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

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.
Assembly	getAssembly() assembly getter
boolean	getFlagAlbedo() albedo getter
boolean	getFlagIr() infrared getter
Parameter	getK0Albedo() K0 albedo getter
Parameter	getK0Ir() K0 infrared getter
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 getter

Returns:

calculation indicator of the infrared force

initDerivatives

void initDerivatives()

derivatives initialisation

getK0Albedo

Parameter getK0Albedo()

K0 albedo getter

Returns:

albedo global multiplicative factor

getK0Ir

Parameter getK0Ir()

K0 infrared getter

Returns:

the infrared global multiplicative factor

getAssembly

Assembly getAssembly()

assembly getter

Returns:

assembly