AbstractJacobiansMapper.java
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*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
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package org.orekit.propagation.integration;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.numerical.NumericalPropagator;
import org.orekit.propagation.semianalytical.dsst.DSSTPropagator;
import org.orekit.utils.ParameterDriversList;
/** Base class for jacobian mapper.
* @author Bryan Cazabonne
* @since 10.0
*/
public abstract class AbstractJacobiansMapper {
/** State dimension, fixed to 6.
* @since 9.0
*/
public static final int STATE_DIMENSION = 6;
/** Name. */
private String name;
/** Selected parameters for Jacobian computation. */
private final ParameterDriversList parameters;
/** Simple constructor.
* @param name name of the Jacobians
* @param parameters selected parameters for Jacobian computation
*/
protected AbstractJacobiansMapper(final String name, final ParameterDriversList parameters) {
this.name = name;
this.parameters = parameters;
}
/** Get the name of the partial Jacobians.
* @return name of the Jacobians
*/
public String getName() {
return name;
}
/** Get the number of parameters.
* @return number of parameters
*/
public int getParameters() {
return parameters.getNbParams();
}
/** Compute the length of the one-dimensional additional state array needed.
* @return length of the one-dimensional additional state array
*/
public abstract int getAdditionalStateDimension();
/** Get the conversion Jacobian between state parameters and parameters used for derivatives.
* <p>
* For a {@link DSSTPropagator DSST propagator}, state parameters and parameters used for derivatives are the same,
* so the Jocabian is simply the identity.
* </p>
* <p>
* For {@link NumericalPropagator Numerical propagator}, parameters used for derivatives are cartesian
* and they can be different from state parameters because the numerical propagator can accept different type
* of orbits.
* </p>
* @param state spacecraft state
* @return conversion Jacobian
*/
protected abstract double[][] getConversionJacobian(SpacecraftState state);
/** Set the Jacobian with respect to state into a one-dimensional additional state array.
* @param state spacecraft state
* @param dY1dY0 Jacobian of current state at time t₁
* with respect to state at some previous time t₀
* @param dY1dP Jacobian of current state at time t₁
* with respect to parameters (may be null if there are no parameters)
* @param p placeholder where to put the one-dimensional additional state
* @see #getStateJacobian(SpacecraftState, double[][])
*/
public abstract void setInitialJacobians(SpacecraftState state, double[][] dY1dY0, double[][] dY1dP, double[] p);
/** Get the Jacobian with respect to state from a one-dimensional additional state array.
* <p>
* This method extract the data from the {@code state} and put it in the
* {@code dYdY0} array.
* </p>
* @param state spacecraft state
* @param dYdY0 placeholder where to put the Jacobian with respect to state
* @see #getParametersJacobian(SpacecraftState, double[][])
*/
public abstract void getStateJacobian(SpacecraftState state, double[][] dYdY0);
/** Get the Jacobian with respect to parameters from a one-dimensional additional state array.
* <p>
* This method extract the data from the {@code state} and put it in the
* {@code dYdP} array.
* </p>
* <p>
* If no parameters have been set in the constructor, the method returns immediately and
* does not reference {@code dYdP} which can safely be null in this case.
* </p>
* @param state spacecraft state
* @param dYdP placeholder where to put the Jacobian with respect to parameters
* @see #getStateJacobian(SpacecraftState, double[][])
*/
public abstract void getParametersJacobian(SpacecraftState state, double[][] dYdP);
}