| getCorrectedSpacecraftStates() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| setMappers(AbstractJacobiansMapper[]) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| getMappers() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| analyticalDerivativeComputations(AbstractJacobiansMapper, SpacecraftState) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| AbstractKalmanModel(List, List, ParameterDriversList, CovarianceMatrixProvider, MatricesHarvester[], PropagationType, PropagationType) |  | 100% |  | 97% | 2 | 37 | 0 | 134 | 0 | 1 |
| getMeasurementMatrix() | | 100% | | 95% | 1 | 12 | 0 | 40 | 0 | 1 |
| getEvolution(double, RealVector, MeasurementDecorator) | | 100% | | 100% | 0 | 10 | 0 | 38 | 0 | 1 |
| getErrorStateTransitionMatrix() | | 100% | | 100% | 0 | 10 | 0 | 20 | 0 | 1 |
| updateParameters() | | 100% | | 100% | 0 | 4 | 0 | 15 | 0 | 1 |
| getPhysicalEstimatedState() | | 100% | | 100% | 0 | 4 | 0 | 12 | 0 | 1 |
| predictState(AbsoluteDate) | | 100% | | 100% | 0 | 4 | 0 | 10 | 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 |
| getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| AbstractKalmanModel(List, List, ParameterDriversList, CovarianceMatrixProvider, MatricesHarvester[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setReferenceTrajectories(Propagator[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setHarvesters(MatricesHarvester[]) | | 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 |
| 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 |