| dependsOnPositionOnly() |  | 100% |  | 66% | 2 | 4 | 0 | 1 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getFieldEventDetectors(Field) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| init(FieldSpacecraftState, FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getEventDetectors() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| RadiationPressureModel(LightFluxModel, RadiationSensitive) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getRadiationSensitive() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLightFluxModel() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |