astro.equinoctial_2_classical#
- hohmannpy.astro.equinoctial_2_classical(sl_rectum, e_component1, e_component2, n_component1, n_component2, true_latitude)#
Converts the modified equinoctial orbital elements to the classical orbital elements.
- Parameters:
sl_rectum (float) – Semi-latus rectum.
e_component1 (float) – x-component of the eccentricity vector in the planet-centered inertial basis.
e_component2 (float) – y-component of the eccentricity vector in the planet-centered inertial basis.
n_component1 (float) – x-component of the nodal vector in the planet-centered inertial basis.
n_component2 (float) – y-component of the nodal vector in the planet-centered inertial basis.
true_latitude (float) – True latitude.
- Returns:
sm_axis (float) – Semi-major axis.
eccentricity (float) – Eccentricity.
raan (float) – Right ascension (longitude) of the ascending node.
argp (float) – Argument of periapsis.
inclination (float) – Inclination.
true_anomaly (float) – True anomaly.