Package | Description |
---|---|
org.orekit.propagation.semianalytical.dsst |
This package provides an implementation of the Draper Semi-analytical
Satellite Theory (DSST).
|
org.orekit.propagation.semianalytical.dsst.forces |
Modifier and Type | Method and Description |
---|---|
void |
DSSTPropagator.addForceModel(DSSTForceModel force)
Add a force model to the global perturbation model.
|
Modifier and Type | Method and Description |
---|---|
static SpacecraftState |
DSSTPropagator.computeMeanState(SpacecraftState osculating,
Collection<DSSTForceModel> forces)
Conversion from osculating to mean, orbit.
|
static SpacecraftState |
DSSTPropagator.computeOsculatingState(SpacecraftState mean,
Collection<DSSTForceModel> forces)
Conversion from mean to osculating orbit.
|
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 |
DSSTCentralBody
Central body gravitational contribution to the
DSSTPropagator . |
class |
DSSTSolarRadiationPressure
Solar radiation pressure contribution to the
DSSTPropagator . |
class |
DSSTThirdBody
Third body attraction perturbation to the
DSSTPropagator . |
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