resetInitialState(FieldSpacecraftState) | | 0% | | n/a | 1 | 1 | 8 | 8 | 1 | 1 |
computePVCoordinates() | | 98% | | 85% | 2 | 8 | 1 | 90 | 0 | 1 |
FieldTLEPropagator(FieldTLE, AttitudeProvider, CalculusFieldElement, CalculusFieldElement[]) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
resetIntermediateState(FieldSpacecraftState, boolean) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getTLE() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getFrame() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getMU() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
initializeCommons(CalculusFieldElement[]) | | 100% | | 100% | 0 | 3 | 0 | 68 | 0 | 1 |
selectExtrapolator(FieldTLE, AttitudeProvider, CalculusFieldElement, Frame, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
FieldTLEPropagator(FieldTLE, AttitudeProvider, CalculusFieldElement, Frame, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
selectExtrapolator(FieldTLE, Frame, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getPVCoordinates(FieldAbsoluteDate, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
selectExtrapolator(FieldTLE, AttitudeProvider, CalculusFieldElement, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
selectExtrapolator(FieldTLE, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMass(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |