line |
stmt |
bran |
cond |
sub |
pod |
time |
code |
1
|
|
|
|
|
|
|
/* |
2
|
|
|
|
|
|
|
*+ |
3
|
|
|
|
|
|
|
* Name: |
4
|
|
|
|
|
|
|
* palRverot |
5
|
|
|
|
|
|
|
|
6
|
|
|
|
|
|
|
* Purpose: |
7
|
|
|
|
|
|
|
* Velocity component in a given direction due to Earth rotation |
8
|
|
|
|
|
|
|
|
9
|
|
|
|
|
|
|
* Language: |
10
|
|
|
|
|
|
|
* Starlink ANSI C |
11
|
|
|
|
|
|
|
|
12
|
|
|
|
|
|
|
* Type of Module: |
13
|
|
|
|
|
|
|
* Library routine |
14
|
|
|
|
|
|
|
|
15
|
|
|
|
|
|
|
* Invocation: |
16
|
|
|
|
|
|
|
* double palRverot ( double phi, double ra, double da, double st ); |
17
|
|
|
|
|
|
|
|
18
|
|
|
|
|
|
|
* Arguments: |
19
|
|
|
|
|
|
|
* phi = double (Given) |
20
|
|
|
|
|
|
|
* latitude of observing station (geodetic) (radians) |
21
|
|
|
|
|
|
|
* ra = double (Given) |
22
|
|
|
|
|
|
|
* apparent RA (radians) |
23
|
|
|
|
|
|
|
* da = double (Given) |
24
|
|
|
|
|
|
|
* apparent Dec (radians) |
25
|
|
|
|
|
|
|
* st = double (Given) |
26
|
|
|
|
|
|
|
* Local apparent sidereal time. |
27
|
|
|
|
|
|
|
|
28
|
|
|
|
|
|
|
* Returned Value: |
29
|
|
|
|
|
|
|
* palRverot = double |
30
|
|
|
|
|
|
|
* Component of Earth rotation in direction RA,DA (km/s). |
31
|
|
|
|
|
|
|
* The result is +ve when the observatory is receding from the |
32
|
|
|
|
|
|
|
* given point on the sky. |
33
|
|
|
|
|
|
|
|
34
|
|
|
|
|
|
|
* Description: |
35
|
|
|
|
|
|
|
* Calculate the velocity component in a given direction due to Earth |
36
|
|
|
|
|
|
|
* rotation. |
37
|
|
|
|
|
|
|
* |
38
|
|
|
|
|
|
|
* The simple algorithm used assumes a spherical Earth, of |
39
|
|
|
|
|
|
|
* a radius chosen to give results accurate to about 0.0005 km/s |
40
|
|
|
|
|
|
|
* for observing stations at typical latitudes and heights. For |
41
|
|
|
|
|
|
|
* applications requiring greater precision, use the routine |
42
|
|
|
|
|
|
|
* palPvobs. |
43
|
|
|
|
|
|
|
|
44
|
|
|
|
|
|
|
* Authors: |
45
|
|
|
|
|
|
|
* PTW: Patrick T. Wallace |
46
|
|
|
|
|
|
|
* TIMJ: Tim Jenness (JAC, Hawaii) |
47
|
|
|
|
|
|
|
* {enter_new_authors_here} |
48
|
|
|
|
|
|
|
|
49
|
|
|
|
|
|
|
* History: |
50
|
|
|
|
|
|
|
* 2012-03-02 (TIMJ): |
51
|
|
|
|
|
|
|
* Initial version |
52
|
|
|
|
|
|
|
* Adapted with permission from the Fortran SLALIB library. |
53
|
|
|
|
|
|
|
* {enter_further_changes_here} |
54
|
|
|
|
|
|
|
|
55
|
|
|
|
|
|
|
* Copyright: |
56
|
|
|
|
|
|
|
* Copyright (C) 1995 Rutherford Appleton Laboratory |
57
|
|
|
|
|
|
|
* Copyright (C) 2012 Science and Technology Facilities Council. |
58
|
|
|
|
|
|
|
* All Rights Reserved. |
59
|
|
|
|
|
|
|
|
60
|
|
|
|
|
|
|
* Licence: |
61
|
|
|
|
|
|
|
* This program is free software; you can redistribute it and/or |
62
|
|
|
|
|
|
|
* modify it under the terms of the GNU General Public License as |
63
|
|
|
|
|
|
|
* published by the Free Software Foundation; either version 3 of |
64
|
|
|
|
|
|
|
* the License, or (at your option) any later version. |
65
|
|
|
|
|
|
|
* |
66
|
|
|
|
|
|
|
* This program is distributed in the hope that it will be |
67
|
|
|
|
|
|
|
* useful, but WITHOUT ANY WARRANTY; without even the implied |
68
|
|
|
|
|
|
|
* warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR |
69
|
|
|
|
|
|
|
* PURPOSE. See the GNU General Public License for more details. |
70
|
|
|
|
|
|
|
* |
71
|
|
|
|
|
|
|
* You should have received a copy of the GNU General Public License |
72
|
|
|
|
|
|
|
* along with this program; if not, write to the Free Software |
73
|
|
|
|
|
|
|
* Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, |
74
|
|
|
|
|
|
|
* MA 02110-1301, USA. |
75
|
|
|
|
|
|
|
|
76
|
|
|
|
|
|
|
* Bugs: |
77
|
|
|
|
|
|
|
* {note_any_bugs_here} |
78
|
|
|
|
|
|
|
*- |
79
|
|
|
|
|
|
|
*/ |
80
|
|
|
|
|
|
|
|
81
|
|
|
|
|
|
|
#include "pal.h" |
82
|
|
|
|
|
|
|
|
83
|
|
|
|
|
|
|
#include |
84
|
|
|
|
|
|
|
|
85
|
0
|
|
|
|
|
|
double palRverot ( double phi, double ra, double da, double st ) { |
86
|
|
|
|
|
|
|
|
87
|
|
|
|
|
|
|
/* Nominal mean sidereal speed of Earth equator in km/s (the actual |
88
|
|
|
|
|
|
|
* value is about 0.4651) */ |
89
|
|
|
|
|
|
|
const double espeed = 0.4655; |
90
|
0
|
|
|
|
|
|
return espeed * cos(phi) * sin(st-ra) * cos(da); |
91
|
|
|
|
|
|
|
} |