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MOD: MATLAB file doppler correction with time derivative of clk_drift
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@ -199,7 +199,13 @@ for t=2:length(navSolution.RX_time)
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pr_m_filt(chan,t)=sat_prg_m(chan,t)+kf_yerr_g(chan,t);% now filtered
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rhoDot_pri_filt(chan,t)=(sat_dopp_hz(chan,t)*Lambda_GPS_L1+corr_kf_state(8,t))-kf_yerr_g(chan+sat_number,t);
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%convert rhoDot_pri to doppler shift!
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sat_dopp_hz_filt(chan,t)=(rhoDot_pri_filt(chan,t)-corr_kf_state(8,t))/Lambda_GPS_L1;
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d_dt_clk_drift=(corr_kf_state(8,t)-corr_kf_state(8,t-1));
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if (t<length(navSolution.RX_time)-point_of_closure)
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sat_dopp_hz_filt(chan,t)=(rhoDot_pri_filt(chan,t)-corr_kf_state(8,t))/Lambda_GPS_L1;
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else
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sat_dopp_hz_filt(chan,t)=(rhoDot_pri_filt(chan,t)-corr_kf_state(8,t)-d_dt_clk_drift)/Lambda_GPS_L1;
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end
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% carrier_phase_rads = 0;
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carrier_freq_hz =GPS_L1_freq_hz+sat_dopp_hz_filt(chan,t);
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@ -24,7 +24,7 @@ clearvars
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SPEED_OF_LIGHT_M_S=299792458.0;
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Lambda_GPS_L1=0.1902937;
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GPS_L1_freq_hz=1575.42e6;
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point_of_closure=3400;
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point_of_closure=4060;
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%% ==================== VARIANCES =============================
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pos_var=100;%m^2
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