mirror of
https://github.com/gnss-sdr/gnss-sdr
synced 2024-11-15 06:14:58 +00:00
[MOD] debug over state added
This commit is contained in:
parent
229c9115e4
commit
6fad047070
@ -42,6 +42,7 @@ void Vtl_Data::init_storage(int n_sats)
|
||||
rx_dts = arma::mat(1, 2);
|
||||
rx_var = arma::vec(1);
|
||||
rx_pvt_var = arma::vec(8);
|
||||
kf_state = arma::vec(8);
|
||||
epoch_tow_s = 0;
|
||||
sample_counter = 0;
|
||||
}
|
||||
@ -54,8 +55,9 @@ void Vtl_Data::debug_print()
|
||||
// sat_dts.print("VTL Sat clocks");
|
||||
// sat_var.print("VTL Sat clock variances");
|
||||
sat_health_flag.print("VTL Sat health");
|
||||
// kf_state.print("EKF STATE");
|
||||
|
||||
// pr_m.print("Satellite Code pseudoranges [m]");
|
||||
pr_m.print("Satellite Code pseudoranges [m]");
|
||||
// doppler_hz.print("satellite Carrier Dopplers [Hz]");
|
||||
// carrier_phase_rads.print("satellite accumulated carrier phases [rads]");
|
||||
}
|
||||
|
@ -50,6 +50,7 @@ public:
|
||||
arma::mat rx_pvt_var; // Receiver position, velocity and time VARIANCE [m/s]
|
||||
arma::mat rx_dts; // Receiver clock bias and drift [s,s/s]
|
||||
arma::colvec rx_var; // Receiver position and clock error variance [m^2]
|
||||
arma::colvec kf_state; // KF STATE
|
||||
// time handling
|
||||
double epoch_tow_s; // current observation RX time [s]
|
||||
uint64_t sample_counter; // current sample counter associated with RX time [samples from start]
|
||||
|
@ -15,6 +15,9 @@
|
||||
*/
|
||||
|
||||
#include "vtl_engine.h"
|
||||
#include "iostream"
|
||||
|
||||
using namespace std;
|
||||
|
||||
Vtl_Engine::Vtl_Engine()
|
||||
{
|
||||
@ -30,7 +33,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data new_data)
|
||||
using arma::as_scalar;
|
||||
// ################## Kalman filter initialization ######################################
|
||||
// covariances (static)
|
||||
kf_P_x = arma::zeros(8, 8); //TODO: use a real value.
|
||||
kf_P_x = arma::eye(8, 8); //TODO: use a real value.
|
||||
kf_x = arma::zeros(8, 1);
|
||||
kf_R = arma::zeros(2*new_data.sat_number, 2*new_data.sat_number);
|
||||
double kf_dt=1e-1;
|
||||
@ -69,8 +72,11 @@ bool Vtl_Engine::vtl_loop(Vtl_Data new_data)
|
||||
}
|
||||
|
||||
// // Kalman state prediction (time update)
|
||||
cout << " KF RTKlib STATE" << kf_x;
|
||||
kf_x = kf_F * kf_x; // state prediction
|
||||
kf_P_x= kf_F * kf_P_x * kf_F.t() + kf_Q; // state error covariance prediction
|
||||
new_data.kf_state=kf_x;
|
||||
cout << " KF priori STATE" << kf_x;
|
||||
//from error state variables to variables
|
||||
//x_u=x_u0+kf_x_pri(0);
|
||||
//y_u=y_u0+kf_x_pri(1);
|
||||
@ -148,7 +154,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data new_data)
|
||||
//kf_delta_x = kf_K * kf_delta_y; // updated error state estimation
|
||||
kf_x = kf_x + kf_K * (kf_y-kf_H*kf_x); // updated state estimation
|
||||
kf_P_x = (arma::eye(size(kf_P_x)) - kf_K * kf_H) * kf_P_x; // update state estimation error covariance matrix
|
||||
|
||||
cout << " KF posteriori STATE" << kf_x;
|
||||
// // // kf_x = kf_x_pri+kf_delta_x; // compute PVT from priori and error estimation (neccesary?)
|
||||
|
||||
|
||||
|
Loading…
Reference in New Issue
Block a user