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
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
use crate;
use crateanp;
use era00;
/// Greenwich mean sidereal time, IAU 2000
///
/// Greenwich mean sidereal time (model consistent with IAU 2000
/// resolutions).
///
/// This function is part of the International Astronomical Union's
/// SOFA (Standards of Fundamental Astronomy) software collection.
///
/// Status: canonical model.
///
/// Given:
/// ```
/// uta,utb double UT1 as a 2-part Julian Date (Notes 1,2)
/// tta,ttb double TT as a 2-part Julian Date (Notes 1,2)
/// ```
/// Returned (function value):
/// ```
/// double Greenwich mean sidereal time (radians)
/// ```
/// Notes:
///
/// 1) The UT1 and TT dates uta+utb and tta+ttb respectively, are both
/// Julian Dates, apportioned in any convenient way between the
/// argument pairs. For example, JD(UT1)=2450123.7 could be
/// expressed in any of these ways, among others:
/// ```
/// Part A Part B
///
/// 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 (in the case of UT; the TT is not at all critical
/// in this respect). The J2000 and MJD methods are good compromises
/// between resolution and convenience. For UT, the date & time
/// method is best matched to the algorithm that is used by the Earth
/// Rotation Angle function, called internally: maximum precision is
/// delivered when the uta argument is for 0hrs UT1 on the day in
/// question and the utb argument lies in the range 0 to 1, or vice
/// versa.
///
/// 2) Both UT1 and TT are required, UT1 to predict the Earth rotation
/// and TT to predict the effects of precession. If UT1 is used for
/// both purposes, errors of order 100 microarcseconds result.
///
/// 3) This GMST is compatible with the IAU 2000 resolutions and must be
/// used only in conjunction with other IAU 2000 compatible
/// components such as precession-nutation and equation of the
/// equinoxes.
///
/// 4) The result is returned in the range 0 to 2pi.
///
/// 5) The algorithm is from Capitaine et al. (2003) and IERS
/// Conventions 2003.
///
/// Called:
/// ```
/// iauEra00 Earth rotation angle, IAU 2000
/// iauAnp normalize angle into range 0 to 2pi
/// ```
/// References:
///
/// Capitaine, N., Wallace, P.T. and McCarthy, D.D., "Expressions to
/// implement the IAU 2000 definition of UT1", Astronomy &
/// Astrophysics, 406, 1135-1149 (2003)
///
/// McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
/// IERS Technical Note No. 32, BKG (2004)