| acceleration(FieldSpacecraftState, CalculusFieldElement[]) |  | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| ParametricAcceleration(Vector3D, boolean, AttitudeProvider, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| ParametricAcceleration(Vector3D, boolean, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| ParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 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 |
| getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFieldEventsDetectors(Field) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |