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use ;
use craterxr;
/// Form the matrix of precession/nutation for a given date, IAU 1976
/// precession model, IAU 1980 nutation model.
///
/// This function is part of the International Astronomical Union's
/// SOFA (Standards of Fundamental Astronomy) software collection.
///
/// Status: support function.
///
/// Given:
/// date1,date2 f64 TT as a 2-part Julian Date (Note 1)
///
/// Returned:
/// rmatpn f64[3][3] combined precession/nutation matrix
///
/// 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:
///
/// ```text
/// 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 operates in the sense V(date) = rmatpn * V(J2000),
/// where the p-vector V(date) is with respect to the true equatorial
/// triad of date date1+date2 and the p-vector V(J2000) is with
/// respect to the mean equatorial triad of epoch J2000.0.
///
/// References:
///
/// Explanatory Supplement to the Astronomical Almanac,
/// P. Kenneth Seidelmann (ed), University Science Books (1992),
/// Section 3.3 (p145).