1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
use crate;
/// Form the celestial to intermediate-frame-of-date matrix for a given
/// date when the CIP X,Y coordinates are known. IAU 2000.
///
/// Given:
/// date1,date2 f64 TT as a 2-part Julian Date (Note 1)
/// x,y f64 Celestial Intermediate Pole (Note 2)
///
/// Returned (function value):
/// [[f64; 3]; 3] celestial-to-intermediate matrix (Note 3)
///
/// 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 Celestial Intermediate Pole coordinates are the x,y components
/// of the unit vector in the Geocentric Celestial Reference System.
///
/// 3) 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.
///
/// 4) Although its name does not include "00", This function is in fact
/// specific to the IAU 2000 models.
///
/// Called:
/// iauC2ixys celestial-to-intermediate matrix, given X,Y and s
/// iauS00 the CIO locator s, given X,Y, IAU 2000A
///
/// Reference:
///
/// McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
/// IERS Technical Note No. 32, BKG (2004)