accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D, FieldVector3D, FieldRotation, DerivativeStructure) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
accelerationDerivatives(SpacecraftState, String) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getParameter(String) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
setParameter(String, double) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody[]) |  | 100% |  | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody[]) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
addContribution(SpacecraftState, TimeDerivativesEquations) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEventsDetectors() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |