AbstractGaussianContribution

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 839100%0 of 38100%0380130019
getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[])100100%10100%0601501
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[])91100%10100%0601401
computeRhoSigmaCoefficients(FieldAbsoluteDate, FieldAbstractGaussianContributionContext, Field)83100%2100%0201301
updateShortPeriodTerms(CalculusFieldElement[], FieldSpacecraftState[])81100%2100%0201301
updateShortPeriodTerms(double[], SpacecraftState[])67100%2100%0201001
computeRhoSigmaCoefficients(AbsoluteDate, AuxiliaryElements)65100%2100%0201001
getMeanElementRate(FieldSpacecraftState, AbstractGaussianContribution.GaussQuadrature, CalculusFieldElement, CalculusFieldElement, FieldAbstractGaussianContributionContext, CalculusFieldElement[])52100%2100%020701
static {...}41100%n/a010301
getMeanElementRate(SpacecraftState, AbstractGaussianContribution.GaussQuadrature, double, double, AbstractGaussianContributionContext, double[])39100%2100%020601
getRatesDiff(CalculusFieldElement[], CalculusFieldElement[], FieldAbstractGaussianContributionContext)39100%2100%020501
AbstractGaussianContribution(String, double, ForceModel, double)38100%n/a010901
getRatesDiff(double[], double[], AbstractGaussianContributionContext)36100%2100%020501
initializeShortPeriodTerms(FieldAuxiliaryElements, PropagationType, CalculusFieldElement[])30100%n/a010401
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[])28100%n/a010401
getParametersDrivers()27100%2100%020601
init(SpacecraftState, AbsoluteDate)6100%n/a010201
initializeStep(AuxiliaryElements, double[])6100%n/a010101
initializeStep(FieldAuxiliaryElements, CalculusFieldElement[])6100%n/a010101
registerAttitudeProvider(AttitudeProvider)4100%n/a010201