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Diffstat (limited to 'src/slalib/precl.f')
-rw-r--r-- | src/slalib/precl.f | 125 |
1 files changed, 125 insertions, 0 deletions
diff --git a/src/slalib/precl.f b/src/slalib/precl.f new file mode 100644 index 0000000..e24b3d3 --- /dev/null +++ b/src/slalib/precl.f @@ -0,0 +1,125 @@ + 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 +*- + + 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 |