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 |