StateMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
mapDoubleToDate(double, AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
mapArrayToState(double, double[], double[], PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
mapDoubleToDate(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
mapDateToDouble(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getReferenceDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAttitudeProvider() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |