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Fix header
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@ -1,5 +1,5 @@
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/*!
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* \file code_generation_test.cc
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* \file glonass_gnav_ephemeris_test.cc.cc
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* \note Code added as part of GSoC 2017 program
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* \author Damian Miralles, 2017. dmiralles2009(at)gmail.com
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* \see <a href="http://russianspacesystems.ru/wp-content/uploads/2016/08/ICD_GLONASS_eng_v5.1.pdf">GLONASS ICD</a>
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@ -7,7 +7,7 @@
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*
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* -------------------------------------------------------------------------
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*
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* Copyright (C) 2010-2015 (see AUTHORS file for a list of contributors)
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* Copyright (C) 2010-2017 (see AUTHORS file for a list of contributors)
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*
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* GNSS-SDR is a software defined Global Navigation
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* Satellite Systems receiver
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@ -32,7 +32,6 @@
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#include <complex>
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#include <ctime>
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#include <iostream>
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#include "gnss_signal_processing.h"
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#include "glonass_gnav_ephemeris.h"
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@ -49,19 +48,19 @@ TEST(GlonassGnavEphemerisTest, ComputeGlonassTime)
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d = d + d2;
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boost::gregorian::date expected_gdate;
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boost::posix_time::time_duration expected_gtime;
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boost::posix_time::time_duration expected_gtime;
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boost::posix_time::ptime gtime = gnav_eph.compute_GLONASS_time(7560);
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expected_gdate = gtime.date();
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expected_gtime = gtime.time_of_day();
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boost::posix_time::ptime gtime = gnav_eph.compute_GLONASS_time(7560);
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expected_gdate = gtime.date();
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expected_gtime = gtime.time_of_day();
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// Perform assertions of decoded fields
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ASSERT_TRUE(expected_gdate.year() - d.year() < FLT_EPSILON );
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ASSERT_TRUE(expected_gdate.month() - d.month() < FLT_EPSILON );
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ASSERT_TRUE(expected_gdate.day() - d.day() < FLT_EPSILON );
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ASSERT_TRUE(expected_gtime.hours() - t.hours() < FLT_EPSILON );
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ASSERT_TRUE(expected_gtime.minutes() - t.minutes() < FLT_EPSILON );
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ASSERT_TRUE(expected_gtime.seconds() - t.seconds() < FLT_EPSILON );
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ASSERT_TRUE(expected_gdate.year() - d.year() < FLT_EPSILON );
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ASSERT_TRUE(expected_gdate.month() - d.month() < FLT_EPSILON );
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ASSERT_TRUE(expected_gdate.day() - d.day() < FLT_EPSILON );
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ASSERT_TRUE(expected_gtime.hours() - t.hours() < FLT_EPSILON );
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ASSERT_TRUE(expected_gtime.minutes() - t.minutes() < FLT_EPSILON );
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ASSERT_TRUE(expected_gtime.seconds() - t.seconds() < FLT_EPSILON );
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}
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/*!
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@ -82,11 +81,11 @@ TEST(GlonassGnavEphemerisTest, ConvertGlonassT2GpsT1)
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double true_week = 1307;
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double true_tow = 480600+true_leap_sec;
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gnav_eph.glot_to_gpst(tod + glo2utc, 0.0, 0.0, &week, &tow);
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gnav_eph.glot_to_gpst(tod + glo2utc, 0.0, 0.0, &week, &tow);
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// Perform assertions of decoded fields
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ASSERT_TRUE(week - true_week < FLT_EPSILON );
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ASSERT_TRUE(tow - true_tow < FLT_EPSILON );
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ASSERT_TRUE(week - true_week < FLT_EPSILON );
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ASSERT_TRUE(tow - true_tow < FLT_EPSILON );
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}
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/*!
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@ -107,11 +106,11 @@ TEST(GlonassGnavEphemerisTest, ConvertGlonassT2GpsT2)
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double true_week = 1915;
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double true_tow = 518400+true_leap_sec+tod;
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gnav_eph.glot_to_gpst(tod + glo2utc, 0.0, 0.0, &week, &tow);
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gnav_eph.glot_to_gpst(tod + glo2utc, 0.0, 0.0, &week, &tow);
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// Perform assertions of decoded fields
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ASSERT_TRUE(week - true_week < FLT_EPSILON );
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ASSERT_TRUE(tow - true_tow < FLT_EPSILON );
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ASSERT_TRUE(week - true_week < FLT_EPSILON );
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ASSERT_TRUE(tow - true_tow < FLT_EPSILON );
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}
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/*!
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@ -132,9 +131,9 @@ TEST(GlonassGnavEphemerisTest, ConvertGlonassT2GpsT3)
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double true_week = 1886;
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double true_tow = 259200+true_leap_sec+tod;
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gnav_eph.glot_to_gpst(tod + glo2utc, 0.0, 0.0, &week, &tow);
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gnav_eph.glot_to_gpst(tod + glo2utc, 0.0, 0.0, &week, &tow);
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// Perform assertions of decoded fields
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ASSERT_TRUE(week - true_week < FLT_EPSILON );
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ASSERT_TRUE(tow - true_tow < FLT_EPSILON );
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ASSERT_TRUE(week - true_week < FLT_EPSILON );
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ASSERT_TRUE(tow - true_tow < FLT_EPSILON );
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}
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