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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