| getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[]) |  | 100% | | 100% | 0 | 6 | 0 | 15 | 0 | 1 |
| getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) | | 100% | | 100% | 0 | 6 | 0 | 14 | 0 | 1 |
| updateShortPeriodTerms(CalculusFieldElement[], FieldSpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
| computeRhoSigmaCoefficients(FieldAbsoluteDate, FieldAbstractGaussianContributionContext, Field) | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
| updateShortPeriodTerms(double[], SpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| computeRhoSigmaCoefficients(AbsoluteDate, AuxiliaryElements) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| getMeanElementRate(FieldSpacecraftState, AbstractGaussianContribution.GaussQuadrature, CalculusFieldElement, CalculusFieldElement, FieldAbstractGaussianContributionContext, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getMeanElementRate(SpacecraftState, AbstractGaussianContribution.GaussQuadrature, double, double, AbstractGaussianContributionContext, double[]) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| getRatesDiff(CalculusFieldElement[], CalculusFieldElement[], FieldAbstractGaussianContributionContext) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| AbstractGaussianContribution(String, double, ForceModel, double) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| getRatesDiff(double[], double[], AbstractGaussianContributionContext) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| initializeShortPeriodTerms(FieldAuxiliaryElements, PropagationType, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getParametersDrivers() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| init(FieldSpacecraftState, FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| initializeStep(AuxiliaryElements, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| initializeStep(FieldAuxiliaryElements, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| registerAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |