initialize(FieldAuxiliaryElements, PropagationType, RealFieldElement[]) | | 93% | | 80% | 1 | 4 | 1 | 14 | 0 | 1 |
initialize(AuxiliaryElements, PropagationType, double[]) | | 91% | | 66% | 1 | 3 | 1 | 12 | 0 | 1 |
getProvider() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
computeMeanElementsTruncations(FieldAuxiliaryElements, RealFieldElement[], Field) | | 99% | | 95% | 1 | 11 | 0 | 59 | 0 | 1 |
computeMeanElementsTruncations(AuxiliaryElements, double[]) | | 99% | | 95% | 1 | 11 | 0 | 58 | 0 | 1 |
computeCijSijCoefficients(FieldAbsoluteDate, DSSTZonal.FieldSlot, DSSTZonal.FieldFourierCjSjCoefficients, RealFieldElement[][], 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(AbsoluteDate, DSSTZonalContext, DSSTZonal.UAnddU) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
updateShortPeriodTerms(RealFieldElement[], FieldSpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
computeRhoSigmaCoefficients(FieldAbsoluteDate, DSSTZonal.FieldSlot, FieldAuxiliaryElements, Field) | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
updateShortPeriodTerms(double[], SpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) | | 100% | | 100% | 0 | 2 | 0 | 17 | 0 | 1 |
computeRhoSigmaCoefficients(AbsoluteDate, 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, RealFieldElement[]) | | 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 |
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, RealFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFieldEventsDetectors(Field) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
registerAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |