Calculates the excentric anomaly E (Kepler element).
E = kepler(M, e) E = kepler(M, e, E0)
mean anomaly [rad]
exzentricity [ ]
(0<e<1)
Startwert of the iteration, approximation of the ex. anomaly
(optional; if not given approximated with M
)
[rad]
exzentric anomaly [rad]
Kepler equation:
Function for the iterative calculation of the excentric anomaly E. (stop criterion: 1e-10).
No warranty, there are no inputchecks.