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 |
dependsOnPositionOnly() |  | 100% |  | 100% | 0 | 4 | 0 | 1 | 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 |
getRadiationSensitiveSpacecraft() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |