AbstractMatricesHarvester.java
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* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
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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;
import org.hipparchus.linear.MatrixUtils;
import org.hipparchus.linear.RealMatrix;
import org.orekit.orbits.PositionAngleType;
import org.orekit.utils.DoubleArrayDictionary;
/** Base harvester between two-dimensional Jacobian matrices and one-dimensional {@link
* SpacecraftState#getAdditionalState(String) additional state arrays}.
* @author Luc Maisonobe
* @since 11.1
*/
public abstract class AbstractMatricesHarvester implements MatricesHarvester {
/** Default state dimension, equivalent to position and velocity vectors. */
public static final int DEFAULT_STATE_DIMENSION = 6;
/** State Transition Matrix state name. */
private String stmName;
/** Initial State Transition Matrix. */
private RealMatrix initialStm;
/** Initial columns of the Jacobians matrix with respect to parameters. */
private DoubleArrayDictionary initialJacobianColumns;
/** Empty constructor.
* <p>
* This constructor is not strictly necessary, but it prevents spurious
* javadoc warnings with JDK 18 and later.
* </p>
* @since 14.0
*/
public AbstractMatricesHarvester() {
// nothing to do
}
/** Set the initial State Transition Matrix.
* <p>
* The arguments for initial matrices <em>must</em> be compatible with the
* {@link org.orekit.orbits.OrbitType orbit type} and
* {@link PositionAngleType position angle} that will be used by propagator,
* which may be different from input and output
* </p>
* @param name State Transition Matrix state name
* @param stm initial State Transition Matrix āY/āIā
* if null (which is the most frequent case), input and output
* orbit types are assumed to be identical and the matrix is
* assumed to be the 6x6 identity
*/
protected void setInitialStm(final String name, final RealMatrix stm) {
this.stmName = name;
this.initialStm = stm == null ?
MatrixUtils.createRealIdentityMatrix(DEFAULT_STATE_DIMENSION) :
stm;
}
/** Set the initial columns of the Jacobians matrix with respect to parameters.
* <p>
* The arguments for initial matrices <em>must</em> be compatible with the
* {@link org.orekit.orbits.OrbitType orbit type} and
* {@link PositionAngleType position angle} that will be used by propagator
* </p>
* @param initialJacobianColumns initial columns of the Jacobians matrix with respect to parameters,
* if null or if some selected parameters are missing from the dictionary, the corresponding
* initial column is assumed to be 0
*/
protected void setInitialJacobianColumns(final DoubleArrayDictionary initialJacobianColumns) {
this.initialJacobianColumns = initialJacobianColumns == null ?
new DoubleArrayDictionary() :
initialJacobianColumns;
}
/**
* Getter for the state dimension.
* @return state dimension
* @since 13.1
*/
public int getStateDimension() {
return initialStm.getColumnDimension();
}
/** Get the State Transition Matrix state name.
* @return State Transition Matrix state name
*/
public String getStmName() {
return stmName;
}
/** Get the initial State Transition Matrix.
* @return initial State Transition Matrix
*/
public RealMatrix getInitialStateTransitionMatrix() {
return initialStm;
}
/** Get the initial column of Jacobian matrix with respect to named parameter.
* @param columnName name of the column
* @return initial column of the Jacobian matrix
*/
public double[] getInitialJacobianColumn(final String columnName) {
final DoubleArrayDictionary.Entry entry = initialJacobianColumns.getEntry(columnName);
return entry == null ? new double[getStateDimension()] : entry.getValue();
}
/** Convert a flattened array to a square matrix.
* @param array input array
* @return the corresponding matrix
* @since 13.1
*/
public RealMatrix toSquareMatrix(final double[] array) {
final int stateDimension = getStateDimension();
final RealMatrix matrix = MatrixUtils.createRealMatrix(stateDimension, stateDimension);
int index = 0;
for (int i = 0; i < stateDimension; ++i) {
for (int j = 0; j < stateDimension; ++j) {
matrix.setEntry(i, j, array[index++]);
}
}
return matrix;
}
/** Set the STM data into an array.
* @param matrix STM matrix
* @return an array containing the STM data
* @since 13.1
*/
public double[] toArray(final double[][] matrix) {
final int stateDimension = matrix.length;
final double[] array = new double[stateDimension * stateDimension];
int index = 0;
for (final double[] row : matrix) {
for (int j = 0; j < stateDimension; ++j) {
array[index++] = row[j];
}
}
return array;
}
/** {@inheritDoc} */
@Override
public void setReferenceState(final SpacecraftState reference) {
// nothing to do
}
/** Freeze the names of the Jacobian columns.
* <p>
* This method is called when propagation starts, i.e. when configuration is completed
* </p>
*/
public abstract void freezeColumnsNames();
}