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https://github.com/gnss-sdr/gnss-sdr
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FORMAT: clang
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@@ -124,7 +124,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data new_data)
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//**************************************
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//**************************************
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// Kalman state prediction (time update)
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// Kalman state prediction (time update)
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//**************************************
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//**************************************
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if (counter < closure_point)
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if (counter < closure_point)
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{
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{
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// receiver solution from rtklib_solver
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// receiver solution from rtklib_solver
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@@ -300,7 +300,6 @@ void Vtl_Engine::kf_H_fill(arma::mat &kf_H, int sat_number, arma::colvec ax, arm
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void Vtl_Engine::kf_F_fill(arma::mat &kf_F, double kf_dt, arma::mat &kf_x)
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void Vtl_Engine::kf_F_fill(arma::mat &kf_F, double kf_dt, arma::mat &kf_x)
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{
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{
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double densidad = 1.0;
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double densidad = 1.0;
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double ballistic_coef = 0.007;
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double ballistic_coef = 0.007;
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double diam_cohete = 120.0e-3; // 120 mm
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double diam_cohete = 120.0e-3; // 120 mm
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@@ -323,14 +322,14 @@ void Vtl_Engine::kf_F_fill(arma::mat &kf_F, double kf_dt, arma::mat &kf_x)
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kf_F(4, 7) = kf_dt;
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kf_F(4, 7) = kf_dt;
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kf_F(5, 8) = kf_dt;
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kf_F(5, 8) = kf_dt;
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kf_F(6, 3) = -beta*(vx*vx/u+u);
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kf_F(6, 3) = -beta * (vx * vx / u + u);
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kf_F(7, 4) = -beta*(vy*vy/u+u);
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kf_F(7, 4) = -beta * (vy * vy / u + u);
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kf_F(8, 5) = -beta*(vz*vz/u+u);
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kf_F(8, 5) = -beta * (vz * vz / u + u);
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kf_F(9, 10) = kf_dt;
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kf_F(9, 10) = kf_dt;
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}
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}
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void Vtl_Engine::obsv_calc(arma::mat &rho_pri, arma::mat &rhoDot_pri, arma::mat &rhoDot2_pri,arma::colvec &ax, arma::colvec &ay, arma::colvec &az, int sat_number, arma::mat sat_p, arma::mat sat_v, arma::mat kf_x)
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void Vtl_Engine::obsv_calc(arma::mat &rho_pri, arma::mat &rhoDot_pri, arma::mat &rhoDot2_pri, arma::colvec &ax, arma::colvec &ay, arma::colvec &az, int sat_number, arma::mat sat_p, arma::mat sat_v, arma::mat kf_x)
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{
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{
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for (int32_t i = 0; i < sat_number; i++) // neccesary quantities
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for (int32_t i = 0; i < sat_number; i++) // neccesary quantities
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{
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{
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@@ -390,7 +389,7 @@ void Vtl_Engine::model3DoF(double &acc_x, double &acc_y, double &acc_z, arma::ma
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if (t_disparo < .2)
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if (t_disparo < .2)
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{
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{
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u_dir = {.90828, -.13984, -.388756}; // launching attitude
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u_dir = {.90828, -.13984, -.388756}; // launching attitude
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}
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}
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else
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else
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{
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{
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@@ -454,11 +453,11 @@ void Vtl_Engine::accelerometer(double &acc_x, double &acc_y, double &acc_z, arma
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if (t_disparo < .2)
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if (t_disparo < .2)
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{
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{
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u_dir = {.90828, -.13984, -.388756}; // launching attitude
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u_dir = {.90828, -.13984, -.388756}; // launching attitude
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}
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}
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else
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else
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{
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{
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u_dir = u_vec / u;
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u_dir = u_vec / u;
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}
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}
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accelerometer = AccLkTable(t_disparo);
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accelerometer = AccLkTable(t_disparo);
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