SemiAnalyticalUnscentedKalmanModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total62 of 1,01293%9 of 5082%96210207037
updateParameters()284561%2466%2441201
getEvolution(double, RealVector[], MeasurementDecorator)1910784%2675%2532401
SemiAnalyticalUnscentedKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider)1522893%41881%41236001
getPhysicalEstimatedState()69100%6100%0401201
getPredictedMeasurements(RealVector[], MeasurementDecorator)66100%2100%020901
finalizeEstimation(ObservedMeasurement, ProcessEstimate)60100%1150%1201201
getInnovation(MeasurementDecorator, RealVector, RealVector, RealMatrix)57100%n/a0101001
processMeasurements(List, UnscentedKalmanFilter)53100%n/a010801
getStm()47100%n/a010901
initializeShortPeriodicTerms(SpacecraftState)36100%2100%020601
estimateMeasurement(ObservedMeasurement, int, SpacecraftState[])28100%n/a010801
updateShortPeriods(SpacecraftState)24100%2100%020401
updateNominalSpacecraftState(SpacecraftState)20100%n/a010401
toRealVector(SpacecraftState)17100%n/a010301
computeOsculatingElements(RealVector, SpacecraftState, RealVector)10100%n/a010201
getPredictedSpacecraftStates()8100%n/a010101
getCorrectedSpacecraftStates()8100%n/a010101
getEstimatedPropagator()5100%n/a010101
setObserver(KalmanObserver)4100%n/a010201
getPhysicalEstimatedCovarianceMatrix()4100%n/a010101
getPhysicalInnovationCovarianceMatrix()4100%n/a010101
getPhysicalKalmanGain()4100%n/a010101
getNumberSelectedOrbitalDrivers()4100%n/a010101
getNumberSelectedPropagationDrivers()4100%n/a010101
getNumberSelectedMeasurementDrivers()4100%n/a010101
getObserver()3100%n/a010101
getEstimate()3100%n/a010101
finalizeOperationsObservationGrid()3100%n/a010201
getEstimatedOrbitalParameters()3100%n/a010101
getEstimatedPropagationParameters()3100%n/a010101
getEstimatedMeasurementsParameters()3100%n/a010101
getCurrentMeasurementNumber()3100%n/a010101
getCurrentDate()3100%n/a010101
getPredictedMeasurement()3100%n/a010101
getCorrectedMeasurement()3100%n/a010101
getPhysicalStateTransitionMatrix()100%n/a010101
getPhysicalMeasurementJacobian()100%n/a010101