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

101 lines
2.5 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_LAND_INIT_COUNT = 1;
static const uint32_t LAND_TIMEOUT = 1000000; // 1.0 s
void BlockLocalPositionEstimator::landInit()
{
// measure
Vector<float, n_y_land> y;
if (landMeasure(y) != OK) {
_landCount = 0;
}
// if finished
if (_landCount > REQ_LAND_INIT_COUNT) {
mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] land init");
_landInitialized = true;
_landFault = FAULT_NONE;
}
}
int BlockLocalPositionEstimator::landMeasure(Vector<float, n_y_land> &y)
{
_time_last_land = _timeStamp;
y.setZero();
_landCount += 1;
return OK;
}
void BlockLocalPositionEstimator::landCorrect()
{
// measure land
Vector<float, n_y_land> y;
if (landMeasure(y) != OK) { return; }
// measurement matrix
Matrix<float, n_y_land, n_x> C;
C.setZero();
// y = -(z - tz)
// TODO could add trig to make this an EKF correction
C(Y_land_z, X_z) = -1; // measured altitude, negative down dir.
C(Y_land_z, X_tz) = 1; // measured altitude, negative down dir.
// use parameter covariance
SquareMatrix<float, n_y_land> R;
R.setZero();
R(0, 0) = _land_z_stddev.get() * _land_z_stddev.get();
// residual
Matrix<float, n_y_land, n_y_land> S_I = inv<float, n_y_land>((C * _P * C.transpose()) + R);
Vector<float, n_y_land> r = y - C * _x;
_pub_innov.get().hagl_innov = r(0);
_pub_innov.get().hagl_innov_var = R(0, 0);
// fault detection
float beta = (r.transpose() * (S_I * r))(0, 0);
if (beta > BETA_TABLE[n_y_land]) {
if (_landFault < FAULT_MINOR) {
_landFault = FAULT_MINOR;
mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] land fault, beta %5.2f", double(beta));
}
// abort correction
return;
} else if (_landFault) { // disable fault if ok
_landFault = FAULT_NONE;
//mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] land OK");
}
// kalman filter correction if no fault
if (_landFault < fault_lvl_disable) {
Matrix<float, n_x, n_y_land> K = _P * C.transpose() * S_I;
Vector<float, n_x> dx = K * r;
correctionLogic(dx);
_x += dx;
_P -= K * C * _P;
}
}
void BlockLocalPositionEstimator::landCheckTimeout()
{
if (_timeStamp - _time_last_land > LAND_TIMEOUT) {
if (_landInitialized) {
_landInitialized = false;
_landCount = 0;
mavlink_and_console_log_info(&mavlink_log_pub, "[lpe] land timeout ");
}
}
}