| computeTesseral(int, int, int, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement[], CalculusFieldElement[], CalculusFieldElement[], CalculusFieldElement[], CalculusFieldElement[], CalculusFieldElement[]) |   | 63% | | 62% | 4 | 9 | 9 | 32 | 0 | 1 |
| isDSConstantOrMuDerivative(CalculusFieldElement) | | 81% | | 70% | 2 | 6 | 2 | 9 | 0 | 1 |
| accelerationWrtState(AbsoluteDate, Frame, FieldVector3D, DerivativeStructure) | | 92% | | 66% | 2 | 4 | 1 | 20 | 0 | 1 |
| isGradientConstantOrMuDerivative(CalculusFieldElement) | | 92% | | 90% | 1 | 6 | 2 | 9 | 0 | 1 |
| isDSStateDerivative(FieldSpacecraftState) | | 98% | | 70% | 3 | 6 | 0 | 11 | 0 | 1 |
| isGradientStateDerivative(FieldSpacecraftState) | | 97% | | 62% | 3 | 5 | 0 | 10 | 0 | 1 |
| gradientHessian(AbsoluteDate, Vector3D, double) | | 100% | | 100% | 0 | 6 | 0 | 104 | 0 | 1 |
| gradient(FieldAbsoluteDate, FieldVector3D, CalculusFieldElement) | | 100% | | 100% | 0 | 4 | 0 | 90 | 0 | 1 |
| gradient(AbsoluteDate, Vector3D, double) | | 100% | | 100% | 0 | 4 | 0 | 68 | 0 | 1 |
| nonCentralPart(AbsoluteDate, Vector3D, double) | | 100% | | 100% | 0 | 4 | 0 | 38 | 0 | 1 |
| HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) | | 100% | | 100% | 0 | 6 | 0 | 26 | 0 | 1 |
| computeTesseral(int, int, int, double, double, double, double[], double[], double[], double[], double[], double[]) | | 100% | | 100% | 0 | 9 | 0 | 31 | 0 | 1 |
| createCosSinArrays(CalculusFieldElement, CalculusFieldElement) | | 100% | | 100% | 0 | 3 | 0 | 14 | 0 | 1 |
| accelerationWrtState(AbsoluteDate, Frame, FieldVector3D, Gradient) | | 100% | | 100% | 0 | 4 | 0 | 19 | 0 | 1 |
| createCosSinArrays(double, double) | | 100% | | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 6 | 0 | 17 | 0 | 1 |
| createDistancePowersArray(CalculusFieldElement) | | 100% | | 75% | 1 | 3 | 0 | 9 | 0 | 1 |
| createDistancePowersArray(double) | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| isVariable(DerivativeStructure, int) | | 100% | | 100% | 0 | 4 | 0 | 5 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| isVariable(Gradient, int) | | 100% | | 100% | 0 | 4 | 0 | 5 | 0 | 1 |
| value(AbsoluteDate, Vector3D, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTideSystem() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| dependsOnPositionOnly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |