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kepler

Calculates the excentric anomaly E (Kepler element).

Calling Sequence

E = kepler(M, e)
E = kepler(M, e, E0)

Parameters

M

mean anomaly [rad]

e

exzentricity [ ] (0<e<1)

E0

Startwert of the iteration, approximation of the ex. anomaly (optional; if not given approximated with M) [rad]

E

exzentric anomaly [rad]

Description

Kepler equation:

Function for the iterative calculation of the excentric anomaly E. (stop criterion: 1e-10).

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