checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList) | | 31% | | 36% | 8 | 12 | 16 | 27 | 0 | 1 |
getCorrectedSpacecraftStates() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
Model(List, List, ParameterDriversList) | | 99% | | 92% | 5 | 35 | 0 | 117 | 0 | 1 |
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) | | 96% | | 75% | 1 | 3 | 1 | 10 | 0 | 1 |
getMeasurementMatrix() | | 100% | | 90% | 2 | 12 | 0 | 42 | 0 | 1 |
getErrorStateTransitionMatrix() | | 100% | | 90% | 2 | 11 | 0 | 23 | 0 | 1 |
getEvolution(double, RealVector, MeasurementDecorator) | | 100% | | 100% | 0 | 8 | 0 | 27 | 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 |
updateReferenceTrajectories(NumericalPropagator[]) | | 100% | | 100% | 0 | 2 | 0 | 9 | 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 |
normalizeCovarianceMatrix(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 |
getPredictedSpacecraftStates() | | 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 |
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 |
getEstimate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |