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authorWilliam Joye <wjoye@cfa.harvard.edu>2019-05-10 16:22:37 (GMT)
committerWilliam Joye <wjoye@cfa.harvard.edu>2019-05-10 16:22:37 (GMT)
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-#include "erfa.h"
-
-void eraApco(double date1, double date2,
- double ebpv[2][3], double ehp[3],
- double x, double y, double s, double theta,
- double elong, double phi, double hm,
- double xp, double yp, double sp,
- double refa, double refb,
- eraASTROM *astrom)
-/*
-** - - - - - - - -
-** e r a A p c o
-** - - - - - - - -
-**
-** For a terrestrial observer, prepare star-independent astrometry
-** parameters for transformations between ICRS and observed
-** coordinates. The caller supplies the Earth ephemeris, the Earth
-** rotation information and the refraction constants as well as the
-** site coordinates.
-**
-** Given:
-** date1 double TDB as a 2-part...
-** date2 double ...Julian Date (Note 1)
-** ebpv double[2][3] Earth barycentric PV (au, au/day, Note 2)
-** ehp double[3] Earth heliocentric P (au, Note 2)
-** x,y double CIP X,Y (components of unit vector)
-** s double the CIO locator s (radians)
-** theta double Earth rotation angle (radians)
-** elong double longitude (radians, east +ve, Note 3)
-** phi double latitude (geodetic, radians, Note 3)
-** hm double height above ellipsoid (m, geodetic, Note 3)
-** xp,yp double polar motion coordinates (radians, Note 4)
-** sp double the TIO locator s' (radians, Note 4)
-** refa double refraction constant A (radians, Note 5)
-** refb double refraction constant B (radians, Note 5)
-**
-** Returned:
-** astrom eraASTROM* star-independent astrometry parameters:
-** pmt double PM time interval (SSB, Julian years)
-** eb double[3] SSB to observer (vector, au)
-** eh double[3] Sun to observer (unit vector)
-** em double distance from Sun to observer (au)
-** v double[3] barycentric observer velocity (vector, c)
-** bm1 double sqrt(1-|v|^2): reciprocal of Lorenz factor
-** bpn double[3][3] bias-precession-nutation matrix
-** along double longitude + s' (radians)
-** xpl double polar motion xp wrt local meridian (radians)
-** ypl double polar motion yp wrt local meridian (radians)
-** sphi double sine of geodetic latitude
-** cphi double cosine of geodetic latitude
-** diurab double magnitude of diurnal aberration vector
-** eral double "local" Earth rotation angle (radians)
-** refa double refraction constant A (radians)
-** refb double refraction constant B (radians)
-**
-** Notes:
-**
-** 1) The TDB date date1+date2 is a Julian Date, apportioned in any
-** convenient way between the two arguments. For example,
-** JD(TDB)=2450123.7 could be expressed in any of these ways, among
-** others:
-**
-** date1 date2
-**
-** 2450123.7 0.0 (JD method)
-** 2451545.0 -1421.3 (J2000 method)
-** 2400000.5 50123.2 (MJD method)
-** 2450123.5 0.2 (date & time method)
-**
-** The JD method is the most natural and convenient to use in cases
-** where the loss of several decimal digits of resolution is
-** acceptable. The J2000 method is best matched to the way the
-** argument is handled internally and will deliver the optimum
-** resolution. The MJD method and the date & time methods are both
-** good compromises between resolution and convenience. For most
-** applications of this function the choice will not be at all
-** critical.
-**
-** TT can be used instead of TDB without any significant impact on
-** accuracy.
-**
-** 2) The vectors eb, eh, and all the astrom vectors, are with respect
-** to BCRS axes.
-**
-** 3) The geographical coordinates are with respect to the ERFA_WGS84
-** reference ellipsoid. TAKE CARE WITH THE LONGITUDE SIGN
-** CONVENTION: the longitude required by the present function is
-** right-handed, i.e. east-positive, in accordance with geographical
-** convention.
-**
-** 4) xp and yp are the coordinates (in radians) of the Celestial
-** Intermediate Pole with respect to the International Terrestrial
-** Reference System (see IERS Conventions), measured along the
-** meridians 0 and 90 deg west respectively. sp is the TIO locator
-** s', in radians, which positions the Terrestrial Intermediate
-** Origin on the equator. For many applications, xp, yp and
-** (especially) sp can be set to zero.
-**
-** Internally, the polar motion is stored in a form rotated onto the
-** local meridian.
-**
-** 5) The refraction constants refa and refb are for use in a
-** dZ = A*tan(Z)+B*tan^3(Z) model, where Z is the observed
-** (i.e. refracted) zenith distance and dZ is the amount of
-** refraction.
-**
-** 6) It is advisable to take great care with units, as even unlikely
-** values of the input parameters are accepted and processed in
-** accordance with the models used.
-**
-** 7) In cases where the caller does not wish to provide the Earth
-** Ephemeris, the Earth rotation information and refraction
-** constants, the function eraApco13 can be used instead of the
-** present function. This starts from UTC and weather readings etc.
-** and computes suitable values using other ERFA functions.
-**
-** 8) This is one of several functions that inserts into the astrom
-** structure star-independent parameters needed for the chain of
-** astrometric transformations ICRS <-> GCRS <-> CIRS <-> observed.
-**
-** The various functions support different classes of observer and
-** portions of the transformation chain:
-**
-** functions observer transformation
-**
-** eraApcg eraApcg13 geocentric ICRS <-> GCRS
-** eraApci eraApci13 terrestrial ICRS <-> CIRS
-** eraApco eraApco13 terrestrial ICRS <-> observed
-** eraApcs eraApcs13 space ICRS <-> GCRS
-** eraAper eraAper13 terrestrial update Earth rotation
-** eraApio eraApio13 terrestrial CIRS <-> observed
-**
-** Those with names ending in "13" use contemporary ERFA models to
-** compute the various ephemerides. The others accept ephemerides
-** supplied by the caller.
-**
-** The transformation from ICRS to GCRS covers space motion,
-** parallax, light deflection, and aberration. From GCRS to CIRS
-** comprises frame bias and precession-nutation. From CIRS to
-** observed takes account of Earth rotation, polar motion, diurnal
-** aberration and parallax (unless subsumed into the ICRS <-> GCRS
-** transformation), and atmospheric refraction.
-**
-** 9) The context structure astrom produced by this function is used by
-** eraAtioq, eraAtoiq, eraAtciq* and eraAticq*.
-**
-** Called:
-** eraAper astrometry parameters: update ERA
-** eraC2ixys celestial-to-intermediate matrix, given X,Y and s
-** eraPvtob position/velocity of terrestrial station
-** eraTrxpv product of transpose of r-matrix and pv-vector
-** eraApcs astrometry parameters, ICRS-GCRS, space observer
-** eraCr copy r-matrix
-**
-** Copyright (C) 2013-2016, NumFOCUS Foundation.
-** Derived, with permission, from the SOFA library. See notes at end of file.
-*/
-{
- double sl, cl, r[3][3], pvc[2][3], pv[2][3];
-
-
-/* Longitude with adjustment for TIO locator s'. */
- astrom->along = elong + sp;
-
-/* Polar motion, rotated onto the local meridian. */
- sl = sin(astrom->along);
- cl = cos(astrom->along);
- astrom->xpl = xp*cl - yp*sl;
- astrom->ypl = xp*sl + yp*cl;
-
-/* Functions of latitude. */
- astrom->sphi = sin(phi);
- astrom->cphi = cos(phi);
-
-/* Refraction constants. */
- astrom->refa = refa;
- astrom->refb = refb;
-
-/* Local Earth rotation angle. */
- eraAper(theta, astrom);
-
-/* Disable the (redundant) diurnal aberration step. */
- astrom->diurab = 0.0;
-
-/* CIO based BPN matrix. */
- eraC2ixys(x, y, s, r);
-
-/* Observer's geocentric position and velocity (m, m/s, CIRS). */
- eraPvtob(elong, phi, hm, xp, yp, sp, theta, pvc);
-
-/* Rotate into GCRS. */
- eraTrxpv(r, pvc, pv);
-
-/* ICRS <-> GCRS parameters. */
- eraApcs(date1, date2, pv, ebpv, ehp, astrom);
-
-/* Store the CIO based BPN matrix. */
- eraCr(r, astrom->bpn );
-
-/* Finished. */
-
-}
-/*----------------------------------------------------------------------
-**
-**
-** Copyright (C) 2013-2016, NumFOCUS Foundation.
-** All rights reserved.
-**
-** This library is derived, with permission, from the International
-** Astronomical Union's "Standards of Fundamental Astronomy" library,
-** available from http://www.iausofa.org.
-**
-** The ERFA version is intended to retain identical functionality to
-** the SOFA library, but made distinct through different function and
-** file names, as set out in the SOFA license conditions. The SOFA
-** original has a role as a reference standard for the IAU and IERS,
-** and consequently redistribution is permitted only in its unaltered
-** state. The ERFA version is not subject to this restriction and
-** therefore can be included in distributions which do not support the
-** concept of "read only" software.
-**
-** Although the intent is to replicate the SOFA API (other than
-** replacement of prefix names) and results (with the exception of
-** bugs; any that are discovered will be fixed), SOFA is not
-** responsible for any errors found in this version of the library.
-**
-** If you wish to acknowledge the SOFA heritage, please acknowledge
-** that you are using a library derived from SOFA, rather than SOFA
-** itself.
-**
-**
-** TERMS AND CONDITIONS
-**
-** Redistribution and use in source and binary forms, with or without
-** modification, are permitted provided that the following conditions
-** are met:
-**
-** 1 Redistributions of source code must retain the above copyright
-** notice, this list of conditions and the following disclaimer.
-**
-** 2 Redistributions in binary form must reproduce the above copyright
-** notice, this list of conditions and the following disclaimer in
-** the documentation and/or other materials provided with the
-** distribution.
-**
-** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
-** the International Astronomical Union nor the names of its
-** contributors may be used to endorse or promote products derived
-** from this software without specific prior written permission.
-**
-** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
-** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
-** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
-** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
-** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
-** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
-** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
-** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
-** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
-** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
-** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
-** POSSIBILITY OF SUCH DAMAGE.
-**
-*/