| addToRow(double[], int, int, double[][], double[][]) |   | 52% | | 50% | 2 | 4 | 2 | 6 | 0 | 1 |
| computeDerivatives(SpacecraftState, double[]) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| getSelectedParameters() | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| derivatives(SpacecraftState) | | 99% | | 94% | 1 | 10 | 0 | 53 | 0 | 1 |
| freezeParametersSelection() | | 100% | | 100% | 0 | 8 | 0 | 21 | 0 | 1 |
| setInitialJacobians(SpacecraftState, double[][], double[][]) | | 100% | | 75% | 2 | 5 | 0 | 13 | 0 | 1 |
| setInitialJacobians(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| EpochDerivativesEquations(String, NumericalPropagator) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| getMapper() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getDimension() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getName() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |