fr.cnes.sirius.patrius.stela.forces

Interface StelaForceModel

All Known Implementing Classes:

AbstractStelaGaussContribution, AbstractStelaLagrangeContribution, NonInertialContribution, SolidTidesAcc, SRPPotential, SRPSquaring, StelaAtmosphericDrag, StelaSRPSquaring, StelaTesseralAttraction, StelaThirdBodyAttraction, StelaZonalAttraction

public interface StelaForceModel

This interface represents a force modifying spacecraft motion for a StelaGTOPropagator.

Objects implementing this interface are intended to be added to a semianalytical Stela GTO propagator before the propagation is started.

Since:

1.3

Version:

$Id: StelaForceModel.java 18195 2017-10-13 11:49:12Z bignon $

Author:

Tiziana Sabatini

See Also:

ForceModel

Method Summary

Methods

Modifier and Type	Method and Description
double[][]	computePartialDerivatives(StelaEquinoctialOrbit orbit) Compute the partial derivatives for a given spacecraft state.
double[]	computeShortPeriods(StelaEquinoctialOrbit orbit) Compute the short periodic variations for a given spacecraft state.
String	getType()

Method Detail

computeShortPeriods

double[] computeShortPeriods(StelaEquinoctialOrbit orbit)
                             throws PatriusException

Compute the short periodic variations for a given spacecraft state.

Parameters:

orbit - current orbit information: date, kinematics

Returns:

the short periodic variations of the current force

Throws:

PatriusException - if short periods computation fails

computePartialDerivatives

double[][] computePartialDerivatives(StelaEquinoctialOrbit orbit)
                                     throws PatriusException

Compute the partial derivatives for a given spacecraft state.

Parameters:

orbit - current orbit information: date, kinematics

Returns:

the partial derivatives of the current force

Throws:

PatriusException - if partial derivatives computation fails

getType

String getType()

Returns:

the type