mirrors/gnss-sdr
1
0
Fork 0
mirror of https://github.com/gnss-sdr/gnss-sdr synced 2024-11-15 22:34:58 +00:00
Code Issues Releases Wiki Activity

MOD: filtro aceleracion vtl

Browse Source
This commit is contained in:
M.A. Gomez 2023-02-15 19:44:21 +01:00
parent 2115bc0aab
commit 08c68d4af9
2 changed files with 36 additions and 14 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

39
src/algorithms/PVT/libs/vtl_engine.cc
View File

@ -42,6 +42,9 @@ bool Vtl_Engine::vtl_loop(Vtl_Data& new_data)
static arma::mat kf_P_x = arma::eye(n_of_states, n_of_states) * 1.0; //TODO: use a real value.;
static arma::mat kf_x = arma::zeros(n_of_states, 1);
static arma::mat kf_dx = arma::zeros(n_of_states, 1);
//TODO: resolver el problema cuando cambie el numero de sat!!
// static arma::colvec rhoDot_pri_old = arma::zeros(new_data.sat_number, 1);
// covariances (static)
kf_R = arma::zeros(3 * new_data.sat_number, 3 * new_data.sat_number);
@ -117,7 +120,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data& new_data)
// It is diagonal 2*NSatellite x 2*NSatellite (NSat psudorange error;NSat pseudo range rate error)
kf_R(i, i) = 80.0;//*50.0/new_data.sat_CN0_dB_hz(i); //TODO: fill with real values.
kf_R(i + new_data.sat_number, i + new_data.sat_number) = 20.0;//*50.0/new_data.sat_CN0_dB_hz(i);
kf_R(i + 2*new_data.sat_number, i + 2*new_data.sat_number) = 100.0;//*50.0/new_data.sat_CN0_dB_hz(i);
kf_R(i + 2*new_data.sat_number, i + 2*new_data.sat_number) = 400.0;//*50.0/new_data.sat_CN0_dB_hz(i);
if(80.0*50.0/new_data.sat_CN0_dB_hz(i)>90||20.0*50.0/new_data.sat_CN0_dB_hz(i)>25){
kf_R(i, i) = 10e4;
@ -137,6 +140,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data& new_data)
d = arma::zeros(new_data.sat_number, 1);
rho_pri = arma::zeros(new_data.sat_number, 1);
rhoDot_pri = arma::zeros(new_data.sat_number, 1);
rhoDot2_pri = arma::zeros(new_data.sat_number, 1);
rho_pri_filt = arma::zeros(new_data.sat_number, 1);
rhoDot_pri_filt = arma::zeros(new_data.sat_number, 1);
@ -154,10 +158,15 @@ bool Vtl_Engine::vtl_loop(Vtl_Data& new_data)
new_data.sat_LOS(i, 2) = a_z(i);
}
kf_H = arma::zeros(2 * new_data.sat_number, n_of_states);
kf_H = arma::zeros(3 * new_data.sat_number, n_of_states);
test = kf_H_fill(kf_H,new_data.sat_number,a_x, a_y, a_z, kf_dt);
for (int32_t i = 0; i < new_data.sat_number; i++) //neccesary quantities
{
// rhoDot2_pri(i)=(rhoDot_pri(i)-rhoDot_pri_old(i))/kf_dt;
}
// Kalman estimation (measurement update)
test = kf_measurements(kf_yerr, new_data.sat_number, rho_pri, rhoDot_pri, new_data.pr_m, new_data.doppler_hz, kf_x);
test = kf_measurements(kf_yerr, new_data.sat_number, rho_pri, rhoDot_pri, rhoDot_pri, new_data.pr_m, new_data.doppler_hz, kf_x);
kf_P_x = kf_F * kf_P_x * kf_F.t() + kf_Q; // state error covariance prediction
// Kalman filter update step
@ -174,6 +183,14 @@ bool Vtl_Engine::vtl_loop(Vtl_Data& new_data)
// // ################## Geometric Transformation ######################################
test = obsv_calc(rho_pri,rhoDot_pri,a_x, a_y, a_z,new_data.sat_number,new_data.sat_p,new_data.sat_v,kf_x);
for (int32_t i = 0; i < new_data.sat_number; i++) //neccesary quantities
{
//acc_effect(i)=(a_x(i)*kf_state(7,t)+a_y(chan,t)*kf_state(8,t)+a_z(chan,t)*kf_state(9,t));
//rhoDot2_pri(chan,t)=(rhoDot_pri(chan,t)-rhoDot_pri(chan,t-1))/kf_dt;
//rhoDot2_pri(chan,t)=-acc_effect(chan,t);
}
test = kf_H_fill(kf_H,new_data.sat_number,a_x, a_y, a_z, kf_dt);
// Re-calculate error measurement vector with the most recent data available: kf_delta_y=kf_H*kf_delta_x
kf_yerr = kf_H * kf_xerr;
@ -191,7 +208,7 @@ bool Vtl_Engine::vtl_loop(Vtl_Data& new_data)
// sample code
trk_cmd.carrier_phase_rads = 0; // difficult of calculation
trk_cmd.carrier_freq_hz = doppler_hz_filt(channel); //+ kf_x(7)/Lambda_GPS_L1; // this is el doppler WITHOUTH sintony correction
trk_cmd.carrier_freq_rate_hz_s =-(a_x(channel)*kf_x(6)+a_y(channel)*kf_x(7)+a_z(channel)*kf_x(8))/ Lambda_GPS_L1;
trk_cmd.carrier_freq_rate_hz_s = 0;//-(a_x(channel)*kf_x(6)+a_y(channel)*kf_x(7)+a_z(channel)*kf_x(8))/ Lambda_GPS_L1;
trk_cmd.code_phase_chips = kf_yerr(channel)/SPEED_OF_LIGHT_M_S*1023e3;
trk_cmd.enable_carrier_nco_cmd = true;
trk_cmd.enable_code_nco_cmd = true;
@ -278,6 +295,13 @@ bool Vtl_Engine::kf_H_fill(arma::mat &kf_H,int sat_number, arma::colvec ax, arma
kf_H(i + sat_number, 8) = az(i)*kf_dt;
kf_H(i + sat_number, 10) = 1.0;
kf_H(i + 2*sat_number, 3) = 0;//ax(i);
kf_H(i + 2*sat_number, 4) = 0;//ay(i);
kf_H(i + 2*sat_number, 5) = 0;//az(i);
kf_H(i + 2*sat_number, 6) = ax(i);
kf_H(i + 2*sat_number, 7) = ay(i);
kf_H(i + 2*sat_number, 8) = az(i);
kf_H(i + 2*sat_number, 10) = kf_dt;
}
return -1;
@ -321,12 +345,13 @@ bool Vtl_Engine::obsv_calc(arma::mat &rho_pri,arma::mat &rhoDot_pri,arma::colvec
return -1;
}
bool Vtl_Engine::kf_measurements(arma::mat &kf_yerr, int sat_number, arma::mat rho_pri, arma::mat rhoDot_pri, arma::colvec pr_m, arma::colvec doppler_hz, arma::mat kf_x)
bool Vtl_Engine::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)
{
for (int32_t i = 0; i < sat_number; i++) // Measurement vector
{
kf_yerr(i) = rho_pri(i) - pr_m(i);
kf_yerr(i + sat_number) = (doppler_hz(i) * Lambda_GPS_L1+kf_x(10)) - rhoDot_pri(i);
kf_yerr(i + 2*sat_number) = -rhoDot2_pri(i);
}
return -1;
}
@ -348,10 +373,6 @@ bool Vtl_Engine::model3DoF(double &acc_x,double &acc_y,double &acc_z,arma::mat k
//modulo de la velocidad
double u = norm(u_vec, 2);
// if(t<1000){
// t_disparo=0;
// }
if(u>4){
t_disparo=t_disparo+dt;
double diam_cohete=120.0e-3;// 120 mm

3
src/algorithms/PVT/libs/vtl_engine.h
View File

@ -56,6 +56,7 @@ private:
arma::colvec d;
arma::colvec rho_pri;
arma::colvec rhoDot_pri;
arma::colvec rhoDot2_pri;
arma::colvec rho_pri_filt;
arma::colvec rhoDot_pri_filt;
arma::colvec doppler_hz_filt;
@ -87,7 +88,7 @@ private:
bool 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
bool kf_F_fill(arma::mat &kf_F,double kf_dt); // System Matrix constructor
bool obsv_calc(arma::mat &rho_pri,arma::mat &rhoDot_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
bool kf_measurements(arma::mat &kf_yerr, int sat_number, arma::mat rho_pri, arma::mat rhoDot_pri, arma::colvec pr_m, arma::colvec doppler_hz, arma::mat kf_x);
bool 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);
bool model3DoF(double &acc_x,double &acc_y,double &acc_z,arma::mat kf_x,double dt);
double EmpujeLkTable(double t_disparo);
};