| gradientHessian(AbsoluteDate, Vector3D) |  | 100% | | 100% | 0 | 6 | 0 | 103 | 0 | 1 |
| gradient(AbsoluteDate, Vector3D) | | 100% | | 100% | 0 | 4 | 0 | 68 | 0 | 1 |
| nonCentralPart(AbsoluteDate, Vector3D) | | 100% |  | 83% | 1 | 4 | 0 | 37 | 0 | 1 |
| HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) | | 100% | | 100% | 0 | 5 | 0 | 24 | 0 | 1 |
| computeTesseral(int, int, int, double, double, double, double[], double[], double[], double[], double[], double[]) | | 100% | | 100% | 0 | 9 | 0 | 31 | 0 | 1 |
| createCosSinArrays(double, double) | | 100% | | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
| accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D, FieldVector3D, FieldRotation, DerivativeStructure) | | 100% | | 100% | 0 | 2 | 0 | 19 | 0 | 1 |
| accelerationDerivatives(SpacecraftState, String) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| createDistancePowersArray(double) | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| addContribution(SpacecraftState, TimeDerivativesEquations) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| value(AbsoluteDate, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setParameter(String, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getParameter(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getTideSystem() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |