Model

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total151 of 1,93792%29 of 18484%2811931340627
checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList)853931%14836%812162701
unNormalizeStateVector(RealVector)280%20%225511
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix)85386%1375%1331201
getEvolution(double, RealVector, MeasurementDecorator)616196%14100%0822901
getPhysicalEstimatedState()60%n/a111111
getPredictedSpacecraftStates()0%n/a111111
getCorrectedSpacecraftStates()0%n/a111111
getCurrentDate()0%n/a111111
getPredictedMeasurement()0%n/a111111
Model(List, List, ParameterDriversList)67799%76189%735011701
getMeasurementMatrix()253100%22090%21204201
getErrorStateTransitionMatrix()171100%21890%21102301
updateParameters()79100%6100%0401501
predictState(AbsoluteDate)65100%1583%1401001
applyDynamicOutlierFilter(EstimatedMeasurement, RealMatrix)58100%6100%0401301
updateReferenceTrajectories(NumericalPropagator[])55100%2100%020901
normalizeCovarianceMatrix(RealMatrix)41100%4100%030701
unNormalizeCovarianceMatrix(RealMatrix)41100%4100%030701
finalizeEstimation(ObservedMeasurement, ProcessEstimate)38100%2100%020801
getEstimatedPropagators()31100%2100%020401
getPhysicalEstimatedCovarianceMatrix()6100%n/a010101
getCurrentMeasurementNumber()100%n/a010101
getCorrectedMeasurement()100%n/a010101
getEstimatedOrbitalParameters()100%n/a010101
getEstimatedPropagationParameters()100%n/a010101
getEstimatedMeasurementsParameters()100%n/a010101
getEstimate()100%n/a010101