Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 12 of 289 | 95% | 1 of 20 | 95% | 1 | 18 | 1 | 45 | 0 | 8 |
addMassDerivative(double) | 52% | 50% | 1 | 2 | 1 | 4 | 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 | 4 | 0 | 11 | 0 | 1 | ||
addNonKeplerianAcceleration(Vector3D) | 100% | 100% | 0 | 2 | 0 | 4 | 0 | 1 | ||
init(SpacecraftState, AbsoluteDate) | 100% | n/a | 0 | 1 | 0 | 2 | 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 |