Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 21 of 109 | 80% | 0 of 0 | n/a | 1 | 10 | 3 | 20 | 1 | 10 |
acceleration(SpacecraftState, double[]) | 0% | n/a | 1 | 1 | 3 | 3 | 1 | 1 | ||
acceleration(FieldSpacecraftState, CalculusFieldElement[]) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
NewtonianAttraction(double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
getMu(Field, FieldAbsoluteDate) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
addContribution(SpacecraftState, TimeDerivativesEquations) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
getMu(AbsoluteDate) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
static {...} | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getParametersDrivers() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
dependsOnPositionOnly() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |