computePVCoordinates() | | 97% | | 85% | 2 | 8 | 1 | 90 | 0 | 1 |
TLEPropagator(TLE, AttitudeProvider, double) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
initializeCommons() | | 100% | | 100% | 0 | 3 | 0 | 54 | 0 | 1 |
selectExtrapolator(TLE, AttitudeProvider, double, Frame) | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
TLEPropagator(TLE, AttitudeProvider, double, Frame) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
getJacobiansColumnsNames() | | 100% | | 87% | 1 | 5 | 0 | 8 | 0 | 1 |
resetIntermediateState(SpacecraftState, boolean) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
resetInitialState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
propagateOrbit(AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
resetTle(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
createHarvester(String, RealMatrix, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getPVCoordinates(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getMass(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDefaultTleGenerationAlgorithm(TimeScale, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
selectExtrapolator(TLE, AttitudeProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
initializeTle(TLE) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
selectExtrapolator(TLE, Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
selectExtrapolator(TLE) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getTLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMU() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |