Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 19 of 85 | 78% | 0 of 0 | n/a | 4 | 8 | 7 | 19 | 4 | 8 |
setParameter(String, double) | ![]() | 0% | n/a | 1 | 1 | 3 | 3 | 1 | 1 | |
getParameter(String) | ![]() | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
getMu() | ![]() | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
getEventsDetectors() | ![]() | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
accelerationDerivatives(SpacecraftState, String) | ![]() | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | |
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D, FieldVector3D, FieldRotation, DerivativeStructure) | ![]() | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
NewtonianAttraction(double) | ![]() | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
addContribution(SpacecraftState, TimeDerivativesEquations) | ![]() | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 |