Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 6 of 264 | 98% | 1 of 16 | 94% | 1 | 18 | 2 | 54 | 0 | 10 |
writeReplace() | 95% | 92% | 1 | 7 | 2 | 22 | 0 | 1 | ||
KeplerianPropagator(Orbit, AttitudeProvider, double, double) | 100% | n/a | 0 | 1 | 0 | 10 | 0 | 1 | ||
propagateOrbit(AbsoluteDate) | 100% | 100% | 0 | 2 | 0 | 4 | 0 | 1 | ||
resetIntermediateState(SpacecraftState, boolean) | 100% | 100% | 0 | 2 | 0 | 5 | 0 | 1 | ||
resetInitialState(SpacecraftState) | 100% | n/a | 0 | 1 | 0 | 4 | 0 | 1 | ||
KeplerianPropagator(Orbit) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
KeplerianPropagator(Orbit, AttitudeProvider) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
KeplerianPropagator(Orbit, double) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
KeplerianPropagator(Orbit, AttitudeProvider, double) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
getMass(AbsoluteDate) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |