Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 15 of 762 | 98% | 3 of 40 | 92% | 2 | 31 | 3 | 91 | 0 | 11 |
getJacobian(Orbit, PositionAngleType, double[][]) | 96% | 86% | 2 | 12 | 3 | 31 | 0 | 1 | ||
updateOrbit(Orbit) | 100% | 100% | 0 | 3 | 0 | 14 | 0 | 1 | ||
SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) | 100% | 100% | 0 | 3 | 0 | 17 | 0 | 1 | ||
evaluateJ0Dot() | 100% | 100% | 0 | 4 | 0 | 15 | 0 | 1 | ||
apply(SpacecraftState) | 100% | 100% | 0 | 2 | 0 | 4 | 0 | 1 | ||
apply(Orbit) | 100% | 100% | 0 | 2 | 0 | 3 | 0 | 1 | ||
SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
updateMass(double) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getDate() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getInertialFrame() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getInertialDV() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |