KalmanModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total94 of 2,20495%25 of 21488%2013718390130
checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList)853931%14836%812162701
getCorrectedSpacecraftStates()0%n/a111111
KalmanModel(List, List, ParameterDriversList)67799%56392%535011701
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix)5396%1375%1311001
getMeasurementMatrix()253100%22090%21204201
getErrorStateTransitionMatrix()171100%21890%21102301
getEvolution(double, RealVector, MeasurementDecorator)164100%14100%0802801
updateParameters()79100%6100%0401501
getPhysicalEstimatedState()68100%6100%0401201
predictState(AbsoluteDate)65100%1583%1401001
applyDynamicOutlierFilter(EstimatedMeasurement, RealMatrix)58100%6100%0401301
getPhysicalMeasurementJacobian()56100%6100%0401101
getPhysicalKalmanGain()56100%6100%0401101
updateReferenceTrajectories(NumericalPropagator[])55100%2100%020901
getPhysicalInnovationCovarianceMatrix()52100%6100%0401001
getPhysicalStateTransitionMatrix()49100%6100%0401001
getPhysicalEstimatedCovarianceMatrix()45100%4100%030701
normalizeCovarianceMatrix(RealMatrix)41100%4100%030701
finalizeEstimation(ObservedMeasurement, ProcessEstimate)41100%2100%020901
getEstimatedPropagators()32100%2100%020401
filterRelevant(ObservedMeasurement, SpacecraftState[])27100%2100%020501
getPredictedSpacecraftStates()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