| electronDensity(DateTimeComponents, double, double, double, double) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| electronDensity(DateTimeComponents, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| clipExp(CalculusFieldElement) |  | 78% | | 75% | 1 | 3 | 1 | 5 | 0 | 1 |
| clipExp(double) | | 86% | | 75% | 1 | 3 | 1 | 5 | 0 | 1 |
| bottomElectronDensity(CalculusFieldElement, FieldNeQuickParameters) | | 100% | | 100% | 0 | 4 | 0 | 28 | 0 | 1 |
| bottomElectronDensity(double, NeQuickParameters) | | 100% | | 100% | 0 | 4 | 0 | 22 | 0 | 1 |
| topElectronDensity(CalculusFieldElement, FieldNeQuickParameters) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| flatten(double[][][]) | | 100% | | 100% | 0 | 4 | 0 | 7 | 0 | 1 |
| topElectronDensity(double, NeQuickParameters) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| pathDelay(FieldSpacecraftState, TopocentricFrame, FieldAbsoluteDate, double, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| pathDelay(SpacecraftState, TopocentricFrame, AbsoluteDate, double, double[]) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| electronDensity(FieldFourierTimeSeries, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| electronDensity(FourierTimeSeries, double, double, double) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| loadsIfNeeded(DateComponents) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| computeFourierTimeSeries(DateTimeComponents, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| computeFourierTimeSeries(DateTimeComponents, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| NeQuickModel(TimeScale) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| stec(AbsoluteDate, GeodeticPoint, GeodeticPoint) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| stec(FieldAbsoluteDate, FieldGeodeticPoint, FieldGeodeticPoint) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| pathDelay(SpacecraftState, TopocentricFrame, double, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| pathDelay(FieldSpacecraftState, TopocentricFrame, double, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getUtc() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |