fr.cnes.sirius.patrius.propagation.numerical.multi

Class MultiPartialDerivativesEquations

java.lang.Object

fr.cnes.sirius.patrius.propagation.numerical.AbstractPartialDerivativesEquations

fr.cnes.sirius.patrius.propagation.numerical.multi.MultiPartialDerivativesEquations

All Implemented Interfaces:

AdditionalEquations, Externalizable, Serializable

public class MultiPartialDerivativesEquations
extends AbstractPartialDerivativesEquations

Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.

This set of equations are automatically added to a numerical propagator in order to compute partial derivatives of the orbit along with the orbit itself. This is useful for example in orbit determination applications.

Since:

4.5

Author:

Emmanuel Bignon

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description
MultiPartialDerivativesEquations() Empty constructor for Externalizable use.
MultiPartialDerivativesEquations(String nameIn, MultiNumericalPropagator propagatorIn, String satId) Simple constructor.

Method Summary

Modifier and Type	Method and Description
protected List<ForceModel>	getForceModels() Returns the propagator force models.
protected Frame	getFrame() Returns the propagator frame.
protected OrbitType	getOrbitType() Returns the propagator orbit type.
protected PositionAngle	getPositionAngle() Returns the propagator position angle.

Methods inherited from class fr.cnes.sirius.patrius.propagation.numerical.AbstractPartialDerivativesEquations

buildAdditionalState, clearSelectedParameters, computeDerivatives, computeSecondDerivatives, concatenate, contains, extractY, extractYDot, getAvailableParameters, getFirstOrderDimension, gethPos, getJacobiansProviders, getMapper, getName, getParamDim, getSecondOrderDimension, getSelectedParameters, isDirty, isInitialJacobians, readExternal, selectParamAndStep, selectParameters, selectParameters, setDirty, setHPos, setInitialJacobians, setInitialJacobians, setInitialJacobians, setInitialJacobians, setSteps, writeExternal

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Constructor Detail

MultiPartialDerivativesEquations

public MultiPartialDerivativesEquations()

Empty constructor for Externalizable use.

MultiPartialDerivativesEquations

public MultiPartialDerivativesEquations(String nameIn,
                                        MultiNumericalPropagator propagatorIn,
                                        String satId)

Simple constructor.

Upon construction, this set of equations is automatically added to the propagator by calling its NumericalPropagator.addAdditionalEquations(AdditionalEquations) method. So there is no need to call this method explicitly for these equations.

Parameters:

nameIn - name of the partial derivatives equations

propagatorIn - the propagator that will handle the orbit propagation

satId - satellite ID

Method Detail

getForceModels

protected List<ForceModel> getForceModels()

Returns the propagator force models.

Specified by:

getForceModels in class AbstractPartialDerivativesEquations

Returns:

the propagator force models

getFrame

protected Frame getFrame()

Returns the propagator frame.

Specified by:

getFrame in class AbstractPartialDerivativesEquations

Returns:

the propagator frame

getOrbitType

protected OrbitType getOrbitType()

Returns the propagator orbit type.

Specified by:

getOrbitType in class AbstractPartialDerivativesEquations

Returns:

the propagator orbit type

getPositionAngle

protected PositionAngle getPositionAngle()

Returns the propagator position angle.

Specified by:

getPositionAngle in class AbstractPartialDerivativesEquations

Returns:

the propagator position angle