| computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, double, OsculatingToMeanConverter) |  | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| resetIntermediateState(SpacecraftState, boolean, OsculatingToMeanConverter) |  | 89% | | 50% | 1 | 2 | 1 | 10 | 0 | 1 |
| resetInitialState(SpacecraftState, PropagationType, OsculatingToMeanConverter) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double, OsculatingToMeanConverter) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| getJacobiansColumnsNames() | | 100% | | 87% | 1 | 5 | 0 | 8 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| computeMeanOrbit(Orbit, double, double, double, double, double, double, double, OsculatingToMeanConverter) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double, double, int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| resetInitialState(SpacecraftState, PropagationType, double, int) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| resetIntermediateState(SpacecraftState, boolean, double, int) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| createHarvester(String, RealMatrix, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| propagateOrbit(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| resetInitialState(SpacecraftState, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| resetIntermediateState(SpacecraftState, boolean) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getMass(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getCk0() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getM2() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getReferenceRadius() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |