KalmanModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total5 of 1,82599%3 of 16298%41101313129
getCorrectedSpacecraftStates()0%n/a111111
KalmanModel(List, List, ParameterDriversList, CovarianceMatrixProvider)747100%27097%237013101
getMeasurementMatrix()246100%12195%11204001
getEvolution(double, RealVector, MeasurementDecorator)220100%18100%01003801
getErrorStateTransitionMatrix()159100%18100%01002001
updateParameters()79100%6100%0401501
getPhysicalEstimatedState()68100%6100%0401201
predictState(AbsoluteDate)65100%6100%0401001
updateReferenceTrajectories(Propagator[])41100%2100%020601
finalizeEstimation(ObservedMeasurement, ProcessEstimate)40100%2100%020901
getEstimatedPropagators()31100%2100%020401
getPhysicalMeasurementJacobian()17100%2100%020301
getPhysicalKalmanGain()17100%2100%020301
getPhysicalInnovationCovarianceMatrix()15100%2100%020301
getPhysicalStateTransitionMatrix()13100%2100%020201
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix)12100%n/a010201
getPhysicalEstimatedCovarianceMatrix()7100%n/a010101
setReferenceTrajectories(Propagator[])100%n/a010201
getPredictedSpacecraftStates()100%n/a010101
getReferenceTrajectories()100%n/a010101
getCurrentMeasurementNumber()100%n/a010101
getCurrentDate()100%n/a010101
getPredictedMeasurement()100%n/a010101
getCorrectedMeasurement()100%n/a010101
getEstimatedOrbitalParameters()100%n/a010101
getEstimatedPropagationParameters()100%n/a010101
getEstimatedMeasurementsParameters()100%n/a010101
getEstimate()100%n/a010101
getBuilders()100%n/a010101