Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 62 of 294 | 78% | 2 of 22 | 90% | 2 | 18 | 8 | 47 | 0 | 7 |
addKeplerContribution(double) | ![]() ![]() | 27% | ![]() ![]() | 75% | 1 | 3 | 7 | 11 | 0 | 1 |
addMassDerivative(double) | ![]() ![]() | 52% | ![]() ![]() | 50% | 1 | 2 | 1 | 4 | 0 | 1 |
computeDerivatives(SpacecraftState) | ![]() | 100% | ![]() | 100% | 0 | 4 | 0 | 13 | 0 | 1 |
NumericalPropagator.Main(NumericalPropagator, ODEIntegrator) | ![]() | 100% | ![]() | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
addNonKeplerianAcceleration(Vector3D) | ![]() | 100% | ![]() | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
init(SpacecraftState, AbsoluteDate) | ![]() | 100% | ![]() | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
lambda$new$0(ODEIntegrator, EventDetector) | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |