Function astro::orbit::parabolic::true_anom_and_rad_vec [] [src]

pub fn true_anom_and_rad_vec(t: f64, T: f64, q: f64) -> (f64, f64)

Computes the true anomaly and radius vector of a body in a parabolic orbit at a given time

Returns

(tru_anom, rad_vec)

Arguments