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https://github.com/gnss-sdr/gnss-sdr
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Fix documentation and typos
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@ -63,7 +63,7 @@ double Gnss_Almanac::predicted_doppler(double rx_time_s,
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// Position in EFEF
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const std::vector<double> pos_rx = {(v + h) * cosp * cosl, (v + h) * cosp * sinl, (v * (1.0 - e2) + h) * sinp};
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// Velovity in EFEF
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// Velocity in EFEF
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const double t = cosp * vu - sinp * vn;
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const std::vector<double> vel_rx = {cosl * t - sinl * ve, sinl * t + cosl * ve, sinp * vu + cosp * vn};
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@ -38,7 +38,8 @@ public:
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*/
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Gnss_Almanac() = default;
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/* \brief Computes prediction of the Doppler shift for a given time and receiver's position and velocity.
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/*!
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* \brief Computes prediction of the Doppler shift for a given time and receiver's position and velocity.
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* \f[
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* f_{d} = - \mathbf{v} \frac{\mathbf{x}^{T}}{\left| \mathbf{x} \right| } \frac{f_{L}}{c}
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* \f]
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@ -72,6 +73,9 @@ public:
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double vu,
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int band) const;
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/*!
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* \brief Computes satellite Position and Velocity, in ECEF, for a given time (expressed in seconds of week)
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*/
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void satellitePosVelComputation(double transmitTime, std::array<double, 7>& pos_vel_dtr) const;
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uint32_t PRN{}; //!< SV PRN NUMBER
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@ -59,7 +59,7 @@ double Gnss_Ephemeris::predicted_doppler(double rx_time_s,
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// Position in EFEF
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const std::vector<double> pos_rx = {(v + h) * cosp * cosl, (v + h) * cosp * sinl, (v * (1.0 - e2) + h) * sinp};
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// Velovity in EFEF
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// Velocity in EFEF
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const double t = cosp * vu - sinp * vn;
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const std::vector<double> vel_rx = {cosl * t - sinl * ve, sinl * t + cosl * ve, sinp * vu + cosp * vn};
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