line |
stmt |
bran |
cond |
sub |
pod |
time |
code |
1
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/* |
2
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*+ |
3
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* Name: |
4
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* palAopqk |
5
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6
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* Purpose: |
7
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* Quick apparent to observed place |
8
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9
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* Language: |
10
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* Starlink ANSI C |
11
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12
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* Type of Module: |
13
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* Library routine |
14
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15
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* Invocation: |
16
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* void palAopqk ( double rap, double dap, const double aoprms[14], |
17
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* double *aob, double *zob, double *hob, |
18
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* double *dob, double *rob ); |
19
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20
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* Arguments: |
21
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* rap = double (Given) |
22
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* Geocentric apparent right ascension |
23
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* dap = double (Given) |
24
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* Geocentric apparent declination |
25
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* aoprms = const double [14] (Given) |
26
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* Star-independent apparent-to-observed parameters. |
27
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* |
28
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* [0] geodetic latitude (radians) |
29
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* [1,2] sine and cosine of geodetic latitude |
30
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* [3] magnitude of diurnal aberration vector |
31
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* [4] height (HM) |
32
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* [5] ambient temperature (T) |
33
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* [6] pressure (P) |
34
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* [7] relative humidity (RH) |
35
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* [8] wavelength (WL) |
36
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* [9] lapse rate (TLR) |
37
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* [10,11] refraction constants A and B (radians) |
38
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* [12] longitude + eqn of equinoxes + sidereal DUT (radians) |
39
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* [13] local apparent sidereal time (radians) |
40
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* aob = double * (Returned) |
41
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* Observed azimuth (radians: N=0,E=90) |
42
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* zob = double * (Returned) |
43
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* Observed zenith distance (radians) |
44
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* hob = double * (Returned) |
45
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* Observed Hour Angle (radians) |
46
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* dob = double * (Returned) |
47
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* Observed Declination (radians) |
48
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* rob = double * (Returned) |
49
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* Observed Right Ascension (radians) |
50
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51
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* Description: |
52
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* Quick apparent to observed place. |
53
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54
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* Authors: |
55
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* TIMJ: Tim Jenness (JAC, Hawaii) |
56
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* PTW: Patrick T. Wallace |
57
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* {enter_new_authors_here} |
58
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59
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* Notes: |
60
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* - This routine returns zenith distance rather than elevation |
61
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* in order to reflect the fact that no allowance is made for |
62
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* depression of the horizon. |
63
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* |
64
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* - The accuracy of the result is limited by the corrections for |
65
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* refraction. Providing the meteorological parameters are |
66
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* known accurately and there are no gross local effects, the |
67
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* observed RA,Dec predicted by this routine should be within |
68
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* about 0.1 arcsec for a zenith distance of less than 70 degrees. |
69
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* Even at a topocentric zenith distance of 90 degrees, the |
70
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* accuracy in elevation should be better than 1 arcmin; useful |
71
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* results are available for a further 3 degrees, beyond which |
72
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* the palRefro routine returns a fixed value of the refraction. |
73
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* The complementary routines palAop (or palAopqk) and palOap |
74
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* (or palOapqk) are self-consistent to better than 1 micro- |
75
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* arcsecond all over the celestial sphere. |
76
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* |
77
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* - It is advisable to take great care with units, as even |
78
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* unlikely values of the input parameters are accepted and |
79
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* processed in accordance with the models used. |
80
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* |
81
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* - "Apparent" place means the geocentric apparent right ascension |
82
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* and declination, which is obtained from a catalogue mean place |
83
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* by allowing for space motion, parallax, precession, nutation, |
84
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* annual aberration, and the Sun's gravitational lens effect. For |
85
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* star positions in the FK5 system (i.e. J2000), these effects can |
86
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* be applied by means of the palMap etc routines. Starting from |
87
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* other mean place systems, additional transformations will be |
88
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* needed; for example, FK4 (i.e. B1950) mean places would first |
89
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* have to be converted to FK5, which can be done with the |
90
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* palFk425 etc routines. |
91
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* |
92
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* - "Observed" Az,El means the position that would be seen by a |
93
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* perfect theodolite located at the observer. This is obtained |
94
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* from the geocentric apparent RA,Dec by allowing for Earth |
95
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|
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* orientation and diurnal aberration, rotating from equator |
96
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* to horizon coordinates, and then adjusting for refraction. |
97
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* The HA,Dec is obtained by rotating back into equatorial |
98
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* coordinates, using the geodetic latitude corrected for polar |
99
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* motion, and is the position that would be seen by a perfect |
100
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* equatorial located at the observer and with its polar axis |
101
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* aligned to the Earth's axis of rotation (n.b. not to the |
102
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|
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* refracted pole). Finally, the RA is obtained by subtracting |
103
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* the HA from the local apparent ST. |
104
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|
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* |
105
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|
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* - To predict the required setting of a real telescope, the |
106
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|
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* observed place produced by this routine would have to be |
107
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* adjusted for the tilt of the azimuth or polar axis of the |
108
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* mounting (with appropriate corrections for mount flexures), |
109
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* for non-perpendicularity between the mounting axes, for the |
110
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* position of the rotator axis and the pointing axis relative |
111
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* to it, for tube flexure, for gear and encoder errors, and |
112
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* finally for encoder zero points. Some telescopes would, of |
113
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* course, exhibit other properties which would need to be |
114
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|
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* accounted for at the appropriate point in the sequence. |
115
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* |
116
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* - The star-independent apparent-to-observed-place parameters |
117
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* in AOPRMS may be computed by means of the palAoppa routine. |
118
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* If nothing has changed significantly except the time, the |
119
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* palAoppat routine may be used to perform the requisite |
120
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* partial recomputation of AOPRMS. |
121
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|
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* |
122
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|
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|
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* - At zenith distances beyond about 76 degrees, the need for |
123
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|
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* special care with the corrections for refraction causes a |
124
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|
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* marked increase in execution time. Moreover, the effect |
125
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|
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* gets worse with increasing zenith distance. Adroit |
126
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|
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* programming in the calling application may allow the |
127
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* problem to be reduced. Prepare an alternative AOPRMS array, |
128
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* computed for zero air-pressure; this will disable the |
129
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* refraction corrections and cause rapid execution. Using |
130
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* this AOPRMS array, a preliminary call to the present routine |
131
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* will, depending on the application, produce a rough position |
132
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* which may be enough to establish whether the full, slow |
133
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* calculation (using the real AOPRMS array) is worthwhile. |
134
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* For example, there would be no need for the full calculation |
135
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* if the preliminary call had already established that the |
136
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* source was well below the elevation limits for a particular |
137
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* telescope. |
138
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* |
139
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* - The azimuths etc produced by the present routine are with |
140
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* respect to the celestial pole. Corrections to the terrestrial |
141
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* pole can be computed using palPolmo. |
142
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143
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* History: |
144
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* 2012-08-25 (TIMJ): |
145
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* Initial version, copied from Fortran SLA |
146
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* Adapted with permission from the Fortran SLALIB library. |
147
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* {enter_further_changes_here} |
148
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149
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* Copyright: |
150
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* Copyright (C) 2003 Rutherford Appleton Laboratory |
151
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* Copyright (C) 2012 Science and Technology Facilities Council. |
152
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* All Rights Reserved. |
153
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154
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* Licence: |
155
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* This program is free software; you can redistribute it and/or |
156
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* modify it under the terms of the GNU General Public License as |
157
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* published by the Free Software Foundation; either version 3 of |
158
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* the License, or (at your option) any later version. |
159
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* |
160
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* This program is distributed in the hope that it will be |
161
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* useful, but WITHOUT ANY WARRANTY; without even the implied |
162
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* warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR |
163
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* PURPOSE. See the GNU General Public License for more details. |
164
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* |
165
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* You should have received a copy of the GNU General Public License |
166
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* along with this program; if not, write to the Free Software |
167
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* Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, |
168
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* MA 02110-1301, USA. |
169
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170
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* Bugs: |
171
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* {note_any_bugs_here} |
172
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*- |
173
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*/ |
174
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175
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#include |
176
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177
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#include "pal.h" |
178
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179
|
3
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void palAopqk ( double rap, double dap, const double aoprms[14], |
180
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double *aob, double *zob, double *hob, |
181
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double *dob, double *rob ) { |
182
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183
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/* Breakpoint for fast/slow refraction algorithm: |
184
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* ZD greater than arctan(4), (see palRefco routine) |
185
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|
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* or vector Z less than cosine(arctan(Z)) = 1/sqrt(17) */ |
186
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const double zbreak = 0.242535625; |
187
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int i; |
188
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189
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double sphi,cphi,st,v[3],xhd,yhd,zhd,diurab,f, |
190
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xhdt,yhdt,zhdt,xaet,yaet,zaet,azobs, |
191
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zdt,refa,refb,zdobs,dzd,dref,ce, |
192
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xaeo,yaeo,zaeo,hmobs,dcobs,raobs; |
193
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194
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|
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/* sin, cos of latitude */ |
195
|
3
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sphi = aoprms[1]; |
196
|
3
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cphi = aoprms[2]; |
197
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|
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|
198
|
|
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/* local apparent sidereal time */ |
199
|
3
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|
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st = aoprms[13]; |
200
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|
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|
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|
201
|
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/* apparent ra,dec to cartesian -ha,dec */ |
202
|
3
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palDcs2c( rap-st, dap, v ); |
203
|
3
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|
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xhd = v[0]; |
204
|
3
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yhd = v[1]; |
205
|
3
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zhd = v[2]; |
206
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207
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/* diurnal aberration */ |
208
|
3
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diurab = aoprms[3]; |
209
|
3
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f = (1.0-diurab*yhd); |
210
|
3
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xhdt = f*xhd; |
211
|
3
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yhdt = f*(yhd+diurab); |
212
|
3
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zhdt = f*zhd; |
213
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214
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/* cartesian -ha,dec to cartesian az,el (s=0,e=90) */ |
215
|
3
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xaet = sphi*xhdt-cphi*zhdt; |
216
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|
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yaet = yhdt; |
217
|
3
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zaet = cphi*xhdt+sphi*zhdt; |
218
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219
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/* azimuth (n=0,e=90) */ |
220
|
3
|
50
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if (xaet == 0.0 && yaet == 0.0) { |
221
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azobs = 0.0; |
222
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} else { |
223
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3
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azobs = atan2(yaet,-xaet); |
224
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} |
225
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226
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/* topocentric zenith distance */ |
227
|
3
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zdt = atan2(sqrt(xaet*xaet+yaet*yaet),zaet); |
228
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229
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/* |
230
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* refraction |
231
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* ---------- */ |
232
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233
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|
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/* fast algorithm using two constant model */ |
234
|
3
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refa = aoprms[10]; |
235
|
3
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refb = aoprms[11]; |
236
|
3
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|
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palRefz(zdt,refa,refb,&zdobs); |
237
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238
|
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|
/* large zenith distance? */ |
239
|
3
|
100
|
|
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|
|
if (cos(zdobs) < zbreak) { |
240
|
|
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241
|
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|
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|
/* yes: use rigorous algorithm */ |
242
|
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243
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|
/* initialize loop (maximum of 10 iterations) */ |
244
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|
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i = 1; |
245
|
|
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|
dzd = 1.0e1; |
246
|
4
|
100
|
|
|
|
|
while (fabs(dzd) > 1e-10 && i <= 10) { |
|
|
50
|
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|
247
|
|
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|
248
|
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|
|
|
|
/* compute refraction using current estimate of observed zd */ |
249
|
3
|
|
|
|
|
|
palRefro(zdobs,aoprms[4],aoprms[5],aoprms[6], |
250
|
|
|
|
|
|
|
aoprms[7],aoprms[8],aoprms[0], |
251
|
|
|
|
|
|
|
aoprms[9],1e-8,&dref); |
252
|
|
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|
|
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|
|
253
|
|
|
|
|
|
|
/* remaining discrepancy */ |
254
|
3
|
|
|
|
|
|
dzd = zdobs+dref-zdt; |
255
|
|
|
|
|
|
|
|
256
|
|
|
|
|
|
|
/* update the estimate */ |
257
|
3
|
|
|
|
|
|
zdobs = zdobs-dzd; |
258
|
|
|
|
|
|
|
|
259
|
|
|
|
|
|
|
/* increment the iteration counter */ |
260
|
3
|
|
|
|
|
|
i++; |
261
|
|
|
|
|
|
|
} |
262
|
|
|
|
|
|
|
} |
263
|
|
|
|
|
|
|
|
264
|
|
|
|
|
|
|
/* to cartesian az/zd */ |
265
|
3
|
|
|
|
|
|
ce = sin(zdobs); |
266
|
3
|
|
|
|
|
|
xaeo = -cos(azobs)*ce; |
267
|
3
|
|
|
|
|
|
yaeo = sin(azobs)*ce; |
268
|
3
|
|
|
|
|
|
zaeo = cos(zdobs); |
269
|
|
|
|
|
|
|
|
270
|
|
|
|
|
|
|
/* cartesian az/zd to cartesian -ha,dec */ |
271
|
3
|
|
|
|
|
|
v[0] = sphi*xaeo+cphi*zaeo; |
272
|
3
|
|
|
|
|
|
v[1] = yaeo; |
273
|
3
|
|
|
|
|
|
v[2] = -cphi*xaeo+sphi*zaeo; |
274
|
|
|
|
|
|
|
|
275
|
|
|
|
|
|
|
/* to spherical -ha,dec */ |
276
|
3
|
|
|
|
|
|
palDcc2s(v,&hmobs,&dcobs); |
277
|
|
|
|
|
|
|
|
278
|
|
|
|
|
|
|
/* right ascension */ |
279
|
3
|
|
|
|
|
|
raobs = palDranrm(st+hmobs); |
280
|
|
|
|
|
|
|
|
281
|
|
|
|
|
|
|
/* return the results */ |
282
|
3
|
|
|
|
|
|
*aob = azobs; |
283
|
3
|
|
|
|
|
|
*zob = zdobs; |
284
|
3
|
|
|
|
|
|
*hob = -hmobs; |
285
|
3
|
|
|
|
|
|
*dob = dcobs; |
286
|
3
|
|
|
|
|
|
*rob = raobs; |
287
|
|
|
|
|
|
|
|
288
|
3
|
|
|
|
|
|
} |