updateParameters() | | 61% | | 66% | 2 | 4 | 4 | 12 | 0 | 1 |
getEvolution(double, RealVector[], MeasurementDecorator) | | 84% | | 75% | 2 | 5 | 3 | 24 | 0 | 1 |
SemiAnalyticalUnscentedKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) | | 93% | | 81% | 4 | 12 | 3 | 60 | 0 | 1 |
getPhysicalEstimatedState() | | 100% | | 100% | 0 | 4 | 0 | 12 | 0 | 1 |
getPredictedMeasurements(RealVector[], MeasurementDecorator) | | 100% | | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
finalizeEstimation(ObservedMeasurement, ProcessEstimate) | | 100% | | 50% | 1 | 2 | 0 | 12 | 0 | 1 |
getInnovation(MeasurementDecorator, RealVector, RealVector, RealMatrix) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
processMeasurements(List, UnscentedKalmanFilter) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
getStm() | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
initializeShortPeriodicTerms(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
estimateMeasurement(ObservedMeasurement, int, SpacecraftState[]) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
updateShortPeriods(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
updateNominalSpacecraftState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
toRealVector(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
computeOsculatingElements(RealVector, SpacecraftState, RealVector) | | 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 |
getEstimatedPropagator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setObserver(KalmanObserver) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getPhysicalEstimatedCovarianceMatrix() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPhysicalInnovationCovarianceMatrix() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPhysicalKalmanGain() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNumberSelectedOrbitalDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNumberSelectedPropagationDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNumberSelectedMeasurementDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getObserver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEstimate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
finalizeOperationsObservationGrid() | | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
getPhysicalStateTransitionMatrix() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPhysicalMeasurementJacobian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |