computeTesseral(int, int, int, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement[], CalculusFieldElement[], CalculusFieldElement[], CalculusFieldElement[], CalculusFieldElement[], CalculusFieldElement[]) |   | 63% |   | 62% | 4 | 9 | 9 | 32 | 0 | 1 |
accelerationWrtState(AbsoluteDate, Frame, FieldVector3D, DerivativeStructure) |   | 92% |   | 66% | 2 | 4 | 1 | 20 | 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 | 3 | 0 | 16 | 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 |