| getReferenceDate() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| KalmanEstimationCommon(List, List, ParameterDriversList, CovarianceMatrixProvider) |  | 100% |  | 97% | 2 | 42 | 0 | 139 | 0 | 1 |
| getNormalizedProcessNoise(int) | | 100% | | 100% | 0 | 13 | 0 | 33 | 0 | 1 |
| getPhysicalEstimatedState() | | 100% | | 100% | 0 | 4 | 0 | 12 | 0 | 1 |
| getEstimatedPropagators() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getPhysicalMeasurementJacobian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getPhysicalKalmanGain() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getPhysicalInnovationCovarianceMatrix() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getPhysicalStateTransitionMatrix() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getPhysicalEstimatedCovarianceMatrix() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| incrementCurrentMeasurementNumber() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setCorrectedSpacecraftState(SpacecraftState, int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setPredictedSpacecraftState(SpacecraftState, int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getPredictedSpacecraftStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCorrectedSpacecraftStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setCorrectedEstimate(ProcessEstimate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setCurrentDate(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setPredictedMeasurement(EstimatedMeasurement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setCorrectedMeasurement(EstimatedMeasurement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
| getOrbitsStartColumns() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPropagationParameterColumns() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMeasurementParameterColumns() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimatedPropagationParametersArray() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimatedOrbitalParametersArray() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCovarianceIndirection() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getScale() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCorrectedEstimate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |