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74
slalib/eqeqx.f
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74
slalib/eqeqx.f
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DOUBLE PRECISION FUNCTION sla_EQEQX (DATE)
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*+
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* - - - - - -
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* E Q E Q X
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* - - - - - -
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*
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* Equation of the equinoxes (IAU 1994, double precision)
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*
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* Given:
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* DATE dp TDB (loosely ET) as Modified Julian Date
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* (JD-2400000.5)
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*
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* The result is the equation of the equinoxes (double precision)
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* in radians:
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*
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* Greenwich apparent ST = GMST + sla_EQEQX
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*
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* References: IAU Resolution C7, Recommendation 3 (1994)
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* Capitaine, N. & Gontier, A.-M., Astron. Astrophys.,
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* 275, 645-650 (1993)
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*
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* Called: sla_NUTC
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*
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* Patrick Wallace Starlink 23 August 1996
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*
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* Copyright (C) 1996 Rutherford Appleton Laboratory
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*
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* License:
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 2 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with this program (see SLA_CONDITIONS); if not, write to the
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* Free Software Foundation, Inc., 59 Temple Place, Suite 330,
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* Boston, MA 02111-1307 USA
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*
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*-
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IMPLICIT NONE
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DOUBLE PRECISION DATE
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* Turns to arc seconds and arc seconds to radians
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DOUBLE PRECISION T2AS,AS2R
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PARAMETER (T2AS=1296000D0,
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: AS2R=0.484813681109535994D-5)
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DOUBLE PRECISION T,OM,DPSI,DEPS,EPS0
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* Interval between basic epoch J2000.0 and current epoch (JC)
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T=(DATE-51544.5D0)/36525D0
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* Longitude of the mean ascending node of the lunar orbit on the
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* ecliptic, measured from the mean equinox of date
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OM=AS2R*(450160.280D0+(-5D0*T2AS-482890.539D0
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: +(7.455D0+0.008D0*T)*T)*T)
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* Nutation
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CALL sla_NUTC(DATE,DPSI,DEPS,EPS0)
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* Equation of the equinoxes
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sla_EQEQX=DPSI*COS(EPS0)+AS2R*(0.00264D0*SIN(OM)+
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: 0.000063D0*SIN(OM+OM))
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END
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