| Package | Description |
|---|---|
| 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.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.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).
|
| Modifier and Type | Method and Description |
|---|---|
static <T extends ObservedMeasurement<T>> |
RangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated,
ParametersDriversProvider 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>> |
RangeModifierUtil.modify(EstimatedMeasurement<T> estimated,
ParametersDriversProvider 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.
|
| Modifier and Type | Interface and Description |
|---|---|
interface |
ForceModel
This interface represents a force modifying spacecraft motion.
|
| Modifier and Type | Class and Description |
|---|---|
class |
AbstractForceModel
Base class for force models.
|
| 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.
|
| Modifier and Type | Class and Description |
|---|---|
class |
ParametricAcceleration
This class implements a parametric acceleration.
|
class |
TimeSpanParametricAcceleration
Time span parametric acceleration model.
|
| 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.
|
| Modifier and Type | Class and Description |
|---|---|
class |
InertialForces
Inertial force model.
|
| 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.
|
| 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.
|
| 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.
|
| 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.
|
| 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.
|
| 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.
|
| Modifier and Type | Method and Description |
|---|---|
Gradient[] |
AbstractGradientConverter.getParameters(FieldSpacecraftState<Gradient> state,
ParametersDriversProvider parametricModel)
Get the parametric model parameters.
|
FieldSpacecraftState<Gradient> |
AbstractGradientConverter.getState(ParametersDriversProvider parametricModel)
Get the state with the number of parameters consistent with parametric model.
|
| Modifier and Type | Class and Description |
|---|---|
class |
CR3BPForceModel
Class calculating the acceleration induced by CR3BP model.
|
| Modifier and Type | Interface and Description |
|---|---|
interface |
DSSTForceModel
This interface represents a force modifying spacecraft motion for a
DSSTPropagator. |
| 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 |
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.
|
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