Calculates a rotation matrix from true ecliptic of date (ECT) to equator of date (EQD).
Details
This is one of the family of functions that returns a rotation matrix for converting from one orientation to another.
Source: ECT = true ecliptic of date.
Target: EQD = equator of date.
Examples
astro_rotation_ECT_EQD(Sys.time())
#> [,1] [,2] [,3]
#> [1,] 1 0.0000000 0.0000000
#> [2,] 0 0.9174887 0.3977619
#> [3,] 0 -0.3977619 0.9174887