AbstractMeasurement

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total105 of 45877%7 of 1656%11321391624
AbstractMeasurement(AbsoluteDate, double, double, double, List, ParameterDriver[])350%20%225511
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List, ParameterDriver[])350%20%225511
AbstractMeasurement(AbsoluteDate, double, double, double, List)105384%1150%1221301
getPropagatorsIndices()90%n/a111111
lambda$new$1(Integer)60%n/a111111
lambda$new$0(Integer)60%n/a111111
lambda$getPropagatorsIndices$2(ObservableSatellite)40%n/a111111
getCoordinates(SpacecraftState, int, DSFactory)87100%n/a0101601
signalTimeOfFlight(TimeStampedFieldPVCoordinates, FieldVector3D, FieldAbsoluteDate)51100%1375%1301001
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate)44100%1375%1301001
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List)37100%n/a0101001
estimate(int, int, SpacecraftState[])23100%2100%020501
addModifier(EstimationModifier)12100%n/a010301
addParameterDriver(ParameterDriver)6100%n/a010201
getTheoreticalStandardDeviation()5100%n/a010101
getBaseWeight()5100%n/a010101
getObservedValue()5100%n/a010101
getParametersDrivers()4100%n/a010101
setEnabled(boolean)4100%n/a010201
getDimension()4100%n/a010101
getModifiers()4100%n/a010101
isEnabled()3100%n/a010101
getSatellites()3100%n/a010101
getDate()3100%n/a010101