| computeElementaryFlux(FieldSpacecraftState, FieldVector3D, FieldVector3D, CalculusFieldElement) |   | 94% | | 75% | 1 | 3 | 1 | 23 | 0 | 1 |
| computeElementaryFlux(SpacecraftState, Vector3D, Vector3D, double) | | 92% | | 75% | 1 | 3 | 1 | 19 | 0 | 1 |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 4 | 0 | 28 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | 100% | 0 | 4 | 0 | 26 | 0 | 1 |
| computeCellArea(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, int) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| computeCellArea(double, double, double, double, int) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| computeAlbedo(FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| computeEmissivity(FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| computeNadirViewFactor(CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| computeAlbedo(AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| computeEmissivity(AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| computeNadirViewFactor(double, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| KnockeRediffusedForceModel(ExtendedPositionProvider, RadiationSensitive, double, double, TimeScale) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| computeSolarFlux(FieldVector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| computeSolarFlux(Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| KnockeRediffusedForceModel(ExtendedPositionProvider, RadiationSensitive, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| dependsOnPositionOnly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |