1 | #ifndef EPHEMERIS_H
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2 | #define EPHEMERIS_H
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3 |
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4 | #include <newmat.h>
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5 | #include <QtCore>
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6 | #include <stdio.h>
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7 | #include <string>
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8 | #include "bnctime.h"
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9 | #include "bncconst.h"
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10 | #include "t_prn.h"
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11 |
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12 | extern "C" {
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13 | # include "rtcm3torinex.h"
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14 | }
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15 |
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16 | class t_orbCorr;
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17 | class t_clkCorr;
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18 |
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19 | class t_eph {
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20 | public:
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21 | enum e_type {unknown, GPS, QZSS, GLONASS, Galileo, SBAS, Compass};
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22 | enum e_checkState {unchecked, ok, bad};
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23 |
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24 | t_eph();
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25 | virtual ~t_eph() {};
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26 |
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27 | virtual e_type type() const = 0;
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28 | virtual QString toString(double version) const = 0;
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29 | virtual int IOD() const = 0;
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30 | virtual int slotNum() const {return 0;}
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31 | bncTime TOC() const {return _TOC;}
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32 | bool isNewerThan(const t_eph* eph) const {return earlierTime(eph, this);}
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33 | e_checkState checkState() const {return _checkState;}
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34 | void setCheckState(e_checkState checkState) {_checkState = checkState;}
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35 | t_prn prn() const {return _prn;}
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36 | t_irc getCrd(const bncTime& tt, ColumnVector& xc, ColumnVector& vv, bool useCorr) const;
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37 | void setOrbCorr(const t_orbCorr* orbCorr);
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38 | void setClkCorr(const t_clkCorr* clkCorr);
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39 | const QDateTime& receptDateTime() const {return _receptDateTime;}
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40 | static QString rinexDateStr(const bncTime& tt, const t_prn& prn, double version);
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41 | static QString rinexDateStr(const bncTime& tt, const QString& prnStr, double version);
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42 | static bool earlierTime(const t_eph* eph1, const t_eph* eph2) {return eph1->_TOC < eph2->_TOC;}
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43 |
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44 | protected:
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45 | virtual t_irc position(int GPSweek, double GPSweeks, double* xc, double* vv) const = 0;
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46 | t_prn _prn;
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47 | bncTime _TOC;
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48 | QDateTime _receptDateTime;
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49 | e_checkState _checkState;
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50 | t_orbCorr* _orbCorr;
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51 | t_clkCorr* _clkCorr;
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52 | };
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53 |
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54 |
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55 | class t_ephGPS : public t_eph {
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56 | friend class t_ephEncoder;
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57 | public:
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58 | t_ephGPS() { }
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59 | t_ephGPS(float rnxVersion, const QStringList& lines);
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60 | virtual ~t_ephGPS() {}
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61 |
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62 | virtual e_type type() const {return (_prn.system() == 'J' ? t_eph::QZSS : t_eph::GPS); }
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63 | virtual QString toString(double version) const;
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64 | virtual int IOD() const { return static_cast<int>(_IODC); }
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65 | void set(const gpsephemeris* ee);
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66 | double TGD() const {return _TGD;} // Timing Group Delay (P1-P2 DCB)
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67 |
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68 | private:
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69 | virtual t_irc position(int GPSweek, double GPSweeks, double* xc, double* vv) const;
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70 |
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71 | double _clock_bias; // [s]
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72 | double _clock_drift; // [s/s]
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73 | double _clock_driftrate; // [s/s^2]
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74 |
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75 | double _IODE;
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76 | double _Crs; // [m]
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77 | double _Delta_n; // [rad/s]
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78 | double _M0; // [rad]
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79 |
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80 | double _Cuc; // [rad]
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81 | double _e; //
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82 | double _Cus; // [rad]
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83 | double _sqrt_A; // [m^0.5]
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84 |
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85 | double _TOEsec; // [s]
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86 | double _Cic; // [rad]
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87 | double _OMEGA0; // [rad]
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88 | double _Cis; // [rad]
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89 |
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90 | double _i0; // [rad]
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91 | double _Crc; // [m]
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92 | double _omega; // [rad]
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93 | double _OMEGADOT; // [rad/s]
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94 |
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95 | double _IDOT; // [rad/s]
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96 | double _L2Codes; // Codes on L2 channel
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97 | double _TOEweek;
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98 | double _L2PFlag; // L2 P data flag
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99 |
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100 | mutable double _ura; // SV accuracy
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101 | double _health; // SV health
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102 | double _TGD; // [s]
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103 | double _IODC;
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104 |
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105 | double _TOT; // Transmisstion time
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106 | double _fitInterval; // Fit interval
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107 | };
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108 |
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109 | class t_ephGlo : public t_eph {
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110 | friend class t_ephEncoder;
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111 | public:
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112 | t_ephGlo() { _xv.ReSize(6); }
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113 | t_ephGlo(float rnxVersion, const QStringList& lines);
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114 | virtual ~t_ephGlo() {}
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115 |
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116 | virtual e_type type() const {return t_eph::GLONASS;}
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117 | virtual QString toString(double version) const;
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118 | virtual int IOD() const;
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119 | virtual int slotNum() const {return int(_frequency_number);}
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120 | void set(const glonassephemeris* ee);
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121 |
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122 | private:
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123 | virtual t_irc position(int GPSweek, double GPSweeks, double* xc, double* vv) const;
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124 | static ColumnVector glo_deriv(double /* tt */, const ColumnVector& xv, double* acc);
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125 |
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126 | mutable bncTime _tt; // time
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127 | mutable ColumnVector _xv; // status vector (position, velocity) at time _tt
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128 |
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129 | double _gps_utc;
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130 | double _tau; // [s]
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131 | double _gamma; //
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132 | mutable double _tki; // message frame time
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133 |
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134 | double _x_pos; // [km]
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135 | double _x_velocity; // [km/s]
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136 | double _x_acceleration; // [km/s^2]
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137 | double _health; // 0 = O.K.
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138 |
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139 | double _y_pos; // [km]
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140 | double _y_velocity; // [km/s]
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141 | double _y_acceleration; // [km/s^2]
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142 | double _frequency_number; // ICD-GLONASS data position
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143 |
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144 | double _z_pos; // [km]
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145 | double _z_velocity; // [km/s]
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146 | double _z_acceleration; // [km/s^2]
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147 | double _E; // Age of Information [days]
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148 | };
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149 |
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150 | class t_ephGal : public t_eph {
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151 | friend class t_ephEncoder;
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152 | public:
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153 | t_ephGal() { }
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154 | t_ephGal(float rnxVersion, const QStringList& lines);
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155 | virtual ~t_ephGal() {}
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156 |
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157 | virtual QString toString(double version) const;
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158 | virtual e_type type() const {return t_eph::Galileo;}
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159 | virtual int IOD() const { return static_cast<int>(_IODnav); }
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160 | void set(const galileoephemeris* ee);
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161 |
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162 | private:
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163 | virtual t_irc position(int GPSweek, double GPSweeks, double* xc, double* vv) const;
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164 |
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165 | double _clock_bias; // [s]
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166 | double _clock_drift; // [s/s]
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167 | double _clock_driftrate; // [s/s^2]
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168 |
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169 | double _IODnav;
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170 | double _Crs; // [m]
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171 | double _Delta_n; // [rad/s]
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172 | double _M0; // [rad]
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173 |
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174 | double _Cuc; // [rad]
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175 | double _e; //
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176 | double _Cus; // [rad]
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177 | double _sqrt_A; // [m^0.5]
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178 |
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179 | double _TOEsec; // [s]
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180 | double _Cic; // [rad]
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181 | double _OMEGA0; // [rad]
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182 | double _Cis; // [rad]
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183 |
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184 | double _i0; // [rad]
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185 | double _Crc; // [m]
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186 | double _omega; // [rad]
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187 | double _OMEGADOT; // [rad/s]
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188 |
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189 | double _IDOT; // [rad/s]
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190 | //
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191 | double _TOEweek;
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192 | // spare
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193 |
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194 | double _SISA; // Signal In Space Accuracy
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195 | double _E5aHS; // E5a Health Status
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196 | double _E5bHS; // E5a Health Status
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197 | double _BGD_1_5A; // group delay [s]
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198 | double _BGD_1_5B; // group delay [s]
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199 |
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200 | double _TOT; // [s]
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201 |
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202 | int _flags;
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203 | };
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204 |
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205 | class t_ephSBAS : public t_eph {
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206 | friend class t_ephEncoder;
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207 | public:
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208 | t_ephSBAS() {}
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209 | t_ephSBAS(float rnxVersion, const QStringList& lines);
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210 | virtual ~t_ephSBAS() {}
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211 |
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212 | void set(const sbasephemeris* ee);
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213 | virtual e_type type() const {return t_eph::SBAS;}
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214 | virtual int IOD() const {return _IODN;}
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215 | virtual QString toString(double version) const;
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216 |
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217 | private:
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218 | virtual t_irc position(int GPSweek, double GPSweeks, double* xc, double* vv) const;
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219 |
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220 | int _IODN;
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221 | double _TOW; // not used (set to 0.9999e9)
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222 | double _agf0; // [s] clock correction
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223 | double _agf1; // [s/s] clock correction drift
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224 |
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225 | double _x_pos; // [m]
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226 | double _x_velocity; // [m/s]
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227 | double _x_acceleration; // [m/s^2]
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228 |
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229 | double _y_pos; // [m]
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230 | double _y_velocity; // [m/s]
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231 | double _y_acceleration; // [m/s^2]
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232 |
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233 | double _z_pos; // [m]
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234 | double _z_velocity; // [m/s]
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235 | double _z_acceleration; // [m/s^2]
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236 |
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237 | double _ura;
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238 | double _health;
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239 | };
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240 |
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241 | class t_ephCompass : public t_eph {
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242 | friend class t_ephEncoder;
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243 | public:
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244 | t_ephCompass() {}
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245 | t_ephCompass(float rnxVersion, const QStringList& lines);
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246 | virtual ~t_ephCompass() {}
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247 |
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248 | // void set(const compassephemeris* ee);
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249 | virtual e_type type() const {return t_eph::Compass;}
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250 | virtual int IOD() const {return _AODC;}
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251 | virtual QString toString(double version) const;
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252 |
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253 | private:
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254 | virtual t_irc position(int GPSweek, double GPSweeks, double* xc, double* vv) const;
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255 |
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256 | bncTime _TOT;
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257 | bncTime _TOE;
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258 | bncTime _TOC_bdt;
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259 | bncTime _TOE_bdt;
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260 | int _AODE;
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261 | int _AODC;
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262 | double _clock_bias; // [s]
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263 | double _clock_drift; // [s/s]
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264 | double _clock_driftrate; // [s/s^2]
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265 | double _Crs; // [m]
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266 | double _Delta_n; // [rad/s]
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267 | double _M0; // [rad]
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268 | double _Cuc; // [rad]
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269 | double _e; //
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270 | double _Cus; // [rad]
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271 | double _sqrt_A; // [m^0.5]
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272 | double _Cic; // [rad]
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273 | double _OMEGA0; // [rad]
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274 | double _Cis; // [rad]
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275 | double _i0; // [rad]
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276 | double _Crc; // [m]
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277 | double _omega; // [rad]
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278 | double _OMEGADOT; // [rad/s]
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279 | double _IDOT; // [rad/s]
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280 | double _TGD1; // [s]
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281 | double _TGD2; // [s]
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282 | int _SatH1; //
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283 | };
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284 |
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285 | #endif
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