Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 0 of 164 | 100% | 0 of 0 | n/a | 0 | 11 | 0 | 33 | 0 | 11 |
EphemerisSegmentPropagator(EphemerisFile.EphemerisSegment, AttitudeProvider) | 100% | n/a | 0 | 1 | 0 | 16 | 0 | 1 | ||
interpolate(AbsoluteDate) | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | ||
propagateOrbit(AbsoluteDate) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
getPosition(AbsoluteDate, Frame) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
getPVCoordinates(AbsoluteDate, Frame) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
resetIntermediateState(SpacecraftState, boolean) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
resetInitialState(SpacecraftState) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getInitialState() | 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 |