| initializeShortPeriodTerms(FieldAuxiliaryElements, PropagationType, CalculusFieldElement[]) |  | 92% |  | 66% | 1 | 3 | 1 | 12 | 0 | 1 |
| initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) | | 91% | | 66% | 1 | 3 | 1 | 12 | 0 | 1 |
| getProvider() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| computeMeanElementsTruncations(FieldAuxiliaryElements, CalculusFieldElement[], Field) | | 99% | | 95% | 1 | 11 | 1 | 60 | 0 | 1 |
| computeMeanElementsTruncations(AuxiliaryElements, double[]) | | 99% | | 95% | 1 | 11 | 1 | 59 | 0 | 1 |
| computeCijSijCoefficients(FieldAbsoluteDate, DSSTZonal.FieldSlot, DSSTZonal.FieldFourierCjSjCoefficients, CalculusFieldElement[][], FieldDSSTZonalContext, FieldAuxiliaryElements, Field, DSSTZonal.FieldUAnddU) | | 100% | | 82% | 5 | 15 | 0 | 130 | 0 | 1 |
| computeCijSijCoefficients(AbsoluteDate, DSSTZonal.Slot, DSSTZonal.FourierCjSjCoefficients, double[][], DSSTZonalContext, AuxiliaryElements, DSSTZonal.UAnddU) | | 100% | | 82% | 5 | 15 | 0 | 126 | 0 | 1 |
| computeMeanElementRates(FieldAbsoluteDate, FieldDSSTZonalContext, DSSTZonal.FieldUAnddU) | | 100% | | n/a | 0 | 1 | 0 | 19 | 0 | 1 |
| computeMeanElementRates(DSSTZonalContext, DSSTZonal.UAnddU) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| updateShortPeriodTerms(CalculusFieldElement[], FieldSpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
| updateShortPeriodTerms(double[], SpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| computeRhoSigmaCoefficients(DSSTZonal.FieldSlot, FieldAuxiliaryElements, Field) | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
| DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) | | 100% | | 100% | 0 | 2 | 0 | 16 | 0 | 1 |
| computeRhoSigmaCoefficients(DSSTZonal.Slot, AuxiliaryElements) | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| computeDiCoefficients(FieldAbsoluteDate, DSSTZonal.FieldSlot, FieldDSSTZonalContext, Field, DSSTZonal.FieldUAnddU) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| computeDiCoefficients(AbsoluteDate, DSSTZonal.Slot, DSSTZonalContext, DSSTZonal.UAnddU) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| checkIndexRange(int, int, int) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| DSSTZonal(UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isBetween(int, int, int) | | 100% | | 100% | 0 | 3 | 0 | 1 | 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 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| registerAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |