pub fn teme2ecef(
rteme: (f64, f64, f64),
vteme: (f64, f64, f64),
ateme: (f64, f64, f64),
ttt: f64,
jdut1: f64,
lod: f64,
xp: f64,
yp: f64,
eqeterms: i32,
) -> Option<((f64, f64, f64), (f64, f64, f64), (f64, f64, f64))>Expand description
Convert a state from TEME to an ECI-like frame (precession+nutation applied).
Inputs are tuples (x,y,z) for position, velocity and acceleration (units: km, km/s, km/s^2
or km/min depending on caller conventions). ttt is Julian centuries from J2000
(TT) and ddpsi, ddeps are optional small nutation corrections.
Returns Some((reci, veci, aeci)) on success.