Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 0 of 191 | 100% | 0 of 0 | n/a | 0 | 7 | 0 | 31 | 0 | 7 |
accelerationDerivatives(SpacecraftState, String) | 100% | n/a | 0 | 1 | 0 | 7 | 0 | 1 | ||
addContribution(SpacecraftState, TimeDerivativesEquations) | 100% | n/a | 0 | 1 | 0 | 7 | 0 | 1 | ||
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D, FieldVector3D, FieldRotation, DerivativeStructure) | 100% | n/a | 0 | 1 | 0 | 7 | 0 | 1 | ||
ThirdBodyAttraction(CelestialBody) | 100% | n/a | 0 | 1 | 0 | 4 | 0 | 1 | ||
setParameter(String, double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
getParameter(String) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
getEventsDetectors() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |