Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 14 of 336 | 95% | 3 of 28 | 89% | 3 | 22 | 1 | 53 | 0 | 8 |
addMassDerivative(double) | ![]() ![]() | 52% | ![]() ![]() | 50% | 1 | 2 | 1 | 4 | 0 | 1 |
init(SpacecraftState, AbsoluteDate) | ![]() ![]() | 96% | ![]() ![]() | 80% | 2 | 6 | 0 | 10 | 0 | 1 |
computeDerivatives(SpacecraftState) | ![]() | 100% | ![]() | 100% | 0 | 4 | 0 | 13 | 0 | 1 |
addKeplerContribution(double) | ![]() | 100% | ![]() | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
NumericalPropagator.Main(NumericalPropagator, ODEIntegrator) | ![]() | 100% | ![]() | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
addNonKeplerianAcceleration(Vector3D) | ![]() | 100% | ![]() | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
lambda$new$0(ODEIntegrator, EventDetector) | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
lambda$init$1(SpacecraftState, AbsoluteDate, ForceModel) | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |