| getMeasurementMatrix() |  | 100% |  | 95% | 1 | 12 | 0 | 45 | 0 | 1 |
| getErrorStateTransitionMatrix() | | 100% | | 100% | 0 | 15 | 0 | 38 | 0 | 1 |
| updateParameters() | | 100% | | 100% | 0 | 4 | 0 | 15 | 0 | 1 |
| predictState(AbsoluteDate) | | 100% | | 87% | 1 | 5 | 0 | 13 | 0 | 1 |
| getEvolution(double, RealVector, MeasurementDecorator) | | 100% | | 100% | 0 | 3 | 0 | 15 | 0 | 1 |
| updateReferenceTrajectories(Propagator[]) | | 100% | | 100% | 0 | 3 | 0 | 10 | 0 | 1 |
| finalizeEstimation(ObservedMeasurement, ProcessEstimate) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| getParametersJacobian(MatricesHarvester, SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| KalmanModel(List, List, ParameterDriversList, CovarianceMatrixProvider) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setReferenceTrajectories(Propagator[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getReferenceTrajectories() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |