Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 14 of 118 | 88% | 0 of 6 | 100% | 2 | 13 | 2 | 22 | 2 | 10 |
getInitialState() | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
resetIntermediateState(SpacecraftState, boolean) | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
AggregateBoundedPropagator(Collection) | 100% | 100% | 0 | 3 | 0 | 10 | 0 | 1 | ||
getPropagator(AbsoluteDate) | 100% | 100% | 0 | 2 | 0 | 4 | 0 | 1 | ||
getPVCoordinates(AbsoluteDate, Frame) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
propagateOrbit(AbsoluteDate) | 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 | ||
getMass(AbsoluteDate) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
resetInitialState(SpacecraftState) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |