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+#include "erfa.h"
+
+int eraStarpv(double ra, double dec,
+ double pmr, double pmd, double px, double rv,
+ double pv[2][3])
+/*
+** - - - - - - - - - -
+** e r a S t a r p v
+** - - - - - - - - - -
+**
+** Convert star catalog coordinates to position+velocity vector.
+**
+** Given (Note 1):
+** ra double right ascension (radians)
+** dec double declination (radians)
+** pmr double RA proper motion (radians/year)
+** pmd double Dec proper motion (radians/year)
+** px double parallax (arcseconds)
+** rv double radial velocity (km/s, positive = receding)
+**
+** Returned (Note 2):
+** pv double[2][3] pv-vector (AU, AU/day)
+**
+** Returned (function value):
+** int status:
+** 0 = no warnings
+** 1 = distance overridden (Note 6)
+** 2 = excessive speed (Note 7)
+** 4 = solution didn't converge (Note 8)
+** else = binary logical OR of the above
+**
+** Notes:
+**
+** 1) The star data accepted by this function are "observables" for an
+** imaginary observer at the solar-system barycenter. Proper motion
+** and radial velocity are, strictly, in terms of barycentric
+** coordinate time, TCB. For most practical applications, it is
+** permissible to neglect the distinction between TCB and ordinary
+** "proper" time on Earth (TT/TAI). The result will, as a rule, be
+** limited by the intrinsic accuracy of the proper-motion and
+** radial-velocity data; moreover, the pv-vector is likely to be
+** merely an intermediate result, so that a change of time unit
+** would cancel out overall.
+**
+** In accordance with normal star-catalog conventions, the object's
+** right ascension and declination are freed from the effects of
+** secular aberration. The frame, which is aligned to the catalog
+** equator and equinox, is Lorentzian and centered on the SSB.
+**
+** 2) The resulting position and velocity pv-vector is with respect to
+** the same frame and, like the catalog coordinates, is freed from
+** the effects of secular aberration. Should the "coordinate
+** direction", where the object was located at the catalog epoch, be
+** required, it may be obtained by calculating the magnitude of the
+** position vector pv[0][0-2] dividing by the speed of light in
+** AU/day to give the light-time, and then multiplying the space
+** velocity pv[1][0-2] by this light-time and adding the result to
+** pv[0][0-2].
+**
+** Summarizing, the pv-vector returned is for most stars almost
+** identical to the result of applying the standard geometrical
+** "space motion" transformation. The differences, which are the
+** subject of the Stumpff paper referenced below, are:
+**
+** (i) In stars with significant radial velocity and proper motion,
+** the constantly changing light-time distorts the apparent proper
+** motion. Note that this is a classical, not a relativistic,
+** effect.
+**
+** (ii) The transformation complies with special relativity.
+**
+** 3) Care is needed with units. The star coordinates are in radians
+** and the proper motions in radians per Julian year, but the
+** parallax is in arcseconds; the radial velocity is in km/s, but
+** the pv-vector result is in AU and AU/day.
+**
+** 4) The RA proper motion is in terms of coordinate angle, not true
+** angle. If the catalog uses arcseconds for both RA and Dec proper
+** motions, the RA proper motion will need to be divided by cos(Dec)
+** before use.
+**
+** 5) Straight-line motion at constant speed, in the inertial frame,
+** is assumed.
+**
+** 6) An extremely small (or zero or negative) parallax is interpreted
+** to mean that the object is on the "celestial sphere", the radius
+** of which is an arbitrary (large) value (see the constant PXMIN).
+** When the distance is overridden in this way, the status,
+** initially zero, has 1 added to it.
+**
+** 7) If the space velocity is a significant fraction of c (see the
+** constant VMAX), it is arbitrarily set to zero. When this action
+** occurs, 2 is added to the status.
+**
+** 8) The relativistic adjustment involves an iterative calculation.
+** If the process fails to converge within a set number (IMAX) of
+** iterations, 4 is added to the status.
+**
+** 9) The inverse transformation is performed by the function
+** eraPvstar.
+**
+** Called:
+** eraS2pv spherical coordinates to pv-vector
+** eraPm modulus of p-vector
+** eraZp zero p-vector
+** eraPn decompose p-vector into modulus and direction
+** eraPdp scalar product of two p-vectors
+** eraSxp multiply p-vector by scalar
+** eraPmp p-vector minus p-vector
+** eraPpp p-vector plus p-vector
+**
+** Reference:
+**
+** Stumpff, P., 1985, Astron.Astrophys. 144, 232-240.
+**
+** Copyright (C) 2013-2014, NumFOCUS Foundation.
+** Derived, with permission, from the SOFA library. See notes at end of file.
+*/
+{
+/* Smallest allowed parallax */
+ static const double PXMIN = 1e-7;
+
+/* Largest allowed speed (fraction of c) */
+ static const double VMAX = 0.5;
+
+/* Maximum number of iterations for relativistic solution */
+ static const int IMAX = 100;
+
+ int i, iwarn;
+ double w, r, rd, rad, decd, v, x[3], usr[3], ust[3],
+ vsr, vst, betst, betsr, bett, betr,
+ dd, ddel, ur[3], ut[3],
+ d = 0.0, del = 0.0, /* to prevent */
+ odd = 0.0, oddel = 0.0, /* compiler */
+ od = 0.0, odel = 0.0; /* warnings */
+
+
+/* Distance (AU). */
+ if (px >= PXMIN) {
+ w = px;
+ iwarn = 0;
+ } else {
+ w = PXMIN;
+ iwarn = 1;
+ }
+ r = ERFA_DR2AS / w;
+
+/* Radial velocity (AU/day). */
+ rd = ERFA_DAYSEC * rv * 1e3 / ERFA_DAU;
+
+/* Proper motion (radian/day). */
+ rad = pmr / ERFA_DJY;
+ decd = pmd / ERFA_DJY;
+
+/* To pv-vector (AU,AU/day). */
+ eraS2pv(ra, dec, r, rad, decd, rd, pv);
+
+/* If excessive velocity, arbitrarily set it to zero. */
+ v = eraPm(pv[1]);
+ if (v / ERFA_DC > VMAX) {
+ eraZp(pv[1]);
+ iwarn += 2;
+ }
+
+/* Isolate the radial component of the velocity (AU/day). */
+ eraPn(pv[0], &w, x);
+ vsr = eraPdp(x, pv[1]);
+ eraSxp(vsr, x, usr);
+
+/* Isolate the transverse component of the velocity (AU/day). */
+ eraPmp(pv[1], usr, ust);
+ vst = eraPm(ust);
+
+/* Special-relativity dimensionless parameters. */
+ betsr = vsr / ERFA_DC;
+ betst = vst / ERFA_DC;
+
+/* Determine the inertial-to-observed relativistic correction terms. */
+ bett = betst;
+ betr = betsr;
+ for (i = 0; i < IMAX; i++) {
+ d = 1.0 + betr;
+ del = sqrt(1.0 - betr*betr - bett*bett) - 1.0;
+ betr = d * betsr + del;
+ bett = d * betst;
+ if (i > 0) {
+ dd = fabs(d - od);
+ ddel = fabs(del - odel);
+ if ((i > 1) && (dd >= odd) && (ddel >= oddel)) break;
+ odd = dd;
+ oddel = ddel;
+ }
+ od = d;
+ odel = del;
+ }
+ if (i >= IMAX) iwarn += 4;
+
+/* Replace observed radial velocity with inertial value. */
+ w = (betsr != 0.0) ? d + del / betsr : 1.0;
+ eraSxp(w, usr, ur);
+
+/* Replace observed tangential velocity with inertial value. */
+ eraSxp(d, ust, ut);
+
+/* Combine the two to obtain the inertial space velocity. */
+ eraPpp(ur, ut, pv[1]);
+
+/* Return the status. */
+ return iwarn;
+
+}
+/*----------------------------------------------------------------------
+**
+**
+** Copyright (C) 2013-2014, 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.
+**
+*/