expressCovarianceInDesiredOutput(Orbit, StateCovariance) | | 82% | | 75% | 1 | 3 | 1 | 10 | 0 | 1 |
AbstractStateCovarianceInterpolator(int, double, TimeInterpolator, LOFType) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
AbstractStateCovarianceInterpolator(int, double, TimeInterpolator, Frame, OrbitType, PositionAngleType) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
interpolate(AbstractTimeInterpolator.InterpolationData) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
buildOrbitList(List) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
interpolateOrbit(AbsoluteDate, List) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getOutFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOutLOF() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOutOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOutPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbitInterpolator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |