| computeElementaryFlux(FieldSpacecraftState, FieldVector3D, FieldVector3D, OneAxisEllipsoid, CalculusFieldElement) |   | 94% | | 75% | 1 | 3 | 1 | 21 | 0 | 1 |
| computeElementaryFlux(SpacecraftState, Vector3D, Vector3D, OneAxisEllipsoid, double) | | 92% | | 75% | 1 | 3 | 1 | 18 | 0 | 1 |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 3 | 0 | 27 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | 100% | 0 | 3 | 0 | 24 | 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 |
| computeAlbedo(AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| computeEmissivity(AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 11 | 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 |