rfa 0.5.9

A port ERFA to Rust.
Documentation 
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use super::{pnm00b::*, c2ibpn::*}; 
///  Form the celestial-to-intermediate matrix for a given date using the
///  IAU 2000B precession-nutation model.
///
///  Given:
///     date1,date2 double       TT as a 2-part Julian Date (Note 1)
///
///  Returned:
///     rc2i        double[3][3] celestial-to-intermediate matrix (Note 2)
///
/// # Notes:
///
///  1) The TT date date1+date2 is a Julian Date, apportioned in any
///     convenient way between the two arguments.  For example,
///     JD(TT)=2450123.7 could be expressed in any of these ways,
///     among others:
///
///     |    date1    |      date2   |                      |
///     |-------------|--------------|----------------------|
///     |2450123.7    |       0.0    |  (JD method)         |
///     |2451545.0    |   -1421.3    |  (J2000 method)      |
///     |2400000.5    |   50123.2    |  (MJD method)        |
///     |2450123.5    |       0.2    | (date & time method) |
///
///     The JD method is the most natural and convenient to use in
///     cases where the loss of several decimal digits of resolution
///     is acceptable.  The J2000 method is best matched to the way
///     the argument is handled internally and will deliver the
///     optimum resolution.  The MJD method and the date & time methods
///     are both good compromises between resolution and convenience.
///
///  2) The matrix rc2i is the first stage in the transformation from
///     celestial to terrestrial coordinates:
///
///        [TRS]  =  RPOM * R_3(ERA) * rc2i * [CRS]
///
///               =  rc2t * [CRS]
///
///     where [CRS] is a vector in the Geocentric Celestial Reference
///     System and [TRS] is a vector in the International Terrestrial
///     Reference System (see IERS Conventions 2003), ERA is the Earth
///     Rotation Angle and RPOM is the polar motion matrix.
///
///  3) The present function is faster, but slightly less accurate (about
///     1 mas), than the eraC2i00a function.
///
/// # Called:
///     eraPnm00b    classical NPB matrix, IAU 2000B
///     eraC2ibpn    celestial-to-intermediate matrix, given NPB matrix
///
/// # References:
///
///     "Expressions for the Celestial Intermediate Pole and Celestial
///     Ephemeris Origin consistent with the IAU 2000A precession-
///     nutation model", Astron.Astrophys. 400, 1145-1154
///     (2003)
///
///     n.b. The celestial ephemeris origin (CEO) was renamed "celestial
///          intermediate origin" (CIO) by IAU 2006 Resolution 2.
///
///     McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
///     IERS Technical Note No. 32, BKG (2004)
///
///  This revision:  2021 May 11
pub fn c2i00b(date1: f64, date2: f64, rc2i: &mut [[f64; 3]; 3])
{
    let mut rbpn = [[0.0; 3]; 3];
 
 
 /* Obtain the celestial-to-true matrix (IAU 2000B). */
    pnm00b(date1, date2, &mut rbpn);
 
 /* Form the celestial-to-intermediate matrix. */
    c2ibpn(date1, date2, &rbpn, rc2i);
 
 /* Finished. */
 
 }