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Improve data types for Galileo navigation data

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This commit is contained in:
Carles Fernandez 2018-12-14 00:42:05 +01:00
parent 3e4728225e
commit 6e665bdf29
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GPG Key ID: 4C583C52B0C3877D
12 changed files with 160 additions and 160 deletions
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8
src/core/system_parameters/Galileo_E1.h
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@ -103,7 +103,7 @@ const std::vector<std::pair<int32_t, int32_t>> PAGE_TYPE_bit({{1, 6}});
/*Page 1 - Word type 1: Ephemeris (1/4)*/
const std::vector<std::pair<int32_t, int32_t>> IOD_nav_1_bit({{7, 10}});
const std::vector<std::pair<int32_t, int32_t>> T0E_1_bit({{17, 14}});
const double t0e_1_LSB = 60;
const int32_t t0e_1_LSB = 60;
const std::vector<std::pair<int32_t, int32_t>> M0_1_bit({{31, 32}});
const double M0_1_LSB = PI_TWO_N31;
const std::vector<std::pair<int32_t, int32_t>> e_1_bit({{63, 32}});
@ -151,7 +151,7 @@ const double C_ic_4_LSB = TWO_N29;
const std::vector<std::pair<int32_t, int32_t>> C_is_4_bit({{39, 16}});
const double C_is_4_LSB = TWO_N29;
const std::vector<std::pair<int32_t, int32_t>> t0c_4_bit({{55, 14}}); //
const double t0c_4_LSB = 60;
const int32_t t0c_4_LSB = 60;
const std::vector<std::pair<int32_t, int32_t>> af0_4_bit({{69, 31}}); //
const double af0_4_LSB = TWO_N34;
const std::vector<std::pair<int32_t, int32_t>> af1_4_bit({{100, 21}}); //
@ -198,7 +198,7 @@ const std::vector<std::pair<int32_t, int32_t>> A1_6_bit({{39, 24}});
const double A1_6_LSB = TWO_N50;
const std::vector<std::pair<int32_t, int32_t>> Delta_tLS_6_bit({{63, 8}});
const std::vector<std::pair<int32_t, int32_t>> t0t_6_bit({{71, 8}});
const double t0t_6_LSB = 3600;
const int32_t t0t_6_LSB = 3600;
const std::vector<std::pair<int32_t, int32_t>> WNot_6_bit({{79, 8}});
const std::vector<std::pair<int32_t, int32_t>> WN_LSF_6_bit({{87, 8}});
const std::vector<std::pair<int32_t, int32_t>> DN_6_bit({{95, 3}});
@ -294,7 +294,7 @@ const double A_0G_10_LSB = TWO_N35;
const std::vector<std::pair<int32_t, int32_t>> A_1G_10_bit({{103, 12}});
const double A_1G_10_LSB = TWO_N51;
const std::vector<std::pair<int32_t, int32_t>> t_0G_10_bit({{115, 8}});
const double t_0G_10_LSB = 3600;
const int32_t t_0G_10_LSB = 3600;
const std::vector<std::pair<int32_t, int32_t>> WN_0G_10_bit({{123, 6}});

8
src/core/system_parameters/Galileo_E5a.h
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@ -83,7 +83,7 @@ const std::vector<std::pair<int32_t, int32_t>> FNAV_PAGE_TYPE_bit({{1, 6}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_SV_ID_PRN_1_bit({{7, 6}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_IODnav_1_bit({{13, 10}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_t0c_1_bit({{23, 14}});
const double FNAV_t0c_1_LSB = 60;
const int32_t FNAV_t0c_1_LSB = 60;
const std::vector<std::pair<int32_t, int32_t>> FNAV_af0_1_bit({{37, 31}});
const double FNAV_af0_1_LSB = TWO_N34;
const std::vector<std::pair<int32_t, int32_t>> FNAV_af1_1_bit({{68, 21}});
@ -143,7 +143,7 @@ const double FNAV_Crc_3_LSB = TWO_N5;
const std::vector<std::pair<int32_t, int32_t>> FNAV_Crs_3_bit({{145, 16}});
const double FNAV_Crs_3_LSB = TWO_N5;
const std::vector<std::pair<int32_t, int32_t>> FNAV_t0e_3_bit({{161, 14}});
const double FNAV_t0e_3_LSB = 60;
const int32_t FNAV_t0e_3_LSB = 60;
const std::vector<std::pair<int32_t, int32_t>> FNAV_WN_3_bit({{175, 12}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_TOW_3_bit({{187, 20}});
@ -159,13 +159,13 @@ const std::vector<std::pair<int32_t, int32_t>> FNAV_A1_4_bit({{81, 24}});
const double FNAV_A1_4_LSB = TWO_N50;
const std::vector<std::pair<int32_t, int32_t>> FNAV_deltatls_4_bit({{105, 8}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_t0t_4_bit({{113, 8}});
const double FNAV_t0t_4_LSB = 3600;
const int32_t FNAV_t0t_4_LSB = 3600;
const std::vector<std::pair<int32_t, int32_t>> FNAV_WNot_4_bit({{121, 8}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_WNlsf_4_bit({{129, 8}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_DN_4_bit({{137, 3}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_deltatlsf_4_bit({{140, 8}});
const std::vector<std::pair<int32_t, int32_t>> FNAV_t0g_4_bit({{148, 8}});
const double FNAV_t0g_4_LSB = 3600;
const int32_t FNAV_t0g_4_LSB = 3600;
const std::vector<std::pair<int32_t, int32_t>> FNAV_A0g_4_bit({{156, 16}});
const double FNAV_A0g_4_LSB = TWO_N35;
const std::vector<std::pair<int32_t, int32_t>> FNAV_A1g_4_bit({{172, 12}});

20
src/core/system_parameters/galileo_ephemeris.cc
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@ -54,26 +54,26 @@ Galileo_Ephemeris::Galileo_Ephemeris()
C_rs_3 = 0.0; // Amplitude of the sine harmonic correction term to the orbit radius [meters]
C_ic_4 = 0.0; // Amplitude of the cosine harmonic correction term to the angle of inclination [radians]
C_is_4 = 0.0; // Amplitude of the sine harmonic correction term to the angle of inclination [radians]
t0e_1 = 0.0; // Ephemeris reference time [s]
t0e_1 = 0; // Ephemeris reference time [s]
// Clock correction parameters
t0c_4 = 0.0; // Clock correction data reference Time of Week [sec]
t0c_4 = 0; // Clock correction data reference Time of Week [sec]
af0_4 = 0.0; // SV clock bias correction coefficient [s]
af1_4 = 0.0; // SV clock drift correction coefficient [s/s]
af2_4 = 0.0; // SV clock drift rate correction coefficient [s/s^2]
// GST
WN_5 = 0.0;
TOW_5 = 0.0;
WN_5 = 0;
TOW_5 = 0;
// SV status
SISA_3 = 0.0;
E5a_HS = 0U;
E5b_HS_5 = 0.0;
E1B_HS_5 = 0.0;
SISA_3 = 0;
E5a_HS = 0;
E5b_HS_5 = 0;
E1B_HS_5 = 0;
E5a_DVS = false;
E5b_DVS_5 = 0.0;
E1B_DVS_5 = 0.0;
E5b_DVS_5 = false;
E1B_DVS_5 = false;
BGD_E1E5a_5 = 0.0; // E1-E5a Broadcast Group Delay [s]
BGD_E1E5b_5 = 0.0; // E1-E5b Broadcast Group Delay [s]

28
src/core/system_parameters/galileo_ephemeris.h
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@ -67,29 +67,29 @@ public:
double C_rs_3; //!< Amplitude of the sine harmonic correction term to the orbit radius [meters]
double C_ic_4; //!< Amplitude of the cosine harmonic correction term to the angle of inclination [radians]
double C_is_4; //!< Amplitude of the sine harmonic correction term to the angle of inclination [radians]
double t0e_1; //!< Ephemeris reference time [s]
int32_t t0e_1; //!< Ephemeris reference time [s]
/*Clock correction parameters*/
double t0c_4; //!< Clock correction data reference Time of Week [sec]
double af0_4; //!< SV clock bias correction coefficient [s]
double af1_4; //!< SV clock drift correction coefficient [s/s]
double af2_4; //!< SV clock drift rate correction coefficient [s/s^2]
int32_t t0c_4; //!< Clock correction data reference Time of Week [sec]
double af0_4; //!< SV clock bias correction coefficient [s]
double af1_4; //!< SV clock drift correction coefficient [s/s]
double af2_4; //!< SV clock drift rate correction coefficient [s/s^2]
/*GST*/
//Not belong to ephemeris set (page 1 to 4)
double WN_5; //!< Week number
double TOW_5; //!< Time of Week
// Not belong to ephemeris set (page 1 to 4)
int32_t WN_5; //!< Week number
int32_t TOW_5; //!< Time of Week
double Galileo_satClkDrift;
double Galileo_dtr; //!< relativistic clock correction term
// SV status
double SISA_3;
uint32_t E5a_HS; //!< E5a Signal Health Status
double E5b_HS_5; //!< E5b Signal Health Status
double E1B_HS_5; //!< E1B Signal Health Status
int32_t SISA_3;
int32_t E5a_HS; //!< E5a Signal Health Status
int32_t E5b_HS_5; //!< E5b Signal Health Status
int32_t E1B_HS_5; //!< E1B Signal Health Status
bool E5a_DVS; //!< E5a Data Validity Status
double E5b_DVS_5; //!< E5b Data Validity Status
double E1B_DVS_5; //!< E1B Data Validity Status
bool E5b_DVS_5; //!< E5b Data Validity Status
bool E1B_DVS_5; //!< E1B Data Validity Status
double BGD_E1E5a_5; //!< E1-E5a Broadcast Group Delay [s]
double BGD_E1E5b_5; //!< E1-E5b Broadcast Group Delay [s]

70
src/core/system_parameters/galileo_fnav_message.cc
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@ -70,11 +70,11 @@ void Galileo_Fnav_Message::reset()
// health and Data validity status
FNAV_SV_ID_PRN_1 = 0;
FNAV_IODnav_1 = -1;
FNAV_t0c_1 = 0.0;
FNAV_t0c_1 = 0;
FNAV_af0_1 = 0.0;
FNAV_af1_1 = 0.0;
FNAV_af2_1 = 0.0;
FNAV_SISA_1 = 0.0;
FNAV_SISA_1 = 0;
FNAV_ai0_1 = 0.0;
FNAV_ai1_1 = 0.0;
FNAV_ai2_1 = 0.0;
@ -85,8 +85,8 @@ void Galileo_Fnav_Message::reset()
FNAV_region5_1 = false;
FNAV_BGD_1 = 0.0;
FNAV_E5ahs_1 = 0;
FNAV_WN_1 = 0.0;
FNAV_TOW_1 = 0.0;
FNAV_WN_1 = 0;
FNAV_TOW_1 = 0;
FNAV_E5advs_1 = false;
// WORD 2 Ephemeris (1/3) and GST
@ -97,8 +97,8 @@ void Galileo_Fnav_Message::reset()
FNAV_a12_2 = 0.0;
FNAV_omega0_2 = 0.0;
FNAV_idot_2 = 0.0;
FNAV_WN_2 = 0.0;
FNAV_TOW_2 = 0.0;
FNAV_WN_2 = 0;
FNAV_TOW_2 = 0;
// WORD 3 Ephemeris (2/3) and GST
FNAV_IODnav_3 = -3;
@ -109,9 +109,9 @@ void Galileo_Fnav_Message::reset()
FNAV_Cus_3 = 0.0;
FNAV_Crc_3 = 0.0;
FNAV_Crs_3 = 0.0;
FNAV_t0e_3 = 0.0;
FNAV_WN_3 = 0.0;
FNAV_TOW_3 = 0.0;
FNAV_t0e_3 = 0;
FNAV_WN_3 = 0;
FNAV_TOW_3 = 0;
// WORD 4 Ephemeris (3/3), GST-UTC conversion, GST-GPS conversion and TOW.
// Note that the clock is repeated in this page type
@ -120,17 +120,17 @@ void Galileo_Fnav_Message::reset()
FNAV_Cis_4 = 0.0;
FNAV_A0_4 = 0.0;
FNAV_A1_4 = 0.0;
FNAV_deltatls_4 = 0.0;
FNAV_t0t_4 = 0.0;
FNAV_WNot_4 = 0.0;
FNAV_WNlsf_4 = 0.0;
FNAV_DN_4 = 0.0;
FNAV_deltatlsf_4 = 0.0;
FNAV_t0g_4 = 0.0;
FNAV_deltatls_4 = 0;
FNAV_t0t_4 = 0;
FNAV_WNot_4 = 0;
FNAV_WNlsf_4 = 0;
FNAV_DN_4 = 0;
FNAV_deltatlsf_4 = 0;
FNAV_t0g_4 = 0;
FNAV_A0g_4 = 0.0;
FNAV_A1g_4 = 0.0;
FNAV_WN0g_4 = 0.0;
FNAV_TOW_4 = 0.0;
FNAV_WN0g_4 = 0;
FNAV_TOW_4 = 0;
// WORD 5 Almanac (SVID1 and SVID2(1/2)), Week Number and almanac reference time
FNAV_IODa_5 = 0;
@ -238,7 +238,7 @@ void Galileo_Fnav_Message::decode_page(const std::string& data)
case 1: // SVID, Clock correction, SISA, Ionospheric correction, BGD, GST, Signal health and Data validity status
FNAV_SV_ID_PRN_1 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_SV_ID_PRN_1_bit));
FNAV_IODnav_1 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_IODnav_1_bit));
FNAV_t0c_1 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_t0c_1_bit));
FNAV_t0c_1 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_t0c_1_bit));
FNAV_t0c_1 *= FNAV_t0c_1_LSB;
FNAV_af0_1 = static_cast<double>(read_navigation_signed(data_bits, FNAV_af0_1_bit));
FNAV_af0_1 *= FNAV_af0_1_LSB;
@ -246,7 +246,7 @@ void Galileo_Fnav_Message::decode_page(const std::string& data)
FNAV_af1_1 *= FNAV_af1_1_LSB;
FNAV_af2_1 = static_cast<double>(read_navigation_signed(data_bits, FNAV_af2_1_bit));
FNAV_af2_1 *= FNAV_af2_1_LSB;
FNAV_SISA_1 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_SISA_1_bit));
FNAV_SISA_1 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_SISA_1_bit));
FNAV_ai0_1 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_ai0_1_bit));
FNAV_ai0_1 *= FNAV_ai0_1_LSB;
FNAV_ai1_1 = static_cast<double>(read_navigation_signed(data_bits, FNAV_ai1_1_bit));
@ -261,8 +261,8 @@ void Galileo_Fnav_Message::decode_page(const std::string& data)
FNAV_BGD_1 = static_cast<double>(read_navigation_signed(data_bits, FNAV_BGD_1_bit));
FNAV_BGD_1 *= FNAV_BGD_1_LSB;
FNAV_E5ahs_1 = static_cast<uint32_t>(read_navigation_unsigned(data_bits, FNAV_E5ahs_1_bit));
FNAV_WN_1 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_WN_1_bit));
FNAV_TOW_1 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_TOW_1_bit));
FNAV_WN_1 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_WN_1_bit));
FNAV_TOW_1 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_TOW_1_bit));
FNAV_E5advs_1 = static_cast<bool>(read_navigation_unsigned(data_bits, FNAV_E5advs_1_bit));
flag_TOW_1 = true;
flag_TOW_set = true;
@ -282,8 +282,8 @@ void Galileo_Fnav_Message::decode_page(const std::string& data)
FNAV_omega0_2 *= FNAV_omega0_2_LSB;
FNAV_idot_2 = static_cast<double>(read_navigation_signed(data_bits, FNAV_idot_2_bit));
FNAV_idot_2 *= FNAV_idot_2_LSB;
FNAV_WN_2 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_WN_2_bit));
FNAV_TOW_2 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_TOW_2_bit));
FNAV_WN_2 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_WN_2_bit));
FNAV_TOW_2 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_TOW_2_bit));
flag_TOW_2 = true;
flag_TOW_set = true;
flag_ephemeris_1 = true;
@ -304,10 +304,10 @@ void Galileo_Fnav_Message::decode_page(const std::string& data)
FNAV_Crc_3 *= FNAV_Crc_3_LSB;
FNAV_Crs_3 = static_cast<double>(read_navigation_signed(data_bits, FNAV_Crs_3_bit));
FNAV_Crs_3 *= FNAV_Crs_3_LSB;
FNAV_t0e_3 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_t0e_3_bit));
FNAV_t0e_3 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_t0e_3_bit));
FNAV_t0e_3 *= FNAV_t0e_3_LSB;
FNAV_WN_3 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_WN_3_bit));
FNAV_TOW_3 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_TOW_3_bit));
FNAV_WN_3 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_WN_3_bit));
FNAV_TOW_3 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_TOW_3_bit));
flag_TOW_3 = true;
flag_TOW_set = true;
flag_ephemeris_2 = true;
@ -323,20 +323,20 @@ void Galileo_Fnav_Message::decode_page(const std::string& data)
FNAV_A1_4 = static_cast<double>(read_navigation_signed(data_bits, FNAV_A1_4_bit));
FNAV_A1_4 *= FNAV_A1_4_LSB;
FNAV_deltatls_4 = static_cast<double>(read_navigation_signed(data_bits, FNAV_deltatls_4_bit));
FNAV_t0t_4 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_t0t_4_bit));
FNAV_t0t_4 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_t0t_4_bit));
FNAV_t0t_4 *= FNAV_t0t_4_LSB;
FNAV_WNot_4 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_WNot_4_bit));
FNAV_WNlsf_4 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_WNlsf_4_bit));
FNAV_DN_4 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_DN_4_bit));
FNAV_deltatlsf_4 = static_cast<double>(read_navigation_signed(data_bits, FNAV_deltatlsf_4_bit));
FNAV_t0g_4 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_t0g_4_bit));
FNAV_WNot_4 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_WNot_4_bit));
FNAV_WNlsf_4 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_WNlsf_4_bit));
FNAV_DN_4 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_DN_4_bit));
FNAV_deltatlsf_4 = static_cast<int32_t>(read_navigation_signed(data_bits, FNAV_deltatlsf_4_bit));
FNAV_t0g_4 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_t0g_4_bit));
FNAV_t0g_4 *= FNAV_t0g_4_LSB;
FNAV_A0g_4 = static_cast<double>(read_navigation_signed(data_bits, FNAV_A0g_4_bit));
FNAV_A0g_4 *= FNAV_A0g_4_LSB;
FNAV_A1g_4 = static_cast<double>(read_navigation_signed(data_bits, FNAV_A1g_4_bit));
FNAV_A1g_4 *= FNAV_A1g_4_LSB;
FNAV_WN0g_4 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_WN0g_4_bit));
FNAV_TOW_4 = static_cast<double>(read_navigation_unsigned(data_bits, FNAV_TOW_4_bit));
FNAV_WN0g_4 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_WN0g_4_bit));
FNAV_TOW_4 = static_cast<int32_t>(read_navigation_unsigned(data_bits, FNAV_TOW_4_bit));
flag_TOW_4 = true;
flag_TOW_set = true;
flag_ephemeris_3 = true;

36
src/core/system_parameters/galileo_fnav_message.h
View File

@ -95,11 +95,11 @@ public:
// health and Data validity status
int32_t FNAV_SV_ID_PRN_1;
int32_t FNAV_IODnav_1;
double FNAV_t0c_1;
int32_t FNAV_t0c_1;
double FNAV_af0_1;
double FNAV_af1_1;
double FNAV_af2_1;
double FNAV_SISA_1;
int32_t FNAV_SISA_1;
double FNAV_ai0_1;
double FNAV_ai1_1;
double FNAV_ai2_1;
@ -110,8 +110,8 @@ public:
bool FNAV_region5_1;
double FNAV_BGD_1;
int32_t FNAV_E5ahs_1;
double FNAV_WN_1;
double FNAV_TOW_1;
int32_t FNAV_WN_1;
int32_t FNAV_TOW_1;
bool FNAV_E5advs_1;
// WORD 2 Ephemeris (1/3) and GST
@ -122,8 +122,8 @@ public:
double FNAV_a12_2;
double FNAV_omega0_2;
double FNAV_idot_2;
double FNAV_WN_2;
double FNAV_TOW_2;
int32_t FNAV_WN_2;
int32_t FNAV_TOW_2;
// WORD 3 Ephemeris (2/3) and GST
int32_t FNAV_IODnav_3;
@ -134,9 +134,9 @@ public:
double FNAV_Cus_3;
double FNAV_Crc_3;
double FNAV_Crs_3;
double FNAV_t0e_3;
double FNAV_WN_3;
double FNAV_TOW_3;
int32_t FNAV_t0e_3;
int32_t FNAV_WN_3;
int32_t FNAV_TOW_3;
// WORD 4 Ephemeris (3/3), GST-UTC conversion, GST-GPS conversion and TOW.
// Note that the clock is repeated in this page type
@ -145,17 +145,17 @@ public:
double FNAV_Cis_4;
double FNAV_A0_4;
double FNAV_A1_4;
double FNAV_deltatls_4;
double FNAV_t0t_4;
double FNAV_WNot_4;
double FNAV_WNlsf_4;
double FNAV_DN_4;
double FNAV_deltatlsf_4;
double FNAV_t0g_4;
int32_t FNAV_deltatls_4;
int32_t FNAV_t0t_4;
int32_t FNAV_WNot_4;
int32_t FNAV_WNlsf_4;
int32_t FNAV_DN_4;
int32_t FNAV_deltatlsf_4;
int32_t FNAV_t0g_4;
double FNAV_A0g_4;
double FNAV_A1g_4;
double FNAV_WN0g_4;
double FNAV_TOW_4;
int32_t FNAV_WN0g_4;
int32_t FNAV_TOW_4;
// WORD 5 Almanac (SVID1 and SVID2(1/2)), Week Number and almanac reference time
int32_t FNAV_IODa_5;

4
src/core/system_parameters/galileo_iono.cc
View File

@ -45,6 +45,6 @@ Galileo_Iono::Galileo_Iono()
Region4_flag_5 = false; // Ionospheric Disturbance Flag for region 4
Region5_flag_5 = false; // Ionospheric Disturbance Flag for region 5
TOW_5 = 0.0;
WN_5 = 0.0;
TOW_5 = 0;
WN_5 = 0;
}

4
src/core/system_parameters/galileo_iono.h
View File

@ -55,8 +55,8 @@ public:
bool Region5_flag_5; //!< Ionospheric Disturbance Flag for region 5
// from page 5 (UTC) to have a timestamp
double TOW_5; //!< UTC data reference Time of Week [s]
double WN_5; //!< UTC data reference Week number [week]
int32_t TOW_5; //!< UTC data reference Time of Week [s]
int32_t WN_5; //!< UTC data reference Week number [week]
/*!
* Default constructor

64
src/core/system_parameters/galileo_navigation_message.cc
View File

@ -74,7 +74,7 @@ void Galileo_Navigation_Message::reset()
// Word type 1: Ephemeris (1/4)
IOD_nav_1 = 0;
t0e_1 = 0.0;
t0e_1 = 0;
M0_1 = 0.0;
e_1 = 0.0;
A_1 = 0.0;
@ -94,7 +94,7 @@ void Galileo_Navigation_Message::reset()
C_us_3 = 0.0; // Amplitude of the sine harmonic correction term to the argument of latitude [radians]
C_rc_3 = 0.0; // Amplitude of the cosine harmonic correction term to the orbit radius [meters]
C_rs_3 = 0.0; // Amplitude of the sine harmonic correction term to the orbit radius [meters]
SISA_3 = 0.0; //
SISA_3 = 0; //
// Word type 4: Ephemeris (4/4) and Clock correction parameter/
IOD_nav_4 = 0;
@ -103,7 +103,7 @@ void Galileo_Navigation_Message::reset()
C_is_4 = 0.0; // Amplitude of the sine harmonic correction term to the angle of inclination [radians]
// Clock correction parameters
t0c_4 = 0.0;
t0c_4 = 0;
af0_4 = 0.0;
af1_4 = 0.0;
af2_4 = 0.0;
@ -129,20 +129,20 @@ void Galileo_Navigation_Message::reset()
E1B_DVS_5 = 0;
// GST
WN_5 = 0.0;
TOW_5 = 0.0;
WN_5 = 0;
TOW_5 = 0;
spare_5 = 0.0;
// Word type 6: GST-UTC conversion parameters
A0_6 = 0.0;
A1_6 = 0.0;
Delta_tLS_6 = 0.0;
t0t_6 = 0.0;
WNot_6 = 0.0;
Delta_tLS_6 = 0;
t0t_6 = 0;
WNot_6 = 0;
WN_LSF_6 = 0;
DN_6 = 0;
Delta_tLSF_6 = 0.0;
TOW_6 = 0.0;
Delta_tLSF_6 = 0;
TOW_6 = 0;
// Word type 7: Almanac for SVID1 (1/2), almanac reference time and almanac reference week number
IOD_a_7 = 0;
@ -199,13 +199,13 @@ void Galileo_Navigation_Message::reset()
// GST-GPS
A_0G_10 = 0.0;
A_1G_10 = 0.0;
t_0G_10 = 0.0;
WN_0G_10 = 0.0;
t_0G_10 = 0;
WN_0G_10 = 0;
// Word type 0: I/NAV Spare Word
Time_0 = 0.0;
WN_0 = 0.0;
TOW_0 = 0.0;
Time_0 = 0;
WN_0 = 0;
TOW_0 = 0;
flag_TOW_6 = false;
@ -653,7 +653,7 @@ int32_t Galileo_Navigation_Message::page_jk_decoder(const char* data_jk)
case 1: // Word type 1: Ephemeris (1/4)
IOD_nav_1 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, IOD_nav_1_bit));
DLOG(INFO) << "IOD_nav_1= " << IOD_nav_1;
t0e_1 = static_cast<double>(read_navigation_unsigned(data_jk_bits, T0E_1_bit));
t0e_1 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, T0E_1_bit));
t0e_1 = t0e_1 * t0e_1_LSB;
DLOG(INFO) << "t0e_1= " << t0e_1;
M0_1 = static_cast<double>(read_navigation_signed(data_jk_bits, M0_1_bit));
@ -709,7 +709,7 @@ int32_t Galileo_Navigation_Message::page_jk_decoder(const char* data_jk)
C_rs_3 = static_cast<double>(read_navigation_signed(data_jk_bits, C_rs_3_bit));
C_rs_3 = C_rs_3 * C_rs_3_LSB;
DLOG(INFO) << "C_rs_3= " << C_rs_3;
SISA_3 = static_cast<double>(read_navigation_unsigned(data_jk_bits, SISA_3_bit));
SISA_3 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, SISA_3_bit));
DLOG(INFO) << "SISA_3= " << SISA_3;
flag_ephemeris_3 = true;
DLOG(INFO) << "flag_tow_set" << flag_TOW_set;
@ -727,7 +727,7 @@ int32_t Galileo_Navigation_Message::page_jk_decoder(const char* data_jk)
C_is_4 = C_is_4 * C_is_4_LSB;
DLOG(INFO) << "C_is_4= " << C_is_4;
// Clock correction parameters
t0c_4 = static_cast<double>(read_navigation_unsigned(data_jk_bits, t0c_4_bit));
t0c_4 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, t0c_4_bit));
t0c_4 = t0c_4 * t0c_4_LSB;
DLOG(INFO) << "t0c_4= " << t0c_4;
af0_4 = static_cast<double>(read_navigation_signed(data_jk_bits, af0_4_bit));
@ -777,14 +777,14 @@ int32_t Galileo_Navigation_Message::page_jk_decoder(const char* data_jk)
DLOG(INFO) << "E5b_HS_5= " << E5b_HS_5;
E1B_HS_5 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, E1B_HS_5_bit));
DLOG(INFO) << "E1B_HS_5= " << E1B_HS_5;
E5b_DVS_5 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, E5b_DVS_5_bit));
E5b_DVS_5 = static_cast<bool>(read_navigation_unsigned(data_jk_bits, E5b_DVS_5_bit));
DLOG(INFO) << "E5b_DVS_5= " << E5b_DVS_5;
E1B_DVS_5 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, E1B_DVS_5_bit));
E1B_DVS_5 = static_cast<bool>(read_navigation_unsigned(data_jk_bits, E1B_DVS_5_bit));
DLOG(INFO) << "E1B_DVS_5= " << E1B_DVS_5;
// GST
WN_5 = static_cast<double>(read_navigation_unsigned(data_jk_bits, WN_5_bit));
WN_5 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, WN_5_bit));
DLOG(INFO) << "WN_5= " << WN_5;
TOW_5 = static_cast<double>(read_navigation_unsigned(data_jk_bits, TOW_5_bit));
TOW_5 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, TOW_5_bit));
DLOG(INFO) << "TOW_5= " << TOW_5;
flag_TOW_5 = true; // set to false externally
spare_5 = static_cast<double>(read_navigation_unsigned(data_jk_bits, spare_5_bit));
@ -801,20 +801,20 @@ int32_t Galileo_Navigation_Message::page_jk_decoder(const char* data_jk)
A1_6 = static_cast<double>(read_navigation_signed(data_jk_bits, A1_6_bit));
A1_6 = A1_6 * A1_6_LSB;
DLOG(INFO) << "A1_6= " << A1_6;
Delta_tLS_6 = static_cast<double>(read_navigation_signed(data_jk_bits, Delta_tLS_6_bit));
Delta_tLS_6 = static_cast<int32_t>(read_navigation_signed(data_jk_bits, Delta_tLS_6_bit));
DLOG(INFO) << "Delta_tLS_6= " << Delta_tLS_6;
t0t_6 = static_cast<double>(read_navigation_unsigned(data_jk_bits, t0t_6_bit));
t0t_6 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, t0t_6_bit));
t0t_6 = t0t_6 * t0t_6_LSB;
DLOG(INFO) << "t0t_6= " << t0t_6;
WNot_6 = static_cast<double>(read_navigation_unsigned(data_jk_bits, WNot_6_bit));
WNot_6 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, WNot_6_bit));
DLOG(INFO) << "WNot_6= " << WNot_6;
WN_LSF_6 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, WN_LSF_6_bit));
DLOG(INFO) << "WN_LSF_6= " << WN_LSF_6;
DN_6 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, DN_6_bit));
DLOG(INFO) << "DN_6= " << DN_6;
Delta_tLSF_6 = static_cast<double>(read_navigation_signed(data_jk_bits, Delta_tLSF_6_bit));
Delta_tLSF_6 = static_cast<int32_t>(read_navigation_signed(data_jk_bits, Delta_tLSF_6_bit));
DLOG(INFO) << "Delta_tLSF_6= " << Delta_tLSF_6;
TOW_6 = static_cast<double>(read_navigation_unsigned(data_jk_bits, TOW_6_bit));
TOW_6 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, TOW_6_bit));
DLOG(INFO) << "TOW_6= " << TOW_6;
flag_TOW_6 = true; // set to false externally
flag_utc_model = true; // set to false externally
@ -963,11 +963,11 @@ int32_t Galileo_Navigation_Message::page_jk_decoder(const char* data_jk)
A_1G_10 = A_1G_10 * A_1G_10_LSB;
flag_GGTO_2 = true;
DLOG(INFO) << "A_1G_10= " << A_1G_10;
t_0G_10 = static_cast<double>(read_navigation_unsigned(data_jk_bits, t_0G_10_bit));
t_0G_10 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, t_0G_10_bit));
t_0G_10 = t_0G_10 * t_0G_10_LSB;
flag_GGTO_3 = true;
DLOG(INFO) << "t_0G_10= " << t_0G_10;
WN_0G_10 = static_cast<double>(read_navigation_unsigned(data_jk_bits, WN_0G_10_bit));
WN_0G_10 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, WN_0G_10_bit));
flag_GGTO_4 = true;
DLOG(INFO) << "WN_0G_10= " << WN_0G_10;
flag_almanac_4 = true;
@ -975,11 +975,11 @@ int32_t Galileo_Navigation_Message::page_jk_decoder(const char* data_jk)
break;
case 0: // Word type 0: I/NAV Spare Word
Time_0 = static_cast<double>(read_navigation_unsigned(data_jk_bits, Time_0_bit));
Time_0 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, Time_0_bit));
DLOG(INFO) << "Time_0= " << Time_0;
WN_0 = static_cast<double>(read_navigation_unsigned(data_jk_bits, WN_0_bit));
WN_0 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, WN_0_bit));
DLOG(INFO) << "WN_0= " << WN_0;
TOW_0 = static_cast<double>(read_navigation_unsigned(data_jk_bits, TOW_0_bit));
TOW_0 = static_cast<int32_t>(read_navigation_unsigned(data_jk_bits, TOW_0_bit));
DLOG(INFO) << "TOW_0= " << TOW_0;
DLOG(INFO) << "flag_tow_set" << flag_TOW_set;
break;

48
src/core/system_parameters/galileo_navigation_message.h
View File

@ -93,7 +93,7 @@ public:
// Word type 1: Ephemeris (1/4)
int32_t IOD_nav_1; //!< IOD_nav page 1
double t0e_1; //!< Ephemeris reference time [s]
int32_t t0e_1; //!< Ephemeris reference time [s]
double M0_1; //!< Mean anomaly at reference time [semi-circles]
double e_1; //!< Eccentricity
double A_1; //!< Square root of the semi-major axis [meters^1/2]
@ -113,7 +113,7 @@ public:
double C_us_3; //!< Amplitude of the sine harmonic correction term to the argument of latitude [radians]
double C_rc_3; //!< Amplitude of the cosine harmonic correction term to the orbit radius [meters]
double C_rs_3; //!< Amplitude of the sine harmonic correction term to the orbit radius [meters]
double SISA_3;
int32_t SISA_3;
// Word type 4: Ephemeris (4/4) and Clock correction parameters*/
int32_t IOD_nav_4; //
@ -122,10 +122,10 @@ public:
double C_is_4; //!< Amplitude of the sine harmonic correction term to the angle of inclination [radians]
// Clock correction parameters
double t0c_4; //!< Clock correction data reference Time of Week [sec]
double af0_4; //!< SV clock bias correction coefficient [s]
double af1_4; //!< SV clock drift correction coefficient [s/s]
double af2_4; //!< clock drift rate correction coefficient [s/s^2]
int32_t t0c_4; //!< Clock correction data reference Time of Week [sec]
double af0_4; //!< SV clock bias correction coefficient [s]
double af1_4; //!< SV clock drift correction coefficient [s/s]
double af2_4; //!< clock drift rate correction coefficient [s/s^2]
double spare_4;
// Word type 5: Ionospheric correction, BGD, signal health and data validity status and GST*/
@ -143,26 +143,26 @@ public:
double BGD_E1E5a_5; //!< E1-E5a Broadcast Group Delay [s]
double BGD_E1E5b_5; //!< E1-E5b Broadcast Group Delay [s]
int32_t E5b_HS_5; //!< E5b Signal Health Status
int32_t E1B_HS_5; //!< E1B Signal Health Status
int32_t E5b_DVS_5; //!< E5b Data Validity Status
int32_t E1B_DVS_5; //!< E1B Data Validity Status
int32_t E5b_HS_5; //!< E5b Signal Health Status
int32_t E1B_HS_5; //!< E1B Signal Health Status
bool E5b_DVS_5; //!< E5b Data Validity Status
bool E1B_DVS_5; //!< E1B Data Validity Status
// GST
double WN_5;
double TOW_5;
int32_t WN_5;
int32_t TOW_5;
double spare_5;
// Word type 6: GST-UTC conversion parameters
double A0_6;
double A1_6;
double Delta_tLS_6;
double t0t_6;
double WNot_6;
int32_t Delta_tLS_6;
int32_t t0t_6;
int32_t WNot_6;
int32_t WN_LSF_6;
int32_t DN_6;
double Delta_tLSF_6;
double TOW_6;
int32_t Delta_tLSF_6;
int32_t TOW_6;
// Word type 7: Almanac for SVID1 (1/2), almanac reference time and almanac reference week number
int32_t IOD_a_7;
@ -217,15 +217,15 @@ public:
int32_t E1B_HS_10;
// GST-GPS conversion
double A_0G_10; //!< Constant term of the offset Delta t systems
double A_1G_10; //!< Rate of change of the offset Delta t systems
double t_0G_10; //!< Reference time for Galileo/GPS Time Offset (GGTO) data
double WN_0G_10; //!< Week Number of Galileo/GPS Time Offset (GGTO) reference
double A_0G_10; //!< Constant term of the offset Delta t systems
double A_1G_10; //!< Rate of change of the offset Delta t systems
int32_t t_0G_10; //!< Reference time for Galileo/GPS Time Offset (GGTO) data
int32_t WN_0G_10; //!< Week Number of Galileo/GPS Time Offset (GGTO) reference
// Word type 0: I/NAV Spare Word
double Time_0;
double WN_0;
double TOW_0;
int32_t Time_0;
int32_t WN_0;
int32_t TOW_0;
double Galileo_satClkDrift;
double Galileo_dtr; //!< Relativistic clock correction term

16
src/core/system_parameters/galileo_utc_model.cc
View File

@ -36,28 +36,28 @@ Galileo_Utc_Model::Galileo_Utc_Model()
// Word type 6: GST-UTC conversion parameters
A0_6 = 0.0;
A1_6 = 0.0;
Delta_tLS_6 = 0.0;
t0t_6 = 0.0;
WNot_6 = 0.0;
Delta_tLS_6 = 0;
t0t_6 = 0;
WNot_6 = 0;
WN_LSF_6 = 0;
DN_6 = 0;
Delta_tLSF_6 = 0.0;
Delta_tLSF_6 = 0;
flag_utc_model = false;
// GPS to Galileo GST conversion parameters
A_0G_10 = 0.0;
A_1G_10 = 0.0;
t_0G_10 = 0.0;
WN_0G_10 = 0.0;
t_0G_10 = 0;
WN_0G_10 = 0;
}
double Galileo_Utc_Model::GST_to_UTC_time(double t_e, int WN)
double Galileo_Utc_Model::GST_to_UTC_time(double t_e, int32_t WN)
{
double t_Utc;
double t_Utc_daytime;
double Delta_t_Utc = 0;
// Determine if the effectivity time of the leap second event is in the past
int weeksToLeapSecondEvent = WN_LSF_6 - (WN % 256);
int32_t weeksToLeapSecondEvent = WN_LSF_6 - (WN % 256);
if ((weeksToLeapSecondEvent) >= 0) // is not in the past
{

14
src/core/system_parameters/galileo_utc_model.h
View File

@ -47,22 +47,22 @@ public:
// Word type 6: GST-UTC conversion parameters
double A0_6;
double A1_6;
double Delta_tLS_6;
double t0t_6; //!< UTC data reference Time of Week [s]
double WNot_6; //!< UTC data reference Week number [week]
int32_t Delta_tLS_6;
int32_t t0t_6; //!< UTC data reference Time of Week [s]
int32_t WNot_6; //!< UTC data reference Week number [week]
int32_t WN_LSF_6;
int32_t DN_6;
double Delta_tLSF_6;
int32_t Delta_tLSF_6;
bool flag_utc_model;
// GPS to Galileo GST conversion parameters
double A_0G_10;
double A_1G_10;
double t_0G_10;
double WN_0G_10;
int32_t t_0G_10;
int32_t WN_0G_10;
//double TOW_6;
double GST_to_UTC_time(double t_e, int WN); //!< GST-UTC Conversion Algorithm and Parameters
double GST_to_UTC_time(double t_e, int32_t WN); //!< GST-UTC Conversion Algorithm and Parameters
/*!
* Default constructor
*/