DSSTNewtonianAttraction

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total4 of 9995%0 of 0n/a115126115
getMu()40%n/a111111
getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[])28100%n/a010601
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[])22100%n/a010501
DSSTNewtonianAttraction(double)13100%n/a010301
initializeStep(AuxiliaryElements, double[])6100%n/a010101
initializeStep(FieldAuxiliaryElements, CalculusFieldElement[])6100%n/a010101
static {...}5100%n/a010101
getParametersDrivers()4100%n/a010101
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[])2100%n/a010101
initializeShortPeriodTerms(FieldAuxiliaryElements, PropagationType, CalculusFieldElement[])2100%n/a010101
getEventsDetectors()2100%n/a010101
getFieldEventsDetectors(Field)2100%n/a010101
registerAttitudeProvider(AttitudeProvider)1100%n/a010101
updateShortPeriodTerms(double[], SpacecraftState[])1100%n/a010101
updateShortPeriodTerms(CalculusFieldElement[], FieldSpacecraftState[])1100%n/a010101