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use craterz;
use pmat06;
/// This function forms three Euler angles which implement general
/// precession from epoch J2000.0, using the IAU 2006 model. Frame
/// bias (the offset between ICRS and mean J2000.0) is included.
///
/// This function is part of the International Astronomical Union's
/// SOFA (Standards of Fundamental Astronomy) software collection.
///
/// Status: support function.
///
/// Given:
/// date1,date2 double TT as a 2-part Julian Date (Note 1)
///
/// Returned (function value):
/// (bzeta, bz, btheta) (f64, f64, f64)
/// bzeta 1st rotation: radians cw around z
/// bz 3rd rotation: radians cw around z
/// btheta 2nd rotation: radians ccw around y
///
/// 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 traditional accumulated precession angles zeta_A, z_A,
/// theta_A cannot be obtained in the usual way, namely through
/// polynomial expressions, because of the frame bias. The latter
/// means that two of the angles undergo rapid changes near this
/// date. They are instead the results of decomposing the
/// precession-bias matrix obtained by using the Fukushima-Williams
/// method, which does not suffer from the problem. The
/// decomposition returns values which can be used in the
/// conventional formulation and which include frame bias.
///
/// 3) The three angles are returned in the conventional order, which
/// is not the same as the order of the corresponding Euler
/// rotations. The precession-bias matrix is
/// R_3(-z) x R_2(+theta) x R_3(-zeta).
///
/// 4) Should zeta_A, z_A, theta_A angles be required that do not
/// contain frame bias, they are available by calling the SOFA
/// function iauP06e.
///
/// Called:
/// iauPmat06 PB matrix, IAU 2006
/// iauRz rotate around Z-axis