| computeDerivatives(SpacecraftState, double[]) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| setInitialJacobians(SpacecraftState, double[][], double[][]) |  | 95% | | 61% | 6 | 10 | 0 | 17 | 0 | 1 |
| derivatives(SpacecraftState) | | 100% | | 100% | 0 | 8 | 0 | 48 | 0 | 1 |
| freezeParametersSelection() | | 100% | | 100% | 0 | 8 | 0 | 21 | 0 | 1 |
| setInitialJacobians(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| DSSTPartialDerivativesEquations(String, DSSTPropagator, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| getMapper() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| addToRow(double[], int, double[][]) | | 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 |