File: mexmultiple.m

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% /*-----------------------------------------------------------------*/
% /*! 
%   \file mexmultiple.m 
%   \brief Example of usage of the multiple file access functions 
%          with the Octave/Matlab interface.
%          This example reads the constant EMRAT, AU, GM_Mer and print their values.
%          It computes for a date
%           the geocentric moon coordinates, 
%           the value TT-TDB 
%           the heliocentric coordinates of Mars.
% 
%   \author  M. Gastineau 
%            Astronomie et Systemes Dynamiques, IMCCE, CNRS, Observatoire de Paris. 
% 
%    Copyright,  2018-2023, CNRS
%    email of the author : Mickael.Gastineau@obspm.fr
% 
%   History:                                                                
% */
% /*-----------------------------------------------------------------*/
% 
%  
% /*-----------------------------------------------------------------*/
% /* License  of this file :
%  This file is 'triple-licensed', you have to choose one  of the three licenses 
%  below to apply on this file.
%  
%     CeCILL-C
%     	The CeCILL-C license is close to the GNU LGPL.
%     	( http://www.cecill.info/licences/Licence_CeCILL-C_V1-en.html )
%    
%  or CeCILL-B
%         The CeCILL-B license is close to the BSD.
%         (http://www.cecill.info/licences/Licence_CeCILL-B_V1-en.txt)
%   
%  or CeCILL v2.1
%       The CeCILL license is compatible with the GNU GPL.
%       ( http://www.cecill.info/licences/Licence_CeCILL_V2.1-en.html )
%  
% 
%  This library is governed by the CeCILL-C, CeCILL-B or the CeCILL license under 
%  French law and abiding by the rules of distribution of free software.  
%  You can  use, modify and/ or redistribute the software under the terms 
%  of the CeCILL-C,CeCILL-B or CeCILL license as circulated by CEA, CNRS and INRIA  
%  at the following URL 'http://www.cecill.info'. 
%  
%  As a counterpart to the access to the source code and  rights to copy,
%  modify and redistribute granted by the license, users are provided only
%  with a limited warranty  and the software's author,  the holder of the
%  economic rights,  and the successive licensors  have only  limited
%  liability. 
%  
%  In this respect, the user's attention is drawn to the risks associated
%  with loading,  using,  modifying and/or developing or reproducing the
%  software by the user in light of its specific status of free software,
%  that may mean  that it is complicated to manipulate,  and  that  also
%  therefore means  that it is reserved for developers  and  experienced
%  professionals having in-depth computer knowledge. Users are therefore
%  encouraged to load and test the software's suitability as regards their
%  requirements in conditions enabling the security of their systems and/or 
%  data to be ensured and,  more generally, to use and operate it in the 
%  same conditions as regards security. 
%  
%  The fact that you are presently reading this means that you have had
%  knowledge of the CeCILL-C,CeCILL-B or CeCILL license and that you accept its terms.
%  */
%  /*-----------------------------------------------------------------*/

% /*-----------------------------------------------------------------*/
% /* main program */
% /*-----------------------------------------------------------------*/
    jd0=2442457
    dt=0.5E0
    % open the ephemeris file 
    peph = CalcephBin.open('example1.dat');
    disp('The ephemeris is already opened\n')

    % print the values of AU, EMRAT and GM_Mer 
    AU = peph.getconstant('AU')
    EMRAT = peph.getconstant('EMRAT')
    GM_Mer = peph.getconstant('GM_Mer')
 
    % compute and print the coordinates 
    % the geocentric moon coordinates 
    disp('geocentric coordinates of the Moon in AU and AU/day')
    [ found, moon ] = peph.getidbyname("Moon",0)
    [ found, earth ] = peph.getidbyname("Earth",0)
    PV = peph.compute(jd0, dt, moon, earth)
    disp('geocentric coordinates of the Moon in km and km/s')
    PV = peph.compute_unit(jd0, dt, NaifId.MOON, NaifId.EARTH, 
                           Constants.UNIT_KM+Constants.UNIT_SEC+Constants.USE_NAIFID)

    % the value TT-TDB 
    PV = peph.compute(jd0, dt, 16, 0);
    printf('TT-TDB = %f\n',PV(1));

    % the heliocentric coordinates of Mars 
    disp('heliocentric coordinates of Mars')
    PV = peph.compute_unit(jd0, dt, NaifId.MARS_BARYCENTER, NaifId.SUN, 
                           Constants.UNIT_AU+Constants.UNIT_DAY+Constants.USE_NAIFID)
 
 
    % print the whole list of the constants
    disp('list of constants');
    for j=1:peph.getconstantcount()
        [ nameconstant, valueconstant ] = peph.getconstantindex(j);
        printf('%s\t= %e\n',nameconstant, valueconstant)
    end   
    % close the ephemeris file 
    peph.close();
    disp('The ephemeris is already closed');