Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 68 of 144 | 53% | 6 of 12 | 50% | 9 | 16 | 18 | 35 | 6 | 10 |
basicPropagate(AbsoluteDate) | 66% | 60% | 2 | 6 | 8 | 18 | 0 | 1 | ||
resetIntermediateState(SpacecraftState, boolean) | 0% | 0% | 2 | 2 | 4 | 4 | 1 | 1 | ||
resetInitialState(SpacecraftState) | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | ||
propagateOrbit(AbsoluteDate) | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
getMass(AbsoluteDate) | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
getEffects() | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
getPropagator() | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
AdapterPropagator(Propagator) | 100% | n/a | 0 | 1 | 0 | 4 | 0 | 1 | ||
addEffect(AdapterPropagator.DifferentialEffect) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
getInitialState() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |