| lambda$addForceModel$0(CalculusFieldElement, double, ParameterDriver) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| addForceModel(ForceModel) |  | 92% | | 83% | 1 | 4 | 1 | 15 | 0 | 1 |
| resetInitialState(FieldSpacecraftState) | | 68% | | 50% | 1 | 2 | 1 | 5 | 0 | 1 |
| setMu(CalculusFieldElement) | | 73% | | 50% | 1 | 2 | 1 | 4 | 0 | 1 |
| removeForceModels() | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| initializeAttitudeProviderForDerivatives() | | 66% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| FieldNumericalPropagator(FieldODEIntegrator, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| hasNewtonianAttraction() | | 100% | | 75% | 1 | 3 | 0 | 2 | 0 | 1 |
| createMapper(FieldAbsoluteDate, CalculusFieldElement, OrbitParamsType, PositionAngleType, AttitudeProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldNumericalPropagator(FieldODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getMainStateEquations(FieldODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setIgnoreCentralAttraction(boolean) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| superSetMu(CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getAllForceModels() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setOrbitParamsType(OrbitParamsType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setPositionAngleType(PositionAngleType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setInitialState(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getOrbitParamsType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| superGetOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |