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Merge branch 'next' of https://github.com/gnss-sdr/gnss-sdr into fpga

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This commit is contained in:
Marc Majoral
2018-08-14 14:40:14 +02:00
parent 5d968e3ba3 edf82644f2
commit 93b5ddc6f9
3 changed files with 13 additions and 17 deletions
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2
src/core/system_parameters/galileo_navigation_message.cc
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@@ -262,7 +262,7 @@ bool Galileo_Navigation_Message::CRC_test(std::bitset<GALILEO_DATA_FRAME_BITS> b
uint64_t Galileo_Navigation_Message::read_navigation_unsigned(std::bitset<GALILEO_DATA_JK_BITS> bits, const std::vector<std::pair<int32_t, int32_t> > parameter)
{
uint64_t value = 0;
uint64_t value = 0ULL;
int32_t num_of_slices = parameter.size();
for (int32_t i = 0; i < num_of_slices; i++)
{

6
src/core/system_parameters/glonass_gnav_navigation_message.cc
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@@ -230,7 +230,7 @@ bool Glonass_Gnav_Navigation_Message::read_navigation_bool(std::bitset<GLONASS_G
uint64_t Glonass_Gnav_Navigation_Message::read_navigation_unsigned(std::bitset<GLONASS_GNAV_STRING_BITS> bits, const std::vector<std::pair<int32_t, int32_t>> parameter)
{
uint64_t value = 0;
uint64_t value = 0ULL;
int32_t num_of_slices = parameter.size();
for (int32_t i = 0; i < num_of_slices; i++)
{
@@ -249,8 +249,8 @@ uint64_t Glonass_Gnav_Navigation_Message::read_navigation_unsigned(std::bitset<G
int64_t Glonass_Gnav_Navigation_Message::read_navigation_signed(std::bitset<GLONASS_GNAV_STRING_BITS> bits, const std::vector<std::pair<int32_t, int32_t>> parameter)
{
int64_t value = 0;
int64_t sign = 0;
int64_t value = 0LL;
int64_t sign = 0LL;
int32_t num_of_slices = parameter.size();
// read the MSB and perform the sign extension
if (bits[GLONASS_GNAV_STRING_BITS - parameter[0].first] == 1)

20
src/core/system_parameters/gps_navigation_message.h
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@@ -61,57 +61,53 @@ private:
public:
bool b_valid_ephemeris_set_flag; // flag indicating that this ephemeris set have passed the validation check
//broadcast orbit 1
// broadcast orbit 1
double d_TOW; //!< Time of GPS Week of the ephemeris set (taken from subframes TOW) [s]
double d_TOW_SF1; //!< Time of GPS Week from HOW word of Subframe 1 [s]
double d_TOW_SF2; //!< Time of GPS Week from HOW word of Subframe 2 [s]
double d_TOW_SF3; //!< Time of GPS Week from HOW word of Subframe 3 [s]
double d_TOW_SF4; //!< Time of GPS Week from HOW word of Subframe 4 [s]
double d_TOW_SF5; //!< Time of GPS Week from HOW word of Subframe 5 [s]
double d_IODE_SF2;
double d_IODE_SF3;
double d_Crs; //!< Amplitude of the Sine Harmonic Correction Term to the Orbit Radius [m]
double d_Delta_n; //!< Mean Motion Difference From Computed Value [semi-circles/s]
double d_M_0; //!< Mean Anomaly at Reference Time [semi-circles]
//broadcast orbit 2
// broadcast orbit 2
double d_Cuc; //!< Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude [rad]
double d_e_eccentricity; //!< Eccentricity [dimensionless]
double d_Cus; //!< Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude [rad]
double d_sqrt_A; //!< Square Root of the Semi-Major Axis [sqrt(m)]
//broadcast orbit 3
// broadcast orbit 3
double d_Toe; //!< Ephemeris data reference time of week (Ref. 20.3.3.4.3 IS-GPS-200E) [s]
double d_Toc; //!< clock data reference time (Ref. 20.3.3.3.3.1 IS-GPS-200E) [s]
double d_Cic; //!< Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination [rad]
double d_OMEGA0; //!< Longitude of Ascending Node of Orbit Plane at Weekly Epoch [semi-circles]
double d_Cis; //!< Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination [rad]
//broadcast orbit 4
// broadcast orbit 4
double d_i_0; //!< Inclination Angle at Reference Time [semi-circles]
double d_Crc; //!< Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius [m]
double d_OMEGA; //!< Argument of Perigee [semi-cicles]
double d_OMEGA_DOT; //!< Rate of Right Ascension [semi-circles/s]
//broadcast orbit 5
// broadcast orbit 5
double d_IDOT; //!< Rate of Inclination Angle [semi-circles/s]
int32_t i_code_on_L2; //!< If 1, P code ON in L2; if 2, C/A code ON in L2;
int32_t i_GPS_week; //!< GPS week number, aka WN [week]
bool b_L2_P_data_flag; //!< When true, indicates that the NAV data stream was commanded OFF on the P-code of the L2 channel
//broadcast orbit 6
// broadcast orbit 6
int32_t i_SV_accuracy; //!< User Range Accuracy (URA) index of the SV (reference paragraph 6.2.1) for the standard positioning service user (Ref 20.3.3.3.1.3 IS-GPS-200E)
int32_t i_SV_health;
double d_TGD; //!< Estimated Group Delay Differential: L1-L2 correction term only for the benefit of "L1 P(Y)" or "L2 P(Y)" s users [s]
double d_IODC; //!< Issue of Data, Clock
//broadcast orbit 7
// broadcast orbit 7
int32_t i_AODO; //!< Age of Data Offset (AODO) term for the navigation message correction table (NMCT) contained in subframe 4 (reference paragraph 20.3.3.5.1.9) [s]
bool b_fit_interval_flag; //!< indicates the curve-fit interval used by the CS (Block II/IIA/IIR/IIR-M/IIF) and SS (Block IIIA) in determining the ephemeris parameters, as follows: 0 = 4 hours, 1 = greater than 4 hours.
double d_spare1;
double d_spare2;
double d_A_f0; //!< Coefficient 0 of code phase offset model [s]
double d_A_f1; //!< Coefficient 1 of code phase offset model [s/s]
double d_A_f2; //!< Coefficient 2 of code phase offset model [s/s^2]
// Almanac
double d_Toa; //!< Almanac reference time [s]
int32_t i_WN_A; //!< Modulo 256 of the GPS week number to which the almanac reference time (d_Toa) is referenced
@@ -151,7 +147,7 @@ public:
uint32_t i_satellite_PRN;
// time synchro
double d_subframe_timestamp_ms; //[ms]
double d_subframe_timestamp_ms; // [ms]
// Ionospheric parameters
bool flag_iono_valid; //!< If set, it indicates that the ionospheric parameters are filled (page 18 has arrived and decoded)