| checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList) |   | 31% | | 36% | 8 | 12 | 16 | 27 | 0 | 1 |
| getCorrectedSpacecraftStates() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| AbstractKalmanModel(List, List, ParameterDriversList, CovarianceMatrixProvider, AbstractJacobiansMapper[], PropagationType, PropagationType) | | 99% | | 92% | 5 | 36 | 0 | 129 | 0 | 1 |
| getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) | | 96% | | 75% | 1 | 3 | 1 | 10 | 0 | 1 |
| getMeasurementMatrix() | | 100% | | 90% | 2 | 12 | 0 | 42 | 0 | 1 |
| getEvolution(double, RealVector, MeasurementDecorator) | | 100% | | 100% | 0 | 9 | 0 | 37 | 0 | 1 |
| getErrorStateTransitionMatrix() | | 100% | | 90% | 2 | 11 | 0 | 24 | 0 | 1 |
| updateParameters() | | 100% | | 100% | 0 | 4 | 0 | 15 | 0 | 1 |
| getPhysicalEstimatedState() | | 100% | | 100% | 0 | 4 | 0 | 12 | 0 | 1 |
| predictState(AbsoluteDate) | | 100% | | 83% | 1 | 4 | 0 | 10 | 0 | 1 |
| applyDynamicOutlierFilter(EstimatedMeasurement, RealMatrix) | | 100% | | 100% | 0 | 4 | 0 | 13 | 0 | 1 |
| getPhysicalMeasurementJacobian() | | 100% | | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
| getPhysicalKalmanGain() | | 100% | | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
| getPhysicalInnovationCovarianceMatrix() | | 100% | | 100% | 0 | 4 | 0 | 10 | 0 | 1 |
| getPhysicalStateTransitionMatrix() | | 100% | | 100% | 0 | 4 | 0 | 10 | 0 | 1 |
| getPhysicalEstimatedCovarianceMatrix() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| finalizeEstimation(ObservedMeasurement, ProcessEstimate) | | 100% | | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
| normalizeCovarianceMatrix(RealMatrix) | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| getEstimatedPropagators() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| filterRelevant(ObservedMeasurement, SpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| AbstractKalmanModel(List, List, ParameterDriversList, CovarianceMatrixProvider, AbstractJacobiansMapper[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setReferenceTrajectories(Propagator[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setMappers(AbstractJacobiansMapper[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getPredictedSpacecraftStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getReferenceTrajectories() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMappers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCurrentMeasurementNumber() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCurrentDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPredictedMeasurement() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCorrectedMeasurement() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimatedOrbitalParameters() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimatedPropagationParameters() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimatedMeasurementsParameters() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getBuilders() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |