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.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 and 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 and 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 and Description
class	AbstractWindUp<T extends ObservedMeasurement<T>> Base class for wind-up effect computation.
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	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 and Description
class	AberrationModifier Class modifying theoretical angular measurement with (the inverse of) stellar aberration.
class	AngularIonosphericDelayModifier Class modifying theoretical angular measurement with ionospheric delay.
class	AngularRadioRefractionModifier Class modifying theoretical angular measurement with ionospheric radio refractive index.
class	AngularTroposphericDelayModifier Class modifying theoretical angular measurement with tropospheric delay.
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 Class modifying theoretical inter-satellites phase measurement with ambiguity.
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 Class modifying theoretical one-way GNSS phase measurement with ambiguity.
class	OutlierFilter<T extends ObservedMeasurement<T>> Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
class	PhaseAmbiguityModifier Class modifying theoretical phase measurement with ambiguity.
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	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	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 and Description
static <T extends ObservedMeasurement<T>> void	RangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, GroundStation station, org.orekit.estimation.measurements.modifiers.ParametricModelEffect modelEffect, org.orekit.estimation.measurements.modifiers.ParametricModelEffectGradient modelEffectGradient) Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, GroundStation station, org.orekit.estimation.measurements.modifiers.ParametricModelEffect modelEffect, org.orekit.estimation.measurements.modifiers.ParametricModelEffectGradient modelEffectGradient) 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 and 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 and Description
class	AbstractDragForceModel Base class for drag force models.
class	DragForce Atmospheric drag force model.
class	TimeSpanDragForce Time span atmospheric drag force model.

Uses of ParameterDriversProvider in org.orekit.forces.empirical

Subinterfaces of ParameterDriversProvider in org.orekit.forces.empirical

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

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

Modifier and Type	Class and 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 and Description
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	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 and 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 and 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 and 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 and 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 and 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 and 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

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

Modifier and Type	Class and 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	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 and 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 and 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 and Description
interface	DiscreteTroposphericModel 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 and Description
class	EstimatedTroposphericModel An estimated tropospheric model.
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	MariniMurrayModel The Marini-Murray tropospheric delay model for laser ranging.
class	MendesPavlisModel The Mendes - Pavlis tropospheric delay model for optical techniques.
class	SaastamoinenModel The modified Saastamoinen model.
class	TimeSpanEstimatedTroposphericModel Time span estimated tropospheric model.
class	ViennaOneModel The Vienna1 tropospheric delay model for radio techniques.
class	ViennaThreeModel The Vienna3 tropospheric delay model for radio techniques.

Uses of ParameterDriversProvider in org.orekit.propagation.analytical

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

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

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

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

Modifier and Type	Class and Description
class	FieldDeepSDP4<T extends org.hipparchus.CalculusFieldElement<T>> This class contains the methods that compute deep space perturbation terms.
class	FieldSGP4<T extends org.hipparchus.CalculusFieldElement<T>> This class contains methods to compute propagated coordinates with the SGP4 model.
class	FieldTLE<T extends org.hipparchus.CalculusFieldElement<T>> This class is a container for a single set of TLE data.
class	FieldTLEPropagator<T extends org.hipparchus.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 and Description
class	FieldIntegratedEphemeris<T extends org.hipparchus.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 and Description
org.hipparchus.analysis.differentiation.Gradient[]	AbstractGradientConverter.getParameters(FieldSpacecraftState<org.hipparchus.analysis.differentiation.Gradient> state, ParameterDriversProvider parametricModel) Get the parametric model parameters, return gradient values for each span of each driver (several gradient values for each parameter).
org.hipparchus.analysis.differentiation.Gradient[]	AbstractGradientConverter.getParametersAtStateDate(FieldSpacecraftState<org.hipparchus.analysis.differentiation.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<org.hipparchus.analysis.differentiation.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 and 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 and 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 and 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.