SemiAnalyticalKalmanModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total32 of 1,77098%8 of 12693%101026340239
getCorrectedSpacecraftStates()90%n/a111111
getPredictedSpacecraftStates()80%n/a111111
processMeasurements(List, ExtendedKalmanFilter)65289%n/a0121001
getEvolution(double, RealVector, MeasurementDecorator)516897%1583%1413301
SemiAnalyticalKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider)434898%32790%31617701
getMeasurementMatrix()230100%11593%1904001
getErrorStateTransitionMatrix()154100%21688%21002401
computeOsculatingElements(RealVector)81100%4100%0301501
updateParameters()73100%6100%0401201
finalizeEstimation(ObservedMeasurement, ProcessEstimate)69100%1150%1201501
getPhysicalEstimatedState()68100%6100%0401201
getPhysicalMeasurementJacobian()56100%6100%0401101
getPhysicalKalmanGain()56100%6100%0401101
getPhysicalInnovationCovarianceMatrix()52100%6100%0401001
getPhysicalStateTransitionMatrix()49100%6100%0401001
updateReferenceTrajectory(DSSTPropagator)47100%2100%020801
getPhysicalEstimatedCovarianceMatrix()45100%4100%030701
normalizeCovarianceMatrix(RealMatrix)41100%4100%030701
initializeShortPeriodicTerms(SpacecraftState)36100%2100%020601
updateShortPeriods(SpacecraftState)28100%2100%020501
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix)12100%n/a010201
updateNominalSpacecraftState(SpacecraftState)10100%n/a010301
getEstimatedPropagator()7100%n/a010101
predictFilterCorrection(RealMatrix)5100%n/a010101
analyticalDerivativeComputations(SpacecraftState)5100%n/a010201
setObserver(KalmanObserver)4100%n/a010201
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