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https://github.com/gnss-sdr/gnss-sdr
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MOD: output print signals
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@ -74,7 +74,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data new_data)
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}
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// // Kalman state prediction (time update)
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cout << " KF RTKlib STATE" << kf_x;
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kf_x.print(" KF RTKlib STATE");
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new_data.kf_state=kf_x;
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//kf_x = kf_F * kf_x; // state prediction
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kf_P_x= kf_F * kf_P_x * kf_F.t() + kf_Q; // state error covariance prediction
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@ -120,7 +120,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data new_data)
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//rhoDot_pri(i)=(new_data.sat_v(i, 0)-0)*a_x(i)+(new_data.sat_v(i, 1)-0)*a_y(i)+(new_data.sat_v(i, 2)-0)*a_z(i);
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}
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cout << " V_LOS sat" << rhoDot_pri;
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rhoDot_pri.print("V_LOS sat");
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kf_H = arma::zeros(2*new_data.sat_number,8);
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@ -145,8 +145,8 @@ bool Vtl_Engine::vtl_loop(Vtl_Data new_data)
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//rhoDot_pri(i)=(rhoDot_pri(i))/Lambda_GPS_L1;
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}
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//cout << " KF measurement vector difference" << kf_yerr;
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cout << " kf_yerr" << kf_yerr;
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//rhoDot_pri.print("DOPPLER stimated [Hz]");
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kf_yerr.print("KF measurement vector difference");
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for (int32_t i = 0; i < new_data.sat_number; i++) // Measurement error Covariance Matrix R assembling
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{
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