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 |