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use crate;
/// Precession angles, IAU 2006 (Fukushima-Williams 4-angle formulation).
///
/// This function is part of the International Astronomical Union's
/// SOFA (Standards of Fundamental Astronomy) software collection.
///
/// Status: canonical model.
///
/// Given:
/// date1,date2 double TT as a 2-part Julian Date (Note 1)
///
/// Returned:
/// gamb double F-W angle gamma_bar (radians)
/// phib double F-W angle phi_bar (radians)
/// psib double F-W angle psi_bar (radians)
/// epsa double F-W angle epsilon_A (radians)
///
/// 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) Naming the following points:
///
/// e = J2000.0 ecliptic pole,
/// p = GCRS pole,
/// E = mean ecliptic pole of date,
/// and P = mean pole of date,
///
/// the four Fukushima-Williams angles are as follows:
///
/// gamb = gamma_bar = epE
/// phib = phi_bar = pE
/// psib = psi_bar = pEP
/// epsa = epsilon_A = EP
///
/// 3) The matrix representing the combined effects of frame bias and
/// precession is:
///
/// PxB = R_1(-epsa).R_3(-psib).R_1(phib).R_3(gamb)
///
/// 4) The matrix representing the combined effects of frame bias,
/// precession and nutation is simply:
///
/// NxPxB = R_1(-epsa-dE).R_3(-psib-dP).R_1(phib).R_3(gamb)
///
/// where dP and dE are the nutation components with respect to the
/// ecliptic of date.
///
/// Reference:
///
/// Hilton, J. et al., 2006, Celest.Mech.Dyn.Astron. 94, 351
///
/// Called:
/// iauObl06 mean obliquity, IAU 2006