FieldAbstractAnalyticalPropagator.FieldBoundedPropagatorView(FieldAbstractAnalyticalPropagator, FieldAbsoluteDate, FieldAbsoluteDate) | | 63% | | 50% | 2 | 3 | 6 | 15 | 0 | 1 |
resetInitialState(FieldSpacecraftState) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
resetIntermediateState(FieldSpacecraftState, boolean) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
getFrame() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMass(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getInitialState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMinDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMaxDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |