fr.cnes.sirius.patrius.forces.radiation

Interface RediffusedRadiationSensitive

All Superinterfaces:

JacobianParametersProvider

All Known Implementing Classes:

RediffusedRadiativeModel

public interface RediffusedRadiationSensitive
extends JacobianParametersProvider

rediffused radiative pressure interface

Since:

1.2

Version:

$Id: RediffusedRadiationSensitive.java 17582 2017-05-10 12:58:16Z bignon $

Author:

ClaudeD

Method Summary

Methods

Modifier and Type	Method and Description
void	addDAccDParamRediffusedRadiativePressure(SpacecraftState s, Parameter param, double[] dAccdParam) Compute acceleration derivatives.
void	addDAccDStateRediffusedRadiativePressure(SpacecraftState s, double[][] dAccdPos, double[][] dAccdVel) Compute acceleration derivatives.
boolean	getFlagAlbedo() albedo getter
boolean	getFlagIr() infrared setter
void	initDerivatives() derivatives initialisation
Vector3D	rediffusedRadiationPressureAcceleration(SpacecraftState state, ElementaryFlux flux) rediffused radiative pressure acceleration

Methods inherited from interface fr.cnes.sirius.patrius.propagation.numerical.JacobianParametersProvider

getJacobianParameters

Method Detail

rediffusedRadiationPressureAcceleration

Vector3D rediffusedRadiationPressureAcceleration(SpacecraftState state,
                                               ElementaryFlux flux)
                                                 throws PatriusException

rediffused radiative pressure acceleration

Parameters:

state - Spacecraft state

flux - elemantary flux

Returns:

acceleration

Throws:

PatriusException - OREKIT exception

Since:

1.2

addDAccDStateRediffusedRadiativePressure

void addDAccDStateRediffusedRadiativePressure(SpacecraftState s,
                                            double[][] dAccdPos,
                                            double[][] dAccdVel)
                                              throws PatriusException

Compute acceleration derivatives.

Parameters:

s - Spacecraft state.

dAccdPos - acceleration derivatives with respect to position

dAccdVel - acceleration derivatives with respect to velocity

Throws:

PatriusException - OREKIT exception

Since:

1.2

addDAccDParamRediffusedRadiativePressure

void addDAccDParamRediffusedRadiativePressure(SpacecraftState s,
                                            Parameter param,
                                            double[] dAccdParam)
                                              throws PatriusException

Compute acceleration derivatives.

Parameters:

s - Spacecraft state.

param - name of the parameter with respect to which derivatives are required

dAccdParam - acceleration derivatives with respect to specified parameters

Throws:

PatriusException - OREKIT exception

Since:

1.2

getFlagAlbedo

boolean getFlagAlbedo()

albedo getter

Returns:

calculation indicator of the albedo force

getFlagIr

boolean getFlagIr()

infrared setter

Returns:

calculation indicator of the infrared force

initDerivatives

void initDerivatives()

derivatives initialisation