getAdditionalState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
getStateCovariance(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
StateCovarianceMatrixProvider(String, String, MatricesHarvester, StateCovariance) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
toRealMatrix(double[]) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
toArray(RealMatrix) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
yields(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getStateCovariance(SpacecraftState, OrbitType, PositionAngleType) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getStateCovariance(SpacecraftState, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getName() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getCovarianceOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |