManeuverTriggers	Base class for triggers.
class	DateBasedManeuverTriggers	Maneuver triggers based on a start and end date.
class	IntervalEventTrigger<T extends AbstractDetector<T>>	Maneuver triggers based on a single event detector that defines firing intervals.
class	StartStopEventsTrigger<A extends AbstractDetector<A>,O extends AbstractDetector<O>>	Maneuver triggers based on a pair of event detectors that defines firing start and stop.

Uses of ParameterDriversProvider in org.orekit.forces.radiation

Subinterfaces of ParameterDriversProvider in org.orekit.forces.radiation

Modifier and Type	Interface	Description
interface	RadiationForceModel	Interface for radiation-related force models.

Classes in org.orekit.forces.radiation that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractRadiationForceModel	Base class for radiation force models.
class	ECOM2	The Empirical CODE Orbit Model 2 (ECOM2) of the Center for Orbit Determination in Europe (CODE).
class	KnockeRediffusedForceModel	The Knocke Earth Albedo and IR emission force model.
class	RadiationPressureModel	Class representing a light-induced radiation pressure force, by leveraging on a given flux model.
class	SolarRadiationPressure	Solar radiation pressure force model.

Uses of ParameterDriversProvider in org.orekit.models.earth.ionosphere

Subinterfaces of ParameterDriversProvider in org.orekit.models.earth.ionosphere

Modifier and Type	Interface	Description
interface	IonosphericModel	Defines 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 ParameterDriversProvider

Modifier and Type	Class	Description
class	EstimatedIonosphericModel	An estimated ionospheric model.
class	GlobalIonosphereMapModel	Global Ionosphere Map (GIM) model.
class	KlobucharIonoModel	Klobuchar ionospheric delay model.
class	NeQuickModel	NeQuick ionospheric delay model.
class	SsrVtecIonosphericModel	Ionospheric model based on SSR IM201 message.

Uses of ParameterDriversProvider in org.orekit.models.earth.troposphere

Subinterfaces of ParameterDriversProvider in org.orekit.models.earth.troposphere

Modifier and Type	Interface	Description
interface	DiscreteTroposphericModel	Deprecated. as of 12.1, replaced by TroposphericModel
interface	TroposphericModel	Defines 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 ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractVienna	The Vienna tropospheric delay model for radio techniques.
class	AskneNordiusModel	The Askne Nordius model.
class	CanonicalSaastamoinenModel	The canonical Saastamoinen model.
class	ConstantTroposphericModel	Defines a constant tropospheric model.
class	EstimatedModel	An estimated tropospheric model.
class	EstimatedTroposphericModel	Deprecated. as of 12.1, replaced by EstimatedModel
class	FixedTroposphericDelay	A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.
class	MariniMurray	The Marini-Murray tropospheric delay model for laser ranging.
class	MariniMurrayModel	Deprecated. as of 12.1, replaced by MariniMurray
class	MendesPavlisModel	The Mendes - Pavlis tropospheric delay model for optical techniques.
class	ModifiedHopfieldModel	The modified Hopfield model.
class	ModifiedSaastamoinenModel	The modified Saastamoinen model.
class	SaastamoinenModel	Deprecated. as of 12.1, replaced by ModifiedSaastamoinenModel
class	TimeSpanEstimatedModel	Time span estimated tropospheric model.
class	TimeSpanEstimatedTroposphericModel	Deprecated. as of 12.1, replaced by TimeSpanEstimatedModel
class	TroposphericModelAdapter	Deprecated. temporary adapter to be removed when DiscreteTroposphericModel is removed
class	ViennaOne	The Vienna 1 tropospheric delay model for radio techniques.
class	ViennaOneModel	Deprecated. as of 12.1, replaced by ViennaOne
class	ViennaThree	The Vienna 3 tropospheric delay model for radio techniques.
class	ViennaThreeModel	Deprecated. as of 12.1, replaced by ViennaThree

Uses of ParameterDriversProvider in org.orekit.propagation.analytical

Classes in org.orekit.propagation.analytical that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractAnalyticalGradientConverter	Converter for analytical orbit propagator.
class	BrouwerLyddanePropagator	This class propagates a SpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
class	FieldAbstractAnalyticalPropagator<T extends CalculusFieldElement<T>>	Common handling of FieldPropagator methods for analytical propagators.
class	FieldBrouwerLyddanePropagator<T extends CalculusFieldElement<T>>	This class propagates a FieldSpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
class	FieldEcksteinHechlerPropagator<T extends CalculusFieldElement<T>>	This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
class	FieldKeplerianPropagator<T extends CalculusFieldElement<T>>	Simple Keplerian orbit propagator.

Uses of ParameterDriversProvider in org.orekit.propagation.analytical.intelsat

Classes in org.orekit.propagation.analytical.intelsat that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	FieldIntelsatElevenElementsPropagator<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 ParameterDriversProvider

Modifier and Type	Class	Description
class	FieldDeepSDP4<T extends CalculusFieldElement<T>>	This class contains the methods that compute deep space perturbation terms.
class	FieldSGP4<T extends CalculusFieldElement<T>>	This class contains methods to compute propagated coordinates with the SGP4 model.
class	FieldTLE<T extends CalculusFieldElement<T>>	This class is a container for a single set of TLE data.
class	FieldTLEPropagator<T extends CalculusFieldElement<T>>	This class provides elements to propagate TLE's.
class	TLE	This 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 ParameterDriversProvider

Modifier and Type	Class	Description
class	FieldIntegratedEphemeris<T extends CalculusFieldElement<T>>	This class stores sequentially generated orbital parameters for later retrieval.

Methods in org.orekit.propagation.integration with parameters of type ParameterDriversProvider

Modifier and Type	Method	Description
Gradient[]	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).
FieldSpacecraftState<Gradient>	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 ParameterDriversProvider

Modifier and Type	Class	Description
class	CR3BPForceModel	Class 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.forces

Modifier and Type	Interface	Description
interface	DSSTForceModel	This interface represents a force modifying spacecraft motion for a DSSTPropagator.

Classes in org.orekit.propagation.semianalytical.dsst.forces that implement ParameterDriversProvider

Modifier and Type	Class	Description
class	AbstractGaussianContribution	Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.
class	DSSTAtmosphericDrag	Atmospheric drag contribution to the DSSTPropagator.
class	DSSTJ2SquaredClosedForm	Second order J2-squared force model.
class	DSSTNewtonianAttraction	Force model for Newtonian central body attraction for the DSST propagator.
class	DSSTSolarRadiationPressure	Solar radiation pressure contribution to the DSSTPropagator.
class	DSSTTesseral	Tesseral contribution to the central body gravitational perturbation.
class	DSSTThirdBody	Third body attraction perturbation to the DSSTPropagator.
class	DSSTZonal	Zonal contribution to the central body gravitational perturbation.