| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, PropagationType, double, double, int) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| resetInitialState(FieldSpacecraftState, PropagationType, double, int) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| resetIntermediateState(FieldSpacecraftState, boolean, double, int) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| resetIntermediateState(FieldSpacecraftState, boolean, OsculatingToMeanConverter) |  | 91% | | 50% | 1 | 2 | 1 | 10 | 0 | 1 |
| getM2(AbsoluteDate) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| resetInitialState(FieldSpacecraftState, PropagationType, OsculatingToMeanConverter) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, PropagationType, double, OsculatingToMeanConverter) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| computeMeanOrbit(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| computeMeanOrbit(FieldOrbit, double, double, double, double, double, double, double, OsculatingToMeanConverter) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, PropagationType, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, double, CalculusFieldElement, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| computeMeanOrbit(FieldOrbit, double, double, double, double, double, double, double, double, int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, double, CalculusFieldElement, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldBrouwerLyddanePropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| resetInitialState(FieldSpacecraftState, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| resetIntermediateState(FieldSpacecraftState, boolean) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| computeMeanOrbit(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMass(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| resetInitialState(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getM2() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |