| checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList) |   | 31% |   | 36% | 8 | 12 | 16 | 27 | 0 | 1 |
| unNormalizeStateVector(RealVector) |  | 0% |  | 0% | 2 | 2 | 5 | 5 | 1 | 1 |
| getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) |   | 86% |   | 75% | 1 | 3 | 3 | 12 | 0 | 1 |
| getEvolution(double, RealVector, MeasurementDecorator) |   | 96% |  | 100% | 0 | 8 | 2 | 29 | 0 | 1 |
| getPhysicalEstimatedState() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getPredictedSpacecraftStates() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getCorrectedSpacecraftStates() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getCurrentDate() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getPredictedMeasurement() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| Model(List, List, ParameterDriversList) |  | 99% |   | 89% | 7 | 35 | 0 | 117 | 0 | 1 |
| getMeasurementMatrix() |  | 100% |   | 90% | 2 | 12 | 0 | 42 | 0 | 1 |
| getErrorStateTransitionMatrix() |  | 100% |   | 90% | 2 | 11 | 0 | 23 | 0 | 1 |
| updateParameters() |  | 100% |  | 100% | 0 | 4 | 0 | 15 | 0 | 1 |
| predictState(AbsoluteDate) |  | 100% |   | 83% | 1 | 4 | 0 | 10 | 0 | 1 |
| applyDynamicOutlierFilter(EstimatedMeasurement, RealMatrix) |  | 100% |  | 100% | 0 | 4 | 0 | 13 | 0 | 1 |
| updateReferenceTrajectories(NumericalPropagator[]) |  | 100% |  | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
| normalizeCovarianceMatrix(RealMatrix) |  | 100% |  | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| unNormalizeCovarianceMatrix(RealMatrix) |  | 100% |  | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| finalizeEstimation(ObservedMeasurement, ProcessEstimate) |  | 100% |  | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| getEstimatedPropagators() |  | 100% |  | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getPhysicalEstimatedCovarianceMatrix() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCurrentMeasurementNumber() | | 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 |