getBody() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
updateShortPeriodTerms(CalculusFieldElement[], FieldSpacecraftState[]) | | 100% | | 100% | 0 | 5 | 0 | 50 | 0 | 1 |
updateShortPeriodTerms(double[], SpacecraftState[]) | | 100% | | 100% | 0 | 5 | 0 | 47 | 0 | 1 |
getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
DSSTThirdBody(CelestialBody, double) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
initializeShortPeriodTerms(FieldAuxiliaryElements, PropagationType, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) | | 100% | | n/a | 0 | 1 | 0 | 9 | 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 |
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 |