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#include "erfa.h" |
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void eraP06e(double date1, double date2, |
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double *eps0, double *psia, double *oma, double *bpa, |
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double *bqa, double *pia, double *bpia, |
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double *epsa, double *chia, double *za, double *zetaa, |
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double *thetaa, double *pa, |
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double *gam, double *phi, double *psi) |
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/* |
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** - - - - - - - - |
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** e r a P 0 6 e |
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** - - - - - - - - |
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** |
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** Precession angles, IAU 2006, equinox based. |
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** |
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** Given: |
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** date1,date2 double TT as a 2-part Julian Date (Note 1) |
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** |
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** Returned (see Note 2): |
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** eps0 double epsilon_0 |
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** psia double psi_A |
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** oma double omega_A |
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** bpa double P_A |
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** bqa double Q_A |
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** pia double pi_A |
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** bpia double Pi_A |
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** epsa double obliquity epsilon_A |
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** chia double chi_A |
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** za double z_A |
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** zetaa double zeta_A |
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** thetaa double theta_A |
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** pa double p_A |
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** gam double F-W angle gamma_J2000 |
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** phi double F-W angle phi_J2000 |
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** psi double F-W angle psi_J2000 |
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** |
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** Notes: |
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** |
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** 1) The TT date date1+date2 is a Julian Date, apportioned in any |
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** convenient way between the two arguments. For example, |
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** JD(TT)=2450123.7 could be expressed in any of these ways, |
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** among others: |
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** |
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** date1 date2 |
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** |
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** 2450123.7 0.0 (JD method) |
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** 2451545.0 -1421.3 (J2000 method) |
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** 2400000.5 50123.2 (MJD method) |
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** 2450123.5 0.2 (date & time method) |
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** |
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** The JD method is the most natural and convenient to use in |
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** cases where the loss of several decimal digits of resolution |
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** is acceptable. The J2000 method is best matched to the way |
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** the argument is handled internally and will deliver the |
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** optimum resolution. The MJD method and the date & time methods |
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** are both good compromises between resolution and convenience. |
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** |
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** 2) This function returns the set of equinox based angles for the |
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** Capitaine et al. "P03" precession theory, adopted by the IAU in |
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** 2006. The angles are set out in Table 1 of Hilton et al. (2006): |
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** |
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** eps0 epsilon_0 obliquity at J2000.0 |
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** psia psi_A luni-solar precession |
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** oma omega_A inclination of equator wrt J2000.0 ecliptic |
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** bpa P_A ecliptic pole x, J2000.0 ecliptic triad |
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** bqa Q_A ecliptic pole -y, J2000.0 ecliptic triad |
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** pia pi_A angle between moving and J2000.0 ecliptics |
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** bpia Pi_A longitude of ascending node of the ecliptic |
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** epsa epsilon_A obliquity of the ecliptic |
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** chia chi_A planetary precession |
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** za z_A equatorial precession: -3rd 323 Euler angle |
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** zetaa zeta_A equatorial precession: -1st 323 Euler angle |
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** thetaa theta_A equatorial precession: 2nd 323 Euler angle |
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** pa p_A general precession (n.b. see below) |
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** gam gamma_J2000 J2000.0 RA difference of ecliptic poles |
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** phi phi_J2000 J2000.0 codeclination of ecliptic pole |
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** psi psi_J2000 longitude difference of equator poles, J2000.0 |
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** |
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** The returned values are all radians. |
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** |
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** Note that the t^5 coefficient in the series for p_A from |
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** Capitaine et al. (2003) is incorrectly signed in Hilton et al. |
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** (2006). |
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** |
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** 3) Hilton et al. (2006) Table 1 also contains angles that depend on |
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** models distinct from the P03 precession theory itself, namely the |
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** IAU 2000A frame bias and nutation. The quoted polynomials are |
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** used in other ERFA functions: |
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** |
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** . eraXy06 contains the polynomial parts of the X and Y series. |
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** |
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** . eraS06 contains the polynomial part of the s+XY/2 series. |
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** |
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** . eraPfw06 implements the series for the Fukushima-Williams |
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** angles that are with respect to the GCRS pole (i.e. the variants |
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** that include frame bias). |
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** |
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** 4) The IAU resolution stipulated that the choice of parameterization |
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** was left to the user, and so an IAU compliant precession |
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** implementation can be constructed using various combinations of |
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** the angles returned by the present function. |
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** |
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** 5) The parameterization used by ERFA is the version of the Fukushima- |
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** Williams angles that refers directly to the GCRS pole. These |
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** angles may be calculated by calling the function eraPfw06. ERFA |
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** also supports the direct computation of the CIP GCRS X,Y by |
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** series, available by calling eraXy06. |
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** |
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** 6) The agreement between the different parameterizations is at the |
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** 1 microarcsecond level in the present era. |
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** |
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** 7) When constructing a precession formulation that refers to the GCRS |
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** pole rather than the dynamical pole, it may (depending on the |
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** choice of angles) be necessary to introduce the frame bias |
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** explicitly. |
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** |
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** 8) It is permissible to re-use the same variable in the returned |
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** arguments. The quantities are stored in the stated order. |
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** |
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** References: |
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** |
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** Capitaine, N., Wallace, P.T. & Chapront, J., 2003, |
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** Astron.Astrophys., 412, 567 |
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** |
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** Hilton, J. et al., 2006, Celest.Mech.Dyn.Astron. 94, 351 |
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** |
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** Called: |
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** eraObl06 mean obliquity, IAU 2006 |
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** |
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** Copyright (C) 2013-2020, NumFOCUS Foundation. |
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** Derived, with permission, from the SOFA library. See notes at end of file. |
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*/ |
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{ |
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double t; |
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/* Interval between fundamental date J2000.0 and given date (JC). */ |
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t = ((date1 - ERFA_DJ00) + date2) / ERFA_DJC; |
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/* Obliquity at J2000.0. */ |
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*eps0 = 84381.406 * ERFA_DAS2R; |
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/* Luni-solar precession. */ |
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*psia = ( 5038.481507 + |
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( -1.0790069 + |
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( -0.00114045 + |
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( 0.000132851 + |
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( -0.0000000951 ) |
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* t) * t) * t) * t) * t * ERFA_DAS2R; |
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/* Inclination of mean equator with respect to the J2000.0 ecliptic. */ |
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*oma = *eps0 + ( -0.025754 + |
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( 0.0512623 + |
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( -0.00772503 + |
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( -0.000000467 + |
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( 0.0000003337 ) |
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* t) * t) * t) * t) * t * ERFA_DAS2R; |
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/* Ecliptic pole x, J2000.0 ecliptic triad. */ |
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*bpa = ( 4.199094 + |
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( 0.1939873 + |
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( -0.00022466 + |
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( -0.000000912 + |
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( 0.0000000120 ) |
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* t) * t) * t) * t) * t * ERFA_DAS2R; |
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/* Ecliptic pole -y, J2000.0 ecliptic triad. */ |
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*bqa = ( -46.811015 + |
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( 0.0510283 + |
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( 0.00052413 + |
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( -0.000000646 + |
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( -0.0000000172 ) |
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* t) * t) * t) * t) * t * ERFA_DAS2R; |
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180
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/* Angle between moving and J2000.0 ecliptics. */ |
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*pia = ( 46.998973 + |
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( -0.0334926 + |
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( -0.00012559 + |
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( 0.000000113 + |
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( -0.0000000022 ) |
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* t) * t) * t) * t) * t * ERFA_DAS2R; |
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/* Longitude of ascending node of the moving ecliptic. */ |
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*bpia = ( 629546.7936 + |
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( -867.95758 + |
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( 0.157992 + |
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( -0.0005371 + |
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( -0.00004797 + |
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( 0.000000072 ) |
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* t) * t) * t) * t) * t) * ERFA_DAS2R; |
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/* Mean obliquity of the ecliptic. */ |
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*epsa = eraObl06(date1, date2); |
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/* Planetary precession. */ |
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*chia = ( 10.556403 + |
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( -2.3814292 + |
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( -0.00121197 + |
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( 0.000170663 + |
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( -0.0000000560 ) |
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* t) * t) * t) * t) * t * ERFA_DAS2R; |
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/* Equatorial precession: minus the third of the 323 Euler angles. */ |
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*za = ( -2.650545 + |
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( 2306.077181 + |
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( 1.0927348 + |
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( 0.01826837 + |
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( -0.000028596 + |
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( -0.0000002904 ) |
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* t) * t) * t) * t) * t) * ERFA_DAS2R; |
221
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222
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/* Equatorial precession: minus the first of the 323 Euler angles. */ |
223
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224
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20
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*zetaa = ( 2.650545 + |
225
|
10
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( 2306.083227 + |
226
|
10
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( 0.2988499 + |
227
|
10
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( 0.01801828 + |
228
|
10
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( -0.000005971 + |
229
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( -0.0000003173 ) |
230
|
60
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* t) * t) * t) * t) * t) * ERFA_DAS2R; |
231
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232
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/* Equatorial precession: second of the 323 Euler angles. */ |
233
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234
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20
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*thetaa = ( 2004.191903 + |
235
|
10
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( -0.4294934 + |
236
|
10
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|
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( -0.04182264 + |
237
|
10
|
|
|
|
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( -0.000007089 + |
238
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|
|
|
|
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( -0.0000001274 ) |
239
|
50
|
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* t) * t) * t) * t) * t * ERFA_DAS2R; |
240
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241
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/* General precession. */ |
242
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243
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20
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*pa = ( 5028.796195 + |
244
|
10
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( 1.1054348 + |
245
|
10
|
|
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|
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( 0.00007964 + |
246
|
10
|
|
|
|
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( -0.000023857 + |
247
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|
|
|
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( -0.0000000383 ) |
248
|
50
|
|
|
|
|
|
* t) * t) * t) * t) * t * ERFA_DAS2R; |
249
|
|
|
|
|
|
|
|
250
|
|
|
|
|
|
|
/* Fukushima-Williams angles for precession. */ |
251
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|
252
|
20
|
|
|
|
|
|
*gam = ( 10.556403 + |
253
|
10
|
|
|
|
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( 0.4932044 + |
254
|
10
|
|
|
|
|
|
( -0.00031238 + |
255
|
10
|
|
|
|
|
|
( -0.000002788 + |
256
|
|
|
|
|
|
|
( 0.0000000260 ) |
257
|
50
|
|
|
|
|
|
* t) * t) * t) * t) * t * ERFA_DAS2R; |
258
|
|
|
|
|
|
|
|
259
|
30
|
|
|
|
|
|
*phi = *eps0 + ( -46.811015 + |
260
|
10
|
|
|
|
|
|
( 0.0511269 + |
261
|
10
|
|
|
|
|
|
( 0.00053289 + |
262
|
10
|
|
|
|
|
|
( -0.000000440 + |
263
|
|
|
|
|
|
|
( -0.0000000176 ) |
264
|
50
|
|
|
|
|
|
* t) * t) * t) * t) * t * ERFA_DAS2R; |
265
|
|
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|
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|
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|
266
|
20
|
|
|
|
|
|
*psi = ( 5038.481507 + |
267
|
10
|
|
|
|
|
|
( 1.5584176 + |
268
|
10
|
|
|
|
|
|
( -0.00018522 + |
269
|
10
|
|
|
|
|
|
( -0.000026452 + |
270
|
|
|
|
|
|
|
( -0.0000000148 ) |
271
|
50
|
|
|
|
|
|
* t) * t) * t) * t) * t * ERFA_DAS2R; |
272
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|
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|
|
273
|
10
|
|
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|
return; |
274
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275
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} |
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/*---------------------------------------------------------------------- |
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** |
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** |
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** Copyright (C) 2013-2020, NumFOCUS Foundation. |
280
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** All rights reserved. |
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** |
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** This library is derived, with permission, from the International |
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** Astronomical Union's "Standards of Fundamental Astronomy" library, |
284
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** available from http://www.iausofa.org. |
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** |
286
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** The ERFA version is intended to retain identical functionality to |
287
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** the SOFA library, but made distinct through different function and |
288
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** file names, as set out in the SOFA license conditions. The SOFA |
289
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|
|
|
|
** original has a role as a reference standard for the IAU and IERS, |
290
|
|
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|
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** and consequently redistribution is permitted only in its unaltered |
291
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** state. The ERFA version is not subject to this restriction and |
292
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|
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|
|
** therefore can be included in distributions which do not support the |
293
|
|
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|
|
|
|
** concept of "read only" software. |
294
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** |
295
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|
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** Although the intent is to replicate the SOFA API (other than |
296
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|
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|
|
** replacement of prefix names) and results (with the exception of |
297
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|
|
|
|
** bugs; any that are discovered will be fixed), SOFA is not |
298
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|
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|
|
** responsible for any errors found in this version of the library. |
299
|
|
|
|
|
|
|
** |
300
|
|
|
|
|
|
|
** If you wish to acknowledge the SOFA heritage, please acknowledge |
301
|
|
|
|
|
|
|
** that you are using a library derived from SOFA, rather than SOFA |
302
|
|
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|
|
|
|
** itself. |
303
|
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|
|
|
|
** |
304
|
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|
|
|
|
|
** |
305
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|
|
|
** TERMS AND CONDITIONS |
306
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|
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|
** |
307
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|
|
|
|
** Redistribution and use in source and binary forms, with or without |
308
|
|
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|
|
|
|
** modification, are permitted provided that the following conditions |
309
|
|
|
|
|
|
|
** are met: |
310
|
|
|
|
|
|
|
** |
311
|
|
|
|
|
|
|
** 1 Redistributions of source code must retain the above copyright |
312
|
|
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|
|
|
|
** notice, this list of conditions and the following disclaimer. |
313
|
|
|
|
|
|
|
** |
314
|
|
|
|
|
|
|
** 2 Redistributions in binary form must reproduce the above copyright |
315
|
|
|
|
|
|
|
** notice, this list of conditions and the following disclaimer in |
316
|
|
|
|
|
|
|
** the documentation and/or other materials provided with the |
317
|
|
|
|
|
|
|
** distribution. |
318
|
|
|
|
|
|
|
** |
319
|
|
|
|
|
|
|
** 3 Neither the name of the Standards Of Fundamental Astronomy Board, |
320
|
|
|
|
|
|
|
** the International Astronomical Union nor the names of its |
321
|
|
|
|
|
|
|
** contributors may be used to endorse or promote products derived |
322
|
|
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|
|
|
|
** from this software without specific prior written permission. |
323
|
|
|
|
|
|
|
** |
324
|
|
|
|
|
|
|
** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
325
|
|
|
|
|
|
|
** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
326
|
|
|
|
|
|
|
** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
327
|
|
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|
|
|
|
** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
328
|
|
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|
|
|
|
** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
329
|
|
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|
|
|
|
** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
330
|
|
|
|
|
|
|
** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; |
331
|
|
|
|
|
|
|
** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER |
332
|
|
|
|
|
|
|
** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
333
|
|
|
|
|
|
|
** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
334
|
|
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|
|
|
|
** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
335
|
|
|
|
|
|
|
** POSSIBILITY OF SUCH DAMAGE. |
336
|
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|
|
|
|
** |
337
|
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|
|
|
|
*/ |