mubody.core.kepler.solve_kepler_equation#

mubody.core.kepler.solve_kepler_equation(n, e, TOF, E=0.1)#

Solves kepler equation iteratively

Parameters:

  • n (float) – Mean angular motion [rad/s]

  • e (float) – Orbit eccentricity [-]

  • E (float) – Eccentric anomaly, staring guess [rad]

Returns:

E – Eccentric anomaly, converged value [rad]

Return type:

float