acceleration(FieldSpacecraftState, CalculusFieldElement[]) |  | 100% | | n/a | 0 | 1 | 0 | 17 | 0 | 1 |
acceleration(SpacecraftState, double[]) |  | 100% | | n/a | 0 | 1 | 0 | 17 | 0 | 1 |
J2OnlyPerturbation(UnnormalizedSphericalHarmonicsProvider, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
J2OnlyPerturbation(double, double, double, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
J2OnlyPerturbation(double, double, TimeScalarFunction, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getJ2(AbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getJ2(FieldAbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMu() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getrEq() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
dependsOnPositionOnly() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |