/*
*+
*  Name:
*     palPlante

*  Purpose:
*     Topocentric RA,Dec of a Solar-System object from heliocentric orbital elements

*  Language:
*     Starlink ANSI C

*  Type of Module:
*     Library routine

*  Invocation:
*     void palPlante ( double date, double elong, double phi, int jform,
*                      double epoch, double orbinc, double anode, double perih,
*                      double aorq, double e, double aorl, double dm,
*                      double *ra, double *dec, double *r, int *jstat );


*  Description:
*     Topocentric apparent RA,Dec of a Solar-System object whose
*     heliocentric orbital elements are known.

*  Arguments:
*     date = double (Given)
*        TT MJD of observation (JD-2400000.5)
*     elong = double (Given)
*        Observer's east longitude (radians)
*     phi = double (Given)
*        Observer's geodetic latitude (radians)
*     jform = int (Given)
*        Element set actually returned (1-3; Note 6)
*     epoch = double (Given)
*        Epoch of elements (TT MJD)
*     orbinc = double (Given)
*        inclination (radians)
*     anode = double (Given)
*        longitude of the ascending node (radians)
*     perih = double (Given)
*        longitude or argument of perihelion (radians)
*     aorq = double (Given)
*        mean distance or perihelion distance (AU)
*     e = double (Given)
*        eccentricity
*     aorl = double (Given)
*        mean anomaly or longitude (radians, JFORM=1,2 only)
*     dm = double (Given)
*        daily motion (radians, JFORM=1 only)
*     ra = double * (Returned)
*        Topocentric apparent RA (radians)
*     dec = double * (Returned)
*        Topocentric apparent Dec (radians)
*     r = double * (Returned)
*        Distance from observer (AU)
*     jstat = int * (Returned)
*        status: 0 = OK
*             - -1 = illegal jform
*             - -2 = illegal e
*             - -3 = illegal aorq
*             - -4 = illegal dm
*             - -5 = numerical error

*  Authors:
*     PTW: Pat Wallace (STFC)
*     TIMJ: Tim Jenness (JAC, Hawaii)
*     {enter_new_authors_here}

*  Notes:
*     - DATE is the instant for which the prediction is required.  It is
*       in the TT timescale (formerly Ephemeris Time, ET) and is a
*       Modified Julian Date (JD-2400000.5).
*     - The longitude and latitude allow correction for geocentric
*       parallax.  This is usually a small effect, but can become
*       important for near-Earth asteroids.  Geocentric positions can be
*       generated by appropriate use of routines palEpv (or palEvp) and
*       palUe2pv.
*     - The elements are with respect to the J2000 ecliptic and equinox.
*     - A choice of three different element-set options is available:
*
*       Option JFORM = 1, suitable for the major planets:
*
*         EPOCH  = epoch of elements (TT MJD)
*         ORBINC = inclination i (radians)
*         ANODE  = longitude of the ascending node, big omega (radians)
*         PERIH  = longitude of perihelion, curly pi (radians)
*         AORQ   = mean distance, a (AU)
*         E      = eccentricity, e (range 0 to <1)
*         AORL   = mean longitude L (radians)
*         DM     = daily motion (radians)
*
*       Option JFORM = 2, suitable for minor planets:
*
*         EPOCH  = epoch of elements (TT MJD)
*         ORBINC = inclination i (radians)
*         ANODE  = longitude of the ascending node, big omega (radians)
*         PERIH  = argument of perihelion, little omega (radians)
*         AORQ   = mean distance, a (AU)
*         E      = eccentricity, e (range 0 to <1)
*         AORL   = mean anomaly M (radians)
*
*       Option JFORM = 3, suitable for comets:
*
*         EPOCH  = epoch of elements and perihelion (TT MJD)
*         ORBINC = inclination i (radians)
*         ANODE  = longitude of the ascending node, big omega (radians)
*         PERIH  = argument of perihelion, little omega (radians)
*         AORQ   = perihelion distance, q (AU)
*         E      = eccentricity, e (range 0 to 10)
*
*       Unused arguments (DM for JFORM=2, AORL and DM for JFORM=3) are not
*       accessed.
*     - Each of the three element sets defines an unperturbed heliocentric
*       orbit.  For a given epoch of observation, the position of the body
*       in its orbit can be predicted from these elements, which are
*       called "osculating elements", using standard two-body analytical
*       solutions.  However, due to planetary perturbations, a given set
*       of osculating elements remains usable for only as long as the
*       unperturbed orbit that it describes is an adequate approximation
*       to reality.  Attached to such a set of elements is a date called
*       the "osculating epoch", at which the elements are, momentarily,
*       a perfect representation of the instantaneous position and
*       velocity of the body.
*
*       Therefore, for any given problem there are up to three different
*       epochs in play, and it is vital to distinguish clearly between
*       them:
*
*       . The epoch of observation:  the moment in time for which the
*         position of the body is to be predicted.
*
*       . The epoch defining the position of the body:  the moment in time
*         at which, in the absence of purturbations, the specified
*         position (mean longitude, mean anomaly, or perihelion) is
*         reached.
*
*       . The osculating epoch:  the moment in time at which the given
*         elements are correct.
*
*       For the major-planet and minor-planet cases it is usual to make
*       the epoch that defines the position of the body the same as the
*       epoch of osculation.  Thus, only two different epochs are
*       involved:  the epoch of the elements and the epoch of observation.
*
*       For comets, the epoch of perihelion fixes the position in the
*       orbit and in general a different epoch of osculation will be
*       chosen.  Thus, all three types of epoch are involved.
*
*       For the present routine:
*
*       . The epoch of observation is the argument DATE.
*
*       . The epoch defining the position of the body is the argument
*         EPOCH.
*
*       . The osculating epoch is not used and is assumed to be close
*         enough to the epoch of observation to deliver adequate accuracy.
*         If not, a preliminary call to sla_PERTEL may be used to update
*         the element-set (and its associated osculating epoch) by
*         applying planetary perturbations.
*     - Two important sources for orbital elements are Horizons, operated
*       by the Jet Propulsion Laboratory, Pasadena, and the Minor Planet
*       Center, operated by the Center for Astrophysics, Harvard.
*
*       The JPL Horizons elements (heliocentric, J2000 ecliptic and
*       equinox) correspond to SLALIB arguments as follows.
*
*        Major planets:
*
*         JFORM  = 1
*         EPOCH  = JDCT-2400000.5
*         ORBINC = IN (in radians)
*         ANODE  = OM (in radians)
*         PERIH  = OM+W (in radians)
*         AORQ   = A
*         E      = EC
*         AORL   = MA+OM+W (in radians)
*         DM     = N (in radians)
*
*         Epoch of osculation = JDCT-2400000.5
*
*        Minor planets:
*
*         JFORM  = 2
*         EPOCH  = JDCT-2400000.5
*         ORBINC = IN (in radians)
*         ANODE  = OM (in radians)
*         PERIH  = W (in radians)
*         AORQ   = A
*         E      = EC
*         AORL   = MA (in radians)
*
*         Epoch of osculation = JDCT-2400000.5
*
*        Comets:
*
*         JFORM  = 3
*         EPOCH  = Tp-2400000.5
*         ORBINC = IN (in radians)
*         ANODE  = OM (in radians)
*         PERIH  = W (in radians)
*         AORQ   = QR
*         E      = EC
*
*         Epoch of osculation = JDCT-2400000.5
*
*      The MPC elements correspond to SLALIB arguments as follows.
*
*        Minor planets:
*
*         JFORM  = 2
*         EPOCH  = Epoch-2400000.5
*         ORBINC = Incl. (in radians)
*         ANODE  = Node (in radians)
*         PERIH  = Perih. (in radians)
*         AORQ   = a
*         E      = e
*         AORL   = M (in radians)
*
*         Epoch of osculation = Epoch-2400000.5
*
*       Comets:
*
*         JFORM  = 3
*         EPOCH  = T-2400000.5
*         ORBINC = Incl. (in radians)
*         ANODE  = Node. (in radians)
*         PERIH  = Perih. (in radians)
*         AORQ   = q
*         E      = e
*
*         Epoch of osculation = Epoch-2400000.5

*  History:
*     2012-03-12 (TIMJ):
*        Initial version direct conversion of SLA/F.
*        Adapted with permission from the Fortran SLALIB library.
*     {enter_further_changes_here}

*  Copyright:
*     Copyright (C) 2004 Patrick T. Wallace
*     Copyright (C) 2012 Science and Technology Facilities Council.
*     All Rights Reserved.

*  Licence:
*     This program is free software; you can redistribute it and/or
*     modify it under the terms of the GNU General Public License as
*     published by the Free Software Foundation; either version 3 of
*     the License, or (at your option) any later version.
*
*     This program is distributed in the hope that it will be
*     useful, but WITHOUT ANY WARRANTY; without even the implied
*     warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR
*     PURPOSE. See the GNU General Public License for more details.
*
*     You should have received a copy of the GNU General Public License
*     along with this program; if not, write to the Free Software
*     Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston,
*     MA 02110-1301, USA.

*  Bugs:
*     {note_any_bugs_here}
*-
*/

#include "pal.h"

void palPlante ( double date, double elong, double phi, int jform,
		 double epoch, double orbinc, double anode, double perih,
		 double aorq, double e, double aorl, double dm,
		 double *ra, double *dec, double *r, int *jstat ) {

  double u[13];

  /* Transform conventional elements to universal elements */
  palEl2ue( date, jform, epoch, orbinc, anode, perih, aorq, e, aorl,
	    dm, u, jstat );

  /* If succcessful, make the prediction */
  if (*jstat == 0) palPlantu( date, elong, phi, u, ra, dec, r, jstat );

}