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eddyem
2015-10-27 19:46:19 +03:00
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SUBROUTINE sla_PRECL (EP0, EP1, RMATP)
*+
* - - - - - -
* P R E C L
* - - - - - -
*
* Form the matrix of precession between two epochs, using the
* model of Simon et al (1994), which is suitable for long
* periods of time.
*
* (double precision)
*
* Given:
* EP0 dp beginning epoch
* EP1 dp ending epoch
*
* Returned:
* RMATP dp(3,3) precession matrix
*
* Notes:
*
* 1) The epochs are TDB Julian epochs.
*
* 2) The matrix is in the sense V(EP1) = RMATP * V(EP0)
*
* 3) The absolute accuracy of the model is limited by the
* uncertainty in the general precession, about 0.3 arcsec per
* 1000 years. The remainder of the formulation provides a
* precision of 1 mas over the interval from 1000AD to 3000AD,
* 0.1 arcsec from 1000BC to 5000AD and 1 arcsec from
* 4000BC to 8000AD.
*
* Reference:
* Simon, J.L. et al., 1994. Astron.Astrophys., 282, 663-683.
*
* Called: sla_DEULER
*
* P.T.Wallace Starlink 23 August 1996
*
* Copyright (C) 1996 Rutherford Appleton Laboratory
*
* 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., 59 Temple Place, Suite 330,
* Boston, MA 02111-1307 USA
*
*-
IMPLICIT NONE
DOUBLE PRECISION EP0,EP1,RMATP(3,3)
* Arc seconds to radians
DOUBLE PRECISION AS2R
PARAMETER (AS2R=0.484813681109535994D-5)
DOUBLE PRECISION T0,T,TAS2R,W,ZETA,Z,THETA
* Interval between basic epoch J2000.0 and beginning epoch (1000JY)
T0 = (EP0-2000D0)/1000D0
* Interval over which precession required (1000JY)
T = (EP1-EP0)/1000D0
* Euler angles
TAS2R = T*AS2R
W = 23060.9097D0+
: (139.7459D0+
: (-0.0038D0+
: (-0.5918D0+
: (-0.0037D0+
: 0.0007D0*T0)*T0)*T0)*T0)*T0
ZETA = (W+(30.2226D0+
: (-0.2523D0+
: (-0.3840D0+
: (-0.0014D0+
: 0.0007D0*T0)*T0)*T0)*T0+
: (18.0183D0+
: (-0.1326D0+
: (0.0006D0+
: 0.0005D0*T0)*T0)*T0+
: (-0.0583D0+
: (-0.0001D0+
: 0.0007D0*T0)*T0+
: (-0.0285D0+
: (-0.0002D0)*T)*T)*T)*T)*T)*TAS2R
Z = (W+(109.5270D0+
: (0.2446D0+
: (-1.3913D0+
: (-0.0134D0+
: 0.0026D0*T0)*T0)*T0)*T0+
: (18.2667D0+
: (-1.1400D0+
: (-0.0173D0+
: 0.0044D0*T0)*T0)*T0+
: (-0.2821D0+
: (-0.0093D0+
: 0.0032D0*T0)*T0+
: (-0.0301D0+
: 0.0006D0*T0
: -0.0001D0*T)*T)*T)*T)*T)*TAS2R
THETA = (20042.0207D0+
: (-85.3131D0+
: (-0.2111D0+
: (0.3642D0+
: (0.0008D0+
: (-0.0005D0)*T0)*T0)*T0)*T0)*T0+
: (-42.6566D0+
: (-0.2111D0+
: (0.5463D0+
: (0.0017D0+
: (-0.0012D0)*T0)*T0)*T0)*T0+
: (-41.8238D0+
: (0.0359D0+
: (0.0027D0+
: (-0.0001D0)*T0)*T0)*T0+
: (-0.0731D0+
: (0.0019D0+
: 0.0009D0*T0)*T0+
: (-0.0127D0+
: 0.0011D0*T0+0.0004D0*T)*T)*T)*T)*T)*TAS2R
* Rotation matrix
CALL sla_DEULER('ZYZ',-ZETA,THETA,-Z,RMATP)
END