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authorJoe Hunkeler <jhunkeler@gmail.com>2015-08-11 16:51:37 -0400
committerJoe Hunkeler <jhunkeler@gmail.com>2015-08-11 16:51:37 -0400
commit40e5a5811c6ffce9b0974e93cdd927cbcf60c157 (patch)
tree4464880c571602d54f6ae114729bf62a89518057 /math/slalib/atmt.f
downloadiraf-osx-40e5a5811c6ffce9b0974e93cdd927cbcf60c157.tar.gz
Repatch (from linux) of OSX IRAF
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+ SUBROUTINE slATMT (R0, T0, ALPHA, GAMM2, DELM2,
+ : C1, C2, C3, C4, C5, C6, R, T, DN, RDNDR)
+*+
+* - - - - -
+* A T M T
+* - - - - -
+*
+* Internal routine used by REFRO
+*
+* Refractive index and derivative with respect to height for the
+* troposphere.
+*
+* Given:
+* R0 d height of observer from centre of the Earth (metre)
+* T0 d temperature at the observer (K)
+* ALPHA d alpha )
+* GAMM2 d gamma minus 2 ) see HMNAO paper
+* DELM2 d delta minus 2 )
+* C1 d useful term )
+* C2 d useful term )
+* C3 d useful term ) see source
+* C4 d useful term ) of slRFRO
+* C5 d useful term )
+* C6 d useful term )
+* R d current distance from the centre of the Earth (metre)
+*
+* Returned:
+* T d temperature at R (K)
+* DN d refractive index at R
+* RDNDR d R * rate the refractive index is changing at R
+*
+* Note that in the optical case C5 and C6 are zero.
+*
+* Last revision: 26 December 2004
+*
+* Copyright P.T.Wallace. All rights reserved.
+*
+* License:
+* This program is free software; you can redistribute it and/or modify
+* it under the terms of the GNU General Public License as published by
+* the Free Software Foundation; either version 2 of the License, or
+* (at your option) any later version.
+*
+* This program is distributed in the hope that it will be useful,
+* but WITHOUT ANY WARRANTY; without even the implied warranty of
+* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
+* GNU General Public License for more details.
+*
+* You should have received a copy of the GNU General Public License
+* along with this program (see SLA_CONDITIONS); if not, write to the
+* Free Software Foundation, Inc., 51 Franklin Street, Fifth Floor,
+* Boston, MA 02110-1301 USA
+*
+* Copyright (C) 1995 Association of Universities for Research in Astronomy Inc.
+*-
+
+ IMPLICIT NONE
+
+ DOUBLE PRECISION R0,T0,ALPHA,GAMM2,DELM2,C1,C2,C3,C4,C5,C6,
+ : R,T,DN,RDNDR
+
+ DOUBLE PRECISION TT0,TT0GM2,TT0DM2
+
+
+ T = MAX(MIN(T0-ALPHA*(R-R0),320D0),100D0)
+ TT0 = T/T0
+ TT0GM2 = TT0**GAMM2
+ TT0DM2 = TT0**DELM2
+ DN = 1D0+(C1*TT0GM2-(C2-C5/T)*TT0DM2)*TT0
+ RDNDR = R*(-C3*TT0GM2+(C4-C6/TT0)*TT0DM2)
+
+ END