fr.cnes.sirius.patrius.stela.propagation

Interface StelaAdditionalEquations

All Known Implementing Classes:

StelaAttitudeAdditionalEquations, StelaPartialDerivativesEquations

public interface StelaAdditionalEquations

Interface representing the Stela GTO propagator additional equations.

Since:

1.3

Version:

$Id$

Author:

Tiziana Sabatini

Method Summary

Modifier and Type	Method and Description
SpacecraftState	addInitialAdditionalState(SpacecraftState state)
void	computeDerivatives(StelaEquinoctialOrbit o, double[] p, double[] pDot) Compute the derivatives related to the additional state parameters.
int	getEquationsDimension()
String	getName() Get the name of the additional state.

Method Detail

getName

String getName()

Get the name of the additional state.

Returns:

name of the additional state

computeDerivatives

void computeDerivatives(StelaEquinoctialOrbit o,
                        double[] p,
                        double[] pDot)
                 throws PatriusException

Compute the derivatives related to the additional state parameters.

Parameters:

o - current orbit information: date, kinematics

p - current value of the additional parameters

pDot - placeholder where the derivatives of the additional parameters should be put

Throws:

PatriusException - if some specific error occurs

addInitialAdditionalState

SpacecraftState addInitialAdditionalState(SpacecraftState state)
                                   throws PatriusException

Parameters:

state - before adding additional state

Returns:

the initial additional state

Throws:

PatriusException - should not happen

getEquationsDimension

int getEquationsDimension()

Returns:

the additional equations dimension