DSSTThirdBody

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 1,89699%0 of 22100%1271193116
getBody()0%n/a111111
updateShortPeriodTerms(CalculusFieldElement[], FieldSpacecraftState[])665100%8100%0505301
updateShortPeriodTerms(double[], SpacecraftState[])563100%8100%0505001
getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[])194100%n/a0102401
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[])157100%n/a0101401
initializeShortPeriodTerms(FieldAuxiliaryElements, PropagationType, CalculusFieldElement[])66100%n/a010901
DSSTThirdBody(CelestialBody, double)62100%n/a0101101
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[])56100%n/a010901
computeAoR3Pow(FieldDSSTThirdBodyDynamicContext)49100%2100%020701
computeAoR3Pow(DSSTThirdBodyDynamicContext)39100%2100%020601
initializeStaticContextIfNeeded(AuxiliaryElements, double, double, double[])16100%2100%020401
initializeStep(AuxiliaryElements, double[])8100%n/a010101
initializeStep(FieldAuxiliaryElements, CalculusFieldElement[])8100%n/a010101
static {...}100%n/a010101
getParametersDrivers()100%n/a010101
registerAttitudeProvider(AttitudeProvider)100%n/a010101