stateChanged(FieldSpacecraftState) | | 90% | | 87% | 1 | 5 | 1 | 10 | 0 | 1 |
updateAdditionalStates(FieldSpacecraftState) | | 100% | | 100% | 0 | 3 | 0 | 10 | 0 | 1 |
initializePropagation() | | 100% | | 100% | 0 | 4 | 0 | 7 | 0 | 1 |
getManagedAdditionalStates() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
addAdditionalStateProvider(FieldAdditionalStateProvider) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
FieldAbstractPropagator(Field) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
isAdditionalStateManaged(String) | | 100% | | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
propagate(FieldAbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
resetInitialState(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getPVCoordinates(FieldAbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setStartDate(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalStateProviders() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getStartDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAttitudeProvider() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getField() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getInitialState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMultiplexer() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |