fr.cnes.sirius.patrius.math.parameter

Interface IJacobiansParameterizable

All Superinterfaces:

IParameterizable, Serializable

All Known Implementing Classes:

AbstractTides, BalminoAttractionModel, ConstantThrustError, ContinuousThrustManeuver, CoriolisRelativisticEffect, CunninghamAttractionModel, DragForce, EmpiricalForce, Jacobianizer, JacobiansParameterizable, LenseThirringRelativisticEffect, NewtonianAttraction, OceanTides, RediffusedRadiationPressure, SchwarzschildRelativisticEffect, SolarRadiationPressureCircular, SolarRadiationPressureEllipsoid, TerrestrialTides, ThirdBodyAttraction, VariablePotentialAttractionModel

public interface IJacobiansParameterizable
extends IParameterizable

This class is used to define jacobian function parameters.

Since:

2.3

Version:

$Id: IJacobiansParameterizable.java 18069 2017-10-02 16:45:28Z bignon $

Author:

auguief

Concurrency :

not thread-safe, uses internal mutable attributes

Method Summary

Methods

Modifier and Type	Method and Description
void	addDAccDParam(SpacecraftState s, Parameter param, double[] dAccdParam) Compute acceleration derivatives with respect to additional parameters.
void	addDAccDState(SpacecraftState s, double[][] dAccdPos, double[][] dAccdVel) Compute acceleration derivatives with respect to state parameters.
boolean	supportsJacobianParameter(Parameter param) Check if a jacobian parameter is supported.

Methods inherited from interface fr.cnes.sirius.patrius.math.parameter.IParameterizable

getParameters, supportsParameter

Method Detail

addDAccDState

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

Compute acceleration derivatives with respect to state parameters.

Parameters:

s - spacecraft state

dAccdPos - acceleration derivatives with respect to position

dAccdVel - acceleration derivatives with respect to velocity

Throws:

PatriusException - if derivatives cannot be computed

addDAccDParam

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

Compute acceleration derivatives with respect to additional parameters.

Parameters:

s - spacecraft state

param - the parameter with respect to which derivatives are required

dAccdParam - acceleration derivatives with respect to specified parameters

Throws:

PatriusException - if derivatives cannot be computed

supportsJacobianParameter

boolean supportsJacobianParameter(Parameter param)

Check if a jacobian parameter is supported.

Parameters:

param - parameter to check

Returns:

true if the parameter is supported.