Files
PX4-Autopilot/src/modules/local_position_estimator/sensors/gps.cpp
T

197 lines
5.0 KiB
C++

#include "../BlockLocalPositionEstimator.hpp"
#include <systemlib/mavlink_log.h>
#include <matrix/math.hpp>
extern orb_advert_t mavlink_log_pub;
// required number of samples for sensor
// to initialize
static const uint32_t REQ_GPS_INIT_COUNT = 10;
static const uint32_t GPS_TIMEOUT = 1000000; // 1.0 s
void BlockLocalPositionEstimator::gpsInit()
{
// measure
Vector<double, n_y_gps> y;
if (gpsMeasure(y) != OK) {
_gpsStats.reset();
return;
}
// if finished
if (_gpsStats.getCount() > REQ_GPS_INIT_COUNT) {
double gpsLatHome = _gpsStats.getMean()(0);
double gpsLonHome = _gpsStats.getMean()(1);
if (!_receivedGps) {
_receivedGps = true;
map_projection_init(&_map_ref, gpsLatHome, gpsLonHome);
}
_gpsAltHome = _gpsStats.getMean()(2);
mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] gps init "
"lat %6.2f lon %6.2f alt %5.1f m",
gpsLatHome,
gpsLonHome,
double(_gpsAltHome));
_gpsInitialized = true;
_gpsFault = FAULT_NONE;
_gpsStats.reset();
if (!_altHomeInitialized) {
_altHomeInitialized = true;
_altHome = _gpsAltHome;
}
}
}
int BlockLocalPositionEstimator::gpsMeasure(Vector<double, n_y_gps> &y)
{
// check for good gps signal
uint8_t nSat = _sub_gps.get().satellites_used;
float eph = _sub_gps.get().eph;
if (nSat < 6 || eph > _gps_eph_max.get()) {
return -1;
}
// gps measurement
y.setZero();
y(0) = _sub_gps.get().lat * 1e-7;
y(1) = _sub_gps.get().lon * 1e-7;
y(2) = _sub_gps.get().alt * 1e-3;
y(3) = _sub_gps.get().vel_n_m_s;
y(4) = _sub_gps.get().vel_e_m_s;
y(5) = _sub_gps.get().vel_d_m_s;
// increament sums for mean
_gpsStats.update(y);
_time_last_gps = _timeStamp;
return OK;
}
void BlockLocalPositionEstimator::gpsCorrect()
{
// measure
Vector<double, n_y_gps> y_global;
if (gpsMeasure(y_global) != OK) { return; }
// gps measurement in local frame
double lat = y_global(0);
double lon = y_global(1);
float alt = y_global(2);
float px = 0;
float py = 0;
float pz = -(alt - _gpsAltHome);
map_projection_project(&_map_ref, lat, lon, &px, &py);
Vector<float, 6> y;
y.setZero();
y(0) = px;
y(1) = py;
y(2) = pz;
y(3) = y_global(3);
y(4) = y_global(4);
y(5) = y_global(5);
// gps measurement matrix, measures position and velocity
Matrix<float, n_y_gps, n_x> C;
C.setZero();
C(Y_gps_x, X_x) = 1;
C(Y_gps_y, X_y) = 1;
C(Y_gps_z, X_z) = 1;
C(Y_gps_vx, X_vx) = 1;
C(Y_gps_vy, X_vy) = 1;
C(Y_gps_vz, X_vz) = 1;
// gps covariance matrix
Matrix<float, n_y_gps, n_y_gps> R;
R.setZero();
// default to parameter, use gps cov if provided
float var_xy = _gps_xy_stddev.get() * _gps_xy_stddev.get();
float var_z = _gps_z_stddev.get() * _gps_z_stddev.get();
float var_vxy = _gps_vxy_stddev.get() * _gps_vxy_stddev.get();
float var_vz = _gps_vz_stddev.get() * _gps_vz_stddev.get();
// if field is not zero, set it to the value provided
if (_sub_gps.get().eph > 1e-3f) {
var_xy = _sub_gps.get().eph * _sub_gps.get().eph;
}
if (_sub_gps.get().epv > 1e-3f) {
var_z = _sub_gps.get().epv * _sub_gps.get().epv;
}
R(0, 0) = var_xy;
R(1, 1) = var_xy;
R(2, 2) = var_z;
R(3, 3) = var_vxy;
R(4, 4) = var_vxy;
R(5, 5) = var_vz;
// get delayed x and P
float t_delay = 0;
int i = 0;
for (i = 1; i < HIST_LEN; i++) {
t_delay = 1.0e-6f * (_timeStamp - _tDelay.get(i)(0, 0));
if (t_delay > _gps_delay.get()) {
break;
}
}
// if you are 3 steps past the delay you wanted, this
// data is probably too old to use
if (t_delay > GPS_DELAY_MAX) {
mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] gps delayed data too old: %8.4f", double(t_delay));
return;
}
Vector<float, n_x> x0 = _xDelay.get(i);
// residual
Vector<float, n_y_gps> r = y - C * x0;
Matrix<float, n_y_gps, n_y_gps> S_I = inv<float, 6>(C * _P * C.transpose() + R);
// fault detection
float beta = (r.transpose() * (S_I * r))(0, 0);
if (beta > BETA_TABLE[n_y_gps]) {
if (_gpsFault < FAULT_MINOR) {
//mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] gps fault, beta: %5.2f", double(beta));
//mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] r: %5.2f %5.2f %5.2f %5.2f %5.2f %5.2f",
//double(r(0)), double(r(1)), double(r(2)),
//double(r(3)), double(r(4)), double(r(5)));
//mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] S_I: %5.2f %5.2f %5.2f %5.2f %5.2f %5.2f",
//double(S_I(0, 0)), double(S_I(1, 1)), double(S_I(2, 2)),
//double(S_I(3, 3)), double(S_I(4, 4)), double(S_I(5, 5)));
_gpsFault = FAULT_MINOR;
}
} else if (_gpsFault) {
_gpsFault = FAULT_NONE;
//mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] GPS OK");
}
// kalman filter correction if no hard fault
if (_gpsFault < fault_lvl_disable) {
Matrix<float, n_x, n_y_gps> K = _P * C.transpose() * S_I;
_x += K * r;
_P -= K * C * _P;
}
}
void BlockLocalPositionEstimator::gpsCheckTimeout()
{
if (_timeStamp - _time_last_gps > GPS_TIMEOUT) {
if (_gpsInitialized) {
_gpsInitialized = false;
_gpsStats.reset();
mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] GPS timeout ");
}
}
}