SemiAnalyticalKalmanModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total32 of 1,75398%8 of 13293%101066324240
getCorrectedSpacecraftStates()90%n/a111111
getPredictedSpacecraftStates()80%n/a111111
processMeasurements(List, ExtendedKalmanFilter)65289%n/a0121001
getEvolution(double, RealVector, MeasurementDecorator)516997%1583%1413301
SemiAnalyticalKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider)438898%33592%32018001
getMeasurementMatrix()260100%11995%11104501
getErrorStateTransitionMatrix()154100%21688%21002401
updateParameters()115100%12100%0701501
getPhysicalEstimatedState()104100%12100%0701501
computeOsculatingElements(RealVector)81100%4100%0301501
finalizeEstimation(ObservedMeasurement, ProcessEstimate)69100%1150%1201501
updateReferenceTrajectory(DSSTPropagator)47100%2100%020801
initializeShortPeriodicTerms(SpacecraftState)38100%2100%020601
updateShortPeriods(SpacecraftState)28100%2100%020501
getNumberSelectedOrbitalDriversValuesToEstimate()22100%2100%020501
getNumberSelectedPropagationDriversValuesToEstimate()22100%2100%020501
getNumberSelectedMeasurementDriversValuesToEstimate()22100%2100%020501
getPhysicalMeasurementJacobian()17100%2100%020301
getPhysicalKalmanGain()17100%2100%020301
getPhysicalInnovationCovarianceMatrix()15100%2100%020301
getPhysicalStateTransitionMatrix()13100%2100%020201
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix)12100%n/a010201
updateNominalSpacecraftState(SpacecraftState)10100%n/a010301
getEstimatedPropagator()7100%n/a010101
getPhysicalEstimatedCovarianceMatrix()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
getObserver()100%n/a010101
getEstimate()100%n/a010101
finalizeOperationsObservationGrid()100%n/a010201
getEstimatedOrbitalParameters()100%n/a010101
getEstimatedPropagationParameters()100%n/a010101
getEstimatedMeasurementsParameters()100%n/a010101
getCurrentMeasurementNumber()100%n/a010101
getCurrentDate()100%n/a010101
getPredictedMeasurement()100%n/a010101
getCorrectedMeasurement()100%n/a010101