| getState(ParameterDriversProvider) |  | 100% | | 100% | 0 | 7 | 0 | 47 | 0 | 1 |
| buildBasicGradientSpacecraftState(SpacecraftState, int, AttitudeProvider) | | 100% | | 100% | 0 | 6 | 0 | 30 | 0 | 1 |
| getParametersAtStateDate(FieldSpacecraftState, ParameterDriversProvider) | | 100% | | 100% | 0 | 6 | 0 | 14 | 0 | 1 |
| getParameters(FieldSpacecraftState, ParameterDriversProvider) | | 100% | | 100% | 0 | 5 | 0 | 16 | 0 | 1 |
| extend(FieldRotation, int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| extend(FieldVector3D, int) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| extend(Gradient, int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| extend(FieldAbsoluteDate, int) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| AbstractGradientConverter(int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| initStates(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getFreeStateParameters() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |