AbstractGaussianContribution

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 855100%0 of 42100%0390128018
getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, RealFieldElement[])100100%10100%0601501
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[])91100%10100%0601401
computeRhoSigmaCoefficients(FieldAbsoluteDate, FieldAbstractGaussianContributionContext, Field)83100%2100%0201201
updateShortPeriodTerms(RealFieldElement[], FieldSpacecraftState[])81100%2100%0201101
updateShortPeriodTerms(double[], SpacecraftState[])67100%2100%020901
computeRhoSigmaCoefficients(AbsoluteDate, AuxiliaryElements)65100%2100%0201001
getMeanElementRate(FieldSpacecraftState, AbstractGaussianContribution.GaussQuadrature, RealFieldElement, RealFieldElement, FieldAbstractGaussianContributionContext, RealFieldElement[])51100%2100%020701
getRatesDiff(RealFieldElement[], RealFieldElement[], FieldAbstractGaussianContributionContext)45100%4100%030601
static {...}41100%n/a010301
getParametersDrivers()40100%2100%020801
getRatesDiff(double[], double[], AbstractGaussianContributionContext)40100%4100%030601
getMeanElementRate(SpacecraftState, AbstractGaussianContribution.GaussQuadrature, double, double, AbstractGaussianContributionContext, double[])39100%2100%020601
AbstractGaussianContribution(String, double, ForceModel, double)38100%n/a010901
initialize(FieldAuxiliaryElements, PropagationType, RealFieldElement[])30100%n/a010401
initialize(AuxiliaryElements, PropagationType, double[])28100%n/a010401
initializeStep(AuxiliaryElements, double[])6100%n/a010101
initializeStep(FieldAuxiliaryElements, RealFieldElement[])6100%n/a010101
registerAttitudeProvider(AttitudeProvider)4100%n/a010201