Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 16 of 107 | 85% | 0 of 6 | 100% | 1 | 9 | 2 | 23 | 1 | 6 |
getIsp(SpacecraftState) | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | ||
getAcceleration(FieldSpacecraftState, FieldAttitude, CalculusFieldElement[]) | 100% | 100% | 0 | 2 | 0 | 7 | 0 | 1 | ||
getAcceleration(SpacecraftState, Attitude, double[]) | 100% | 100% | 0 | 2 | 0 | 7 | 0 | 1 | ||
getDirection(SpacecraftState) | 100% | 100% | 0 | 2 | 0 | 5 | 0 | 1 | ||
getMassDerivatives(SpacecraftState, double[]) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getMassDerivatives(FieldSpacecraftState, CalculusFieldElement[]) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |