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https://github.com/csete/gpredict
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1589991e65
git-svn-id: https://gpredict.svn.sourceforge.net/svnroot/gpredict/trunk@122 ab6734ba-2843-0410-b83b-99c217ef6c0f
108 lines
3.9 KiB
C
108 lines
3.9 KiB
C
/* -*- Mode: C; tab-width: 4; indent-tabs-mode: t; c-basic-offset: 4 -*- */
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/*
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Gpredict: Real-time satellite tracking and orbit prediction program
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Copyright (C) 2001-2008 Alexandru Csete, OZ9AEC.
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Parts are Copyright John A. Magliacane, KD2BD 1991-2003 (indicated below)
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Authors: Alexandru Csete <oz9aec@gmail.com>
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John A. Magliacane, KD2BD.
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Comments, questions and bugreports should be submitted via
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http://sourceforge.net/projects/gpredict/
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More details can be found at the project home page:
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http://gpredict.oz9aec.net/
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This program is free software; you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation; either version 2 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program; if not, visit http://www.fsf.org/
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*/
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#include <glib.h>
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#include <glib/gi18n.h>
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#include "sgpsdp/sgp4sdp4.h"
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#include "sat-log.h"
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#ifdef HAVE_CONFIG_H
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# include <build-config.h>
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#endif
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#include "tle-tools.h"
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/** \brief Convert NASA 2-line orbital element set to tle_t structure.
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* \param line1 The first line containing the satellite name.
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* \param line2 The second line.
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* \param line3 The third line.
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* \param checksum Flag indicating whether to perform checksum check.
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* \param tle Pointer to a tle_t structure where the TLE data will be put.
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* \return TLE_CONV_SUCCESS if the conversion is successful or TLE_CONV_ERROR
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* if an error has occurred during the conversion.
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*
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* This function converts NASA 2-line orbital element data (as read from a tle
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* file) into a tle_t structure, which is used all over in gpredict. Note that
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* a standard 2-line data actually consists of three lines, the extra line
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* containing the name of the satellite in a field of 25 characters.
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*
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* The flag checksum can be used to control whether verification of the checksum
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* should be fperformed or not. If the flag is TRUE and the checksum is invalid,
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* an error message is logged and the function returns TLE_CONV_ERROR. The caller
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* can still ignore the error code since the tle structure will be populated;
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* however, the data may be nonsense.
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*/
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gint
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twoline2tle (gchar *line1, gchar *line2, gchar *line3,
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gboolean checksum, tle_t *tle)
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{
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/* check function parameters */
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if G_UNLIKELY((line1 == NULL) || (line2 == NULL) || (line3 == NULL)) {
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sat_log_log (SAT_LOG_LEVEL_BUG,
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_("%s: NULL input data!"), __FUNCTION__);
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return TLE_CONV_ERROR;
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}
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if G_UNLIKELY(tle == NULL) {
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sat_log_log (SAT_LOG_LEVEL_BUG,
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_("%s: NULL output storage!"), __FUNCTION__);
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return TLE_CONV_ERROR;
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}
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return TLE_CONV_SUCCESS;
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}
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/** \brief Convert internal tle_t structure to NASA 2-line oribital element set.
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* \param tle Pointer to the tle_t structure that holds the data to be
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* converted.
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* \param line1 Pointer to unallocated memory where the first line will be
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* stored. The pointer should be freed when no longer needed.
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* \param line2 Pointer to unallocated memory where the second line will be
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* stored. The pointer should be freed when no longer needed.
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* \param line3 Pointer to unallocated memory where the third line will be
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* stored. The pointer should be freed when no longer needed.
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* \return TLE_CONV_SUCCESS if conversion went OK, TLE_CONV_ERROR otherwise.
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*
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* \note An error message will be logged if an error occurs.
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*/
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gint
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tle2twoline (tle_t *tle, gchar *line1, gchar *line2, gchar *line3)
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{
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return TLE_CONV_SUCCESS;
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}
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