Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 18 of 189 | 90% | 0 of 0 | n/a | 2 | 12 | 4 | 24 | 2 | 12 |
getThrustVector(AbsoluteDate) | 0% | n/a | 1 | 1 | 3 | 3 | 1 | 1 | ||
getFlowRate(AbsoluteDate) | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
ScaledConstantThrustPropulsionModel(double, double, Vector3D, String) | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | ||
getThrustVector(CalculusFieldElement[]) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
getParametersDrivers() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getThrustVector(double, double, double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
getThrustVector() | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
getThrustVector(double[]) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getFlowRate(CalculusFieldElement[]) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
static {...} | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getFlowRate() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getFlowRate(double[]) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |