getReferenceDate() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
KalmanEstimationCommon(List, List, ParameterDriversList, CovarianceMatrixProvider) | | 100% | | 97% | 2 | 37 | 0 | 130 | 0 | 1 |
getNormalizedProcessNoise(int) | | 100% | | 100% | 0 | 8 | 0 | 24 | 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 |