Package | Description |
---|---|
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.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 | Interface and Description |
---|---|
interface |
ForceModel
This interface represents a force modifying spacecraft motion.
|
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 with finite-valued acceleration magnitude, as opposed to instantaneous changes
in the velocity vector which are defined via detectors (in
ImpulseManeuver and
FieldImpulseManeuver ). |
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.
|
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.
|
Modifier and Type | Interface and Description |
---|---|
interface |
ManeuverTriggers
Generic interface for the maneuver triggers used in a
Maneuver . |
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.
|
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 | 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 |
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.
|
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