DSSTThirdBody

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 1,68799%0 of 16100%1231167115
getBody()0%n/a111111
updateShortPeriodTerms(CalculusFieldElement[], FieldSpacecraftState[])641100%8100%0505001
updateShortPeriodTerms(double[], SpacecraftState[])537100%8100%0504701
getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[])176100%n/a0102201
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[])139100%n/a0101201
DSSTThirdBody(CelestialBody, double)59100%n/a0101001
initializeShortPeriodTerms(FieldAuxiliaryElements, PropagationType, CalculusFieldElement[])54100%n/a010901
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[])48100%n/a010901
initializeStep(AuxiliaryElements, double[])8100%n/a010101
initializeStep(FieldAuxiliaryElements, CalculusFieldElement[])8100%n/a010101
static {...}100%n/a010101
getParametersDrivers()100%n/a010101
getEventsDetectors()100%n/a010101
getFieldEventsDetectors(Field)100%n/a010101
registerAttitudeProvider(AttitudeProvider)100%n/a010101