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use crate::;
use crate;
use crateir;
use crate;
use crate*;
use craterxr;
/// Frame bias and precession, IAU 2000.
///
/// Given:
/// * date1,date2 double TT as a 2-part Julian Date (Note 1)
///
/// Returned:
/// * rb frame bias matrix (Note 2)
/// * rp precession matrix (Note 3)
/// * rbp bias-precession matrix (Note 4)
///
/// # 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 rb transforms vectors from GCRS to mean J2000.0 by
/// applying frame bias.
///
/// 3) The matrix rp transforms vectors from J2000.0 mean equator and
/// equinox to mean equator and equinox of date by applying
/// precession.
///
/// 4) The matrix rbp transforms vectors from GCRS to mean equator and
/// equinox of date by applying frame bias then precession. It is
/// the product rp x rb.
///
/// 5) It is permissible to re-use the same array in the returned
/// arguments. The arrays are filled in the order given.
///
/// # Called:
/// * bi00 frame bias components, IAU 2000
/// * pr00 IAU 2000 precession adjustments
/// * ir initialize r-matrix to identity
/// * rx rotate around X-axis
/// * ry rotate around Y-axis
/// * rz rotate around Z-axis
/// * cr copy r-matrix
/// * rxr product of two r-matrices
///
/// # Reference:
/// * "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.
///
/// This revision: 2021 May 11