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Minor documentation improvements

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git-svn-id: https://svn.code.sf.net/p/gnss-sdr/code/trunk@449 64b25241-fba3-4117-9849-534c7e92360d
This commit is contained in:
Carles Fernandez 2013-11-24 23:55:32 +00:00
parent 3daf65bfc4
commit de9415571d
7 changed files with 43 additions and 65 deletions
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14
src/algorithms/PVT/gnuradio_blocks/galileo_e1_pvt_cc.h
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@ -1,10 +1,11 @@
/*!
* \file gps_l1_ca_pvt_cc.h
* \file galileo_e1_pvt_cc.h
* \brief Interface of a Position Velocity and Time computation block for Galileo E1
* \author Javier Arribas, 2011. jarribas(at)cttc.es
* \author Javier Arribas, 2013. jarribas(at)cttc.es
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2012 (see AUTHORS file for a list of contributors)
* Copyright (C) 2010-2013 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
@ -56,7 +57,7 @@ galileo_e1_pvt_cc_sptr
galileo_e1_make_pvt_cc(unsigned int n_channels, boost::shared_ptr<gr::msg_queue> queue, bool dump, std::string dump_filename, int averaging_depth, bool flag_averaging, int output_rate_ms, int display_rate_ms, bool flag_nmea_tty_port, std::string nmea_dump_filename, std::string nmea_dump_devname);
/*!
* \brief This class implements a block that computes the PVT solution
* \brief This class implements a block that computes the PVT solution with Galileo E1 signals
*/
class galileo_e1_pvt_cc : public gr::block
{
@ -81,13 +82,10 @@ private:
Nmea_Printer *d_nmea_printer;
double d_rx_time;
galileo_e1_ls_pvt *d_ls_pvt; /*modify PVT/libs/galileo_e1_ls_pvt*/
bool pseudoranges_pairCompare_min( std::pair<int,Gnss_Synchro> a, std::pair<int,Gnss_Synchro> b);
public:
~galileo_e1_pvt_cc (); //!< Default destructor
/*!
* \brief Set the queue for getting navigation messages from the GpsL1CaTelemetryDecoder
*/
int general_work (int noutput_items, gr_vector_int &ninput_items,
gr_vector_const_void_star &input_items, gr_vector_void_star &output_items); //!< PVT Signal Processing

3
src/algorithms/PVT/gnuradio_blocks/gps_l1_ca_pvt_cc.h
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@ -83,9 +83,6 @@ private:
public:
~gps_l1_ca_pvt_cc (); //!< Default destructor
/*!
* \brief Set the queue for getting navigation messages from the GpsL1CaTelemetryDecoder
*/
int general_work (int noutput_items, gr_vector_int &ninput_items,
gr_vector_const_void_star &input_items, gr_vector_void_star &output_items); //!< PVT Signal Processing

3
src/algorithms/observables/gnuradio_blocks/galileo_e1_observables_cc.cc
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@ -3,9 +3,10 @@
* \brief Implementation of the pseudorange computation block for GPS L1 C/A
* \author Mara Branzanti 2013. mara.branzanti(at)gmail.com
* \author Javier Arribas 2013. jarribas(at)cttc.es
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2012 (see AUTHORS file for a list of contributors)
* Copyright (C) 2010-2013 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver

9
src/algorithms/observables/gnuradio_blocks/galileo_e1_observables_cc.h
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@ -1,11 +1,12 @@
/*!
* \file gps_l1_ca_observables_cc.h
* \brief Interface of the pseudorange computation block for GPS L1 C/A
* \file galileo_e1_observables_cc.h
* \brief Interface of the observables computation block for Galileo E1
* \author Mara Branzanti 2013. mara.branzanti(at)gmail.com
* \author Javier Arribas 2013. jarribas(at)cttc.es
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2012 (see AUTHORS file for a list of contributors)
* Copyright (C) 2010-2013 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
@ -54,7 +55,7 @@ galileo_e1_observables_cc_sptr
galileo_e1_make_observables_cc(unsigned int n_channels, boost::shared_ptr<gr::msg_queue> queue, bool dump, std::string dump_filename, int output_rate_ms, bool flag_averaging);
/*!
* \brief This class implements a block that computes Galielo observables
* \brief This class implements a block that computes Galileo observables
*/
class galileo_e1_observables_cc : public gr::block
{

72
src/core/system_parameters/galileo_ephemeris.h
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@ -1,8 +1,9 @@
/*!
* \file galileo_navigation_message.h
* \file galileo_ephemeris.h
* \brief Interface of a Galileo EPHEMERIS storage
* \author Javier Arribas, 2013. jarribas(at)cttc.es
* \author Javier Arribas, 2013. jarribas(at)cttc.es,
* \author Mara Branzanti 2013. mara.branzanti(at)gmail.com
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2013 (see AUTHORS file for a list of contributors)
@ -40,6 +41,7 @@
/*!
* \brief This class is a storage and orbital model functions for the Galileo SV ephemeris data as described in Galileo ICD paragraph 5.1.1
* (See http://ec.europa.eu/enterprise/policies/satnav/galileo/files/galileo-os-sis-icd-issue1-revision1_en.pdf )
*
*/
class Galileo_Ephemeris
@ -99,56 +101,36 @@ public:
double sv_clock_relativistic_term(double transmitTime); //!< Satellite Time Correction Algorithm, ICD 5.1.4
Galileo_Ephemeris();
/*
template<class Archive>
\\brief Serialize is a boost standard method to be called by the boost XML serialization. Here is used to save the ephemeris data on disk file.
/*!
* \brief Serialize is a boost standard method to be called by the boost XML serialization. Here is used to save the ephemeris data on disk file.
*/
void serialize(Archive& archive, const unsigned int version)
{
using boost::serialization::make_nvp;
archive & make_nvp("i_satellite_PRN",i_satellite_PRN); // SV PRN NUMBER
archive & make_nvp("d_TOW",d_TOW); //!< Time of GPS Week of the ephemeris set (taken from subframes TOW) [s]
archive & make_nvp("d_Crs",d_Crs); //!< Amplitude of the Sine Harmonic Correction Term to the Orbit Radius [m]
archive & make_nvp("d_Delta_n",d_Delta_n); //!< Mean Motion Difference From Computed Value [semi-circles/s]
archive & make_nvp("d_M_0",d_M_0); //!< Mean Anomaly at Reference Time [semi-circles]
archive & make_nvp("d_Cuc",d_Cuc); //!< Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude [rad]
archive & make_nvp("d_e_eccentricity",d_e_eccentricity); //!< Eccentricity [dimensionless]
archive & make_nvp("d_Cus",d_Cus); //!< Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude [rad]
archive & make_nvp("d_sqrt_A",d_sqrt_A); //!< Square Root of the Semi-Major Axis [sqrt(m)]
archive & make_nvp("d_Toe",d_Toe); //!< Ephemeris data reference time of week (Ref. 20.3.3.4.3 IS-GPS-200E) [s]
archive & make_nvp("d_Toc",d_Toe); //!< clock data reference time (Ref. 20.3.3.3.3.1 IS-GPS-200E) [s]
archive & make_nvp("d_Cic",d_Cic); //!< Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination [rad]
archive & make_nvp("d_OMEGA0",d_OMEGA0); //!< Longitude of Ascending Node of Orbit Plane at Weekly Epoch [semi-circles]
archive & make_nvp("d_Cis",d_Cis); //!< Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination [rad]
archive & make_nvp("d_i_0",d_i_0); //!< Inclination Angle at Reference Time [semi-circles]
archive & make_nvp("d_Crc",d_Crc); //!< Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius [m]
archive & make_nvp("d_OMEGA",d_OMEGA); //!< Argument of Perigee [semi-cicles]
archive & make_nvp("d_OMEGA_DOT",d_OMEGA_DOT); //!< Rate of Right Ascension [semi-circles/s]
archive & make_nvp("d_IDOT",d_IDOT); //!< Rate of Inclination Angle [semi-circles/s]
archive & make_nvp("i_code_on_L2",i_code_on_L2); //!< If 1, P code ON in L2; if 2, C/A code ON in L2;
archive & make_nvp("i_GPS_week",i_GPS_week); //!< GPS week number, aka WN [week]
archive & make_nvp("b_L2_P_data_flag",b_L2_P_data_flag); //!< When true, indicates that the NAV data stream was commanded OFF on the P-code of the L2 channel
archive & make_nvp("i_SV_accuracy",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)
archive & make_nvp("i_SV_health",i_SV_health);
archive & make_nvp("d_TGD",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]
archive & make_nvp("d_IODC",d_IODC); //!< Issue of Data, Clock
archive & make_nvp("i_AODO",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]
archive & make_nvp("b_fit_interval_flag",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.
archive & make_nvp("d_spare1",d_spare1);
archive & make_nvp("d_spare2",d_spare2);
archive & make_nvp("d_A_f0",d_A_f0); //!< Coefficient 0 of code phase offset model [s]
archive & make_nvp("d_A_f1",d_A_f1); //!< Coefficient 1 of code phase offset model [s/s]
archive & make_nvp("d_A_f2",d_A_f2); //!< Coefficient 2 of code phase offset model [s/s^2]
archive & make_nvp("b_integrity_status_flag",b_integrity_status_flag);
archive & make_nvp("b_alert_flag",b_alert_flag); //!< If true, indicates that the SV URA may be worse than indicated in d_SV_accuracy, use that SV at our own risk.
archive & make_nvp("b_antispoofing_flag",b_antispoofing_flag); //!< If true, the AntiSpoofing mode is ON in that SV
archive & make_nvp("i_satellite_PRN",i_satellite_PRN);
archive & make_nvp("M0_1", M0_1);
archive & make_nvp("e_1", e_1);
archive & make_nvp("A_1", A_1);
archive & make_nvp("OMEGA_0_2", OMEGA_0_2);
archive & make_nvp("i_0_2", i_0_2);
archive & make_nvp("omega_2", omega_2);
archive & make_nvp("OMEGA_dot_3", OMEGA_dot_3);
archive & make_nvp("iDot_2", iDot_2);
archive & make_nvp("C_uc_3", C_uc_3);
archive & make_nvp("C_us_3", C_us_3);
archive & make_nvp("C_rc_3", C_rc_3);
archive & make_nvp("C_rs_3", C_rs_3);
archive & make_nvp("C_ic_4", C_ic_4);
archive & make_nvp("C_is_4", C_is_4);
archive & make_nvp("t0e_1", t0e_1);
archive & make_nvp("t0c_4", t0c_4);
archive & make_nvp("af0_4", af0_4);
archive & make_nvp("af1_4", af1_4);
archive & make_nvp("af2_4", af2_4);
}
*/
};
#endif

4
src/core/system_parameters/galileo_navigation_message.h
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@ -51,17 +51,17 @@
/*!
* \brief This class handles the Galileo I/NAV Data message, as described in the
* Galileo Open Service Signal in Space Interface Control Document (OS SIS ICD), Issue 1.1 (Sept 2010).
* See http://ec.europa.eu/enterprise/policies/satnav/galileo/files/galileo-os-sis-icd-issue1-revision1_en.pdf
*/
class Galileo_Navigation_Message
{
private:
bool CRC_test(std::bitset<GALILEO_DATA_FRAME_BITS> bits,boost::uint32_t checksum);
bool CRC_test(std::bitset<GALILEO_DATA_FRAME_BITS> bits, boost::uint32_t checksum);
bool read_navigation_bool(std::bitset<GALILEO_DATA_JK_BITS> bits, const std::vector<std::pair<int,int> > parameter);
//void print_galileo_word_bytes(unsigned int GPS_word);
unsigned long int read_navigation_unsigned(std::bitset<GALILEO_DATA_JK_BITS> bits, const std::vector< std::pair<int,int> > parameter);
unsigned long int read_page_type_unsigned(std::bitset<GALILEO_PAGE_TYPE_BITS> bits, const std::vector< std::pair<int,int> > parameter);
signed long int read_navigation_signed(std::bitset<GALILEO_DATA_JK_BITS> bits, const std::vector<std::pair<int,int> > parameter);
int x,y;
public:
int Page_type_time_stamp;
int flag_even_word;

3
src/core/system_parameters/sbas_ephemeris.h
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@ -1,7 +1,6 @@
/*
/*!
* \file sbas_ephemeris.h
* \brief Interface of a SBAS REFERENCE LOCATION storage
*
* \author Daniel Fehr, 2013. daniel.co(at)bluewin.ch
*
* -------------------------------------------------------------------------