| min(double, CalculusFieldElement) |   | 46% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| max(double, CalculusFieldElement) | | 46% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getLightingRatio(FieldSpacecraftState, FieldVector3D) | | 98% | | 92% | 1 | 8 | 1 | 34 | 0 | 1 |
| getLightingRatio(SpacecraftState, Vector3D) | | 98% | | 92% | 1 | 8 | 1 | 31 | 0 | 1 |
| maskingRatio(OccultationEngine.FieldOccultationAngles) | | 100% | | 100% | 0 | 3 | 0 | 23 | 0 | 1 |
| maskingRatio(OccultationEngine.OccultationAngles) | | 100% | | 100% | 0 | 3 | 0 | 23 | 0 | 1 |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getLightingRatio(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLightingRatio(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| isSunCenteredFrame(Vector3D) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| SolarRadiationPressure(ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |