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#include "erfa.h" |
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void eraApco(double date1, double date2, |
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double ebpv[2][3], double ehp[3], |
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double x, double y, double s, double theta, |
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double elong, double phi, double hm, |
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double xp, double yp, double sp, |
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double refa, double refb, |
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eraASTROM *astrom) |
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/* |
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** - - - - - - - - |
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** e r a A p c o |
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** - - - - - - - - |
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** |
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** For a terrestrial observer, prepare star-independent astrometry |
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** parameters for transformations between ICRS and observed |
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** coordinates. The caller supplies the Earth ephemeris, the Earth |
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** rotation information and the refraction constants as well as the |
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** site coordinates. |
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** |
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** Given: |
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** date1 double TDB as a 2-part... |
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** date2 double ...Julian Date (Note 1) |
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** ebpv double[2][3] Earth barycentric PV (au, au/day, Note 2) |
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** ehp double[3] Earth heliocentric P (au, Note 2) |
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** x,y double CIP X,Y (components of unit vector) |
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** s double the CIO locator s (radians) |
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** theta double Earth rotation angle (radians) |
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** elong double longitude (radians, east +ve, Note 3) |
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** phi double latitude (geodetic, radians, Note 3) |
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** hm double height above ellipsoid (m, geodetic, Note 3) |
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** xp,yp double polar motion coordinates (radians, Note 4) |
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** sp double the TIO locator s' (radians, Note 4) |
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** refa double refraction constant A (radians, Note 5) |
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** refb double refraction constant B (radians, Note 5) |
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** |
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** Returned: |
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** astrom eraASTROM* star-independent astrometry parameters: |
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** pmt double PM time interval (SSB, Julian years) |
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** eb double[3] SSB to observer (vector, au) |
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** eh double[3] Sun to observer (unit vector) |
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** em double distance from Sun to observer (au) |
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** v double[3] barycentric observer velocity (vector, c) |
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** bm1 double sqrt(1-|v|^2): reciprocal of Lorenz factor |
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** bpn double[3][3] bias-precession-nutation matrix |
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** along double longitude + s' (radians) |
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** xpl double polar motion xp wrt local meridian (radians) |
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** ypl double polar motion yp wrt local meridian (radians) |
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** sphi double sine of geodetic latitude |
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** cphi double cosine of geodetic latitude |
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** diurab double magnitude of diurnal aberration vector |
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** eral double "local" Earth rotation angle (radians) |
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** refa double refraction constant A (radians) |
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** refb double refraction constant B (radians) |
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** |
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** Notes: |
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** |
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** 1) The TDB 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(TDB)=2450123.7 could be expressed in any of these ways, among |
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** 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 cases |
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** where the loss of several decimal digits of resolution is |
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** acceptable. The J2000 method is best matched to the way the |
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** argument is handled internally and will deliver the optimum |
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** resolution. The MJD method and the date & time methods are both |
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** good compromises between resolution and convenience. For most |
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** applications of this function the choice will not be at all |
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** critical. |
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** |
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** TT can be used instead of TDB without any significant impact on |
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** accuracy. |
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** |
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** 2) The vectors eb, eh, and all the astrom vectors, are with respect |
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** to BCRS axes. |
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** |
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** 3) The geographical coordinates are with respect to the ERFA_WGS84 |
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** reference ellipsoid. TAKE CARE WITH THE LONGITUDE SIGN |
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** CONVENTION: the longitude required by the present function is |
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** right-handed, i.e. east-positive, in accordance with geographical |
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** convention. |
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** |
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** 4) xp and yp are the coordinates (in radians) of the Celestial |
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** Intermediate Pole with respect to the International Terrestrial |
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** Reference System (see IERS Conventions), measured along the |
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** meridians 0 and 90 deg west respectively. sp is the TIO locator |
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** s', in radians, which positions the Terrestrial Intermediate |
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** Origin on the equator. For many applications, xp, yp and |
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** (especially) sp can be set to zero. |
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** |
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** Internally, the polar motion is stored in a form rotated onto the |
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** local meridian. |
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** |
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** 5) The refraction constants refa and refb are for use in a |
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** dZ = A*tan(Z)+B*tan^3(Z) model, where Z is the observed |
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** (i.e. refracted) zenith distance and dZ is the amount of |
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** refraction. |
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** |
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** 6) It is advisable to take great care with units, as even unlikely |
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** values of the input parameters are accepted and processed in |
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** accordance with the models used. |
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** |
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** 7) In cases where the caller does not wish to provide the Earth |
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** Ephemeris, the Earth rotation information and refraction |
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** constants, the function eraApco13 can be used instead of the |
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** present function. This starts from UTC and weather readings etc. |
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** and computes suitable values using other ERFA functions. |
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** |
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** 8) This is one of several functions that inserts into the astrom |
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** structure star-independent parameters needed for the chain of |
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** astrometric transformations ICRS <-> GCRS <-> CIRS <-> observed. |
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** |
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** The various functions support different classes of observer and |
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** portions of the transformation chain: |
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** |
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** functions observer transformation |
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** |
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** eraApcg eraApcg13 geocentric ICRS <-> GCRS |
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** eraApci eraApci13 terrestrial ICRS <-> CIRS |
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** eraApco eraApco13 terrestrial ICRS <-> observed |
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** eraApcs eraApcs13 space ICRS <-> GCRS |
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** eraAper eraAper13 terrestrial update Earth rotation |
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** eraApio eraApio13 terrestrial CIRS <-> observed |
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** |
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** Those with names ending in "13" use contemporary ERFA models to |
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** compute the various ephemerides. The others accept ephemerides |
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** supplied by the caller. |
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** |
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** The transformation from ICRS to GCRS covers space motion, |
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** parallax, light deflection, and aberration. From GCRS to CIRS |
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** comprises frame bias and precession-nutation. From CIRS to |
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** observed takes account of Earth rotation, polar motion, diurnal |
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** aberration and parallax (unless subsumed into the ICRS <-> GCRS |
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** transformation), and atmospheric refraction. |
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** |
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** 9) The context structure astrom produced by this function is used by |
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** eraAtioq, eraAtoiq, eraAtciq* and eraAticq*. |
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** |
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** Called: |
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** eraAper astrometry parameters: update ERA |
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** eraC2ixys celestial-to-intermediate matrix, given X,Y and s |
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** eraPvtob position/velocity of terrestrial station |
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** eraTrxpv product of transpose of r-matrix and pv-vector |
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** eraApcs astrometry parameters, ICRS-GCRS, space observer |
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** eraCr copy r-matrix |
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** |
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** Copyright (C) 2013-2019, 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 sl, cl, r[3][3], pvc[2][3], pv[2][3]; |
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161
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162
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/* Longitude with adjustment for TIO locator s'. */ |
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astrom->along = elong + sp; |
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/* Polar motion, rotated onto the local meridian. */ |
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sl = sin(astrom->along); |
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cl = cos(astrom->along); |
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astrom->xpl = xp*cl - yp*sl; |
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astrom->ypl = xp*sl + yp*cl; |
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/* Functions of latitude. */ |
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astrom->sphi = sin(phi); |
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astrom->cphi = cos(phi); |
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/* Refraction constants. */ |
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astrom->refa = refa; |
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astrom->refb = refb; |
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/* Local Earth rotation angle. */ |
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eraAper(theta, astrom); |
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/* Disable the (redundant) diurnal aberration step. */ |
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astrom->diurab = 0.0; |
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185
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/* CIO based BPN matrix. */ |
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eraC2ixys(x, y, s, r); |
187
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188
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/* Observer's geocentric position and velocity (m, m/s, CIRS). */ |
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eraPvtob(elong, phi, hm, xp, yp, sp, theta, pvc); |
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191
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/* Rotate into GCRS. */ |
192
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eraTrxpv(r, pvc, pv); |
193
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194
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/* ICRS <-> GCRS parameters. */ |
195
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eraApcs(date1, date2, pv, ebpv, ehp, astrom); |
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197
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/* Store the CIO based BPN matrix. */ |
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eraCr(r, astrom->bpn ); |
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200
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/* Finished. */ |
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} |
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/*---------------------------------------------------------------------- |
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** |
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** |
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** Copyright (C) 2013-2019, NumFOCUS Foundation. |
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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, |
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** available from http://www.iausofa.org. |
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** |
213
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** The ERFA version is intended to retain identical functionality to |
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** the SOFA library, but made distinct through different function and |
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** file names, as set out in the SOFA license conditions. The SOFA |
216
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** original has a role as a reference standard for the IAU and IERS, |
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** and consequently redistribution is permitted only in its unaltered |
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** state. The ERFA version is not subject to this restriction and |
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** therefore can be included in distributions which do not support the |
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** concept of "read only" software. |
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** |
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** Although the intent is to replicate the SOFA API (other than |
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** replacement of prefix names) and results (with the exception of |
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** bugs; any that are discovered will be fixed), SOFA is not |
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** responsible for any errors found in this version of the library. |
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** |
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** If you wish to acknowledge the SOFA heritage, please acknowledge |
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** that you are using a library derived from SOFA, rather than SOFA |
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** itself. |
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** |
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** |
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** TERMS AND CONDITIONS |
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** |
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** Redistribution and use in source and binary forms, with or without |
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** modification, are permitted provided that the following conditions |
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** are met: |
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** |
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** 1 Redistributions of source code must retain the above copyright |
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** notice, this list of conditions and the following disclaimer. |
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** |
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** 2 Redistributions in binary form must reproduce the above copyright |
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** notice, this list of conditions and the following disclaimer in |
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** the documentation and/or other materials provided with the |
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** distribution. |
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** |
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** 3 Neither the name of the Standards Of Fundamental Astronomy Board, |
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** the International Astronomical Union nor the names of its |
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** contributors may be used to endorse or promote products derived |
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** from this software without specific prior written permission. |
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** |
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** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
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** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
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** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
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** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
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** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
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** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
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** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; |
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** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER |
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** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
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** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
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** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
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** POSSIBILITY OF SUCH DAMAGE. |
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** |
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*/ |