shiftedBy(Orbit, double) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, Frame, RealMatrix, OrbitType, PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, LOFType, RealMatrix, OrbitType, PositionAngle) | | 100% | | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
changeTypeAndCreate(Orbit, AbsoluteDate, Frame, OrbitType, PositionAngle, OrbitType, PositionAngle, RealMatrix) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
changeFrameAndCreate(Orbit, AbsoluteDate, LOFType, Frame, RealMatrix) | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
changeCovarianceType(Orbit, OrbitType, PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
changeCovarianceFrame(Orbit, LOFType) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
changeCovarianceFrame(Orbit, Frame) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getStm(Orbit, double) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
checkInputConsistency(Frame, OrbitType) | | 100% | | 100% | 0 | 4 | 0 | 6 | 0 | 1 |
StateCovariance(RealMatrix, AbsoluteDate, Frame, LOFType, OrbitType, PositionAngle) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
changeFrameAndCreate(Orbit, AbsoluteDate, LOFType, LOFType, RealMatrix) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
getJacobian(Transform) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
StateCovariance(RealMatrix, AbsoluteDate, LOFType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
StateCovariance(RealMatrix, AbsoluteDate, Frame, OrbitType, PositionAngle) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMatrix() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionAngle() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLOFType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |