Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 48 of 124 | 61% | 2 of 8 | 75% | 7 | 14 | 12 | 29 | 6 | 10 |
resetIntermediateState(SpacecraftState, boolean) | ![]() | 0% | ![]() | 0% | 2 | 2 | 4 | 4 | 1 | 1 |
basicPropagate(AbsoluteDate) | ![]() ![]() | 88% | ![]() | 100% | 0 | 4 | 2 | 12 | 0 | 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 |