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https://github.com/gnss-sdr/gnss-sdr
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ADD: 3DoF model linearization in F matrix
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@ -124,7 +124,6 @@ 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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//**************************************
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kf_F_fill(kf_F, kf_dt);
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if (counter < closure_point)
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{
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@ -161,7 +160,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data new_data)
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// kf_x(7) = (kf_x(7)-kf_dx(7))/kf_dt;
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// kf_x(8) = (kf_x(8)-kf_dx(8))/kf_dt;
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}
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kf_F_fill(kf_F, kf_dt, kf_x);
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obsv_calc(rho_pri, rhoDot_pri, rhoDot2_pri, a_x, a_y, a_z, new_data.sat_number, new_data.sat_p, new_data.sat_v, kf_x);
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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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@ -299,8 +298,20 @@ void Vtl_Engine::kf_H_fill(arma::mat &kf_H, int sat_number, arma::colvec ax, arm
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}
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}
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void Vtl_Engine::kf_F_fill(arma::mat &kf_F, double kf_dt)
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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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double densidad = 1.0;
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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 mass_rocket = 50.0; // 50Kg
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double beta = (GNSS_PI * densidad * diam_cohete * diam_cohete / 8) * ballistic_coef;
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// modulo de la velocidad
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double vx = kf_x(3);
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double vy = kf_x(4);
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double vz = kf_x(5);
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double u = norm(kf_x.rows(3, 5), 2);
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kf_F(0, 3) = kf_dt;
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kf_F(0, 6) = kf_dt * kf_dt / 2;
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kf_F(1, 4) = kf_dt;
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@ -312,6 +323,10 @@ void Vtl_Engine::kf_F_fill(arma::mat &kf_F, double 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(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(8, 5) = -beta*(vz*vz/u+u);
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kf_F(9, 10) = kf_dt;
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}
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@ -104,7 +104,7 @@ private:
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double delta_t_cmd = 0;
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void kf_H_fill(arma::mat &kf_H, int sat_number, arma::colvec ax, arma::colvec ay, arma::colvec az, double kf_dt); // Observation Matrix constructor
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void kf_F_fill(arma::mat &kf_F, double kf_dt); // System Matrix constructor
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void kf_F_fill(arma::mat &kf_F, double kf_dt, arma::mat &kf_x); // System Matrix constructor
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void 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); // Observables calculation
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void kf_measurements(arma::mat &kf_yerr, int sat_number, arma::mat rho_pri, arma::mat rhoDot_pri, arma::mat rhoDot2_pri, arma::colvec pr_m, arma::colvec doppler_hz, arma::mat kf_x);
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void model3DoF(double &acc_x, double &acc_y, double &acc_z, arma::mat kf_x, double dt, int counter);
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