Class ThirdBodyAttractionEpoch

    • Method Detail

      • getDerivativesToEpoch

        public double[] getDerivativesToEpoch​(SpacecraftState s,
                                              double[] parameters)
        Compute derivatives of the state w.r.t epoch.
        Parameters:
        s - current state information: date, kinematics, attitude
        parameters - values of the force model parameters
        Returns:
        derivatives