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mirror of https://github.com/gnss-sdr/gnss-sdr synced 2025-09-11 23:36:03 +00:00

FORMAT: clang

This commit is contained in:
M.A. Gomez
2023-06-18 23:47:24 +02:00
parent 352ded5036
commit 3f33a0fdd4

View File

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