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EKF: Disable GPS drift checks when the vehicle is moving.

master
Paul Riseborough 7 years ago committed by Lorenz Meier
parent
commit
4d01883f75
  1. 104
      EKF/gps_checks.cpp

104
EKF/gps_checks.cpp

@ -129,85 +129,79 @@ bool Ekf::gps_is_good(struct gps_message *gps) @@ -129,85 +129,79 @@ bool Ekf::gps_is_good(struct gps_message *gps)
_gps_error_norm = fmaxf((gps->eph / _params.req_hacc) , (gps->epv / _params.req_vacc));
_gps_error_norm = fmaxf(_gps_error_norm , (gps->sacc / _params.req_sacc));
// Calculate position movement since last measurement
float delta_posN = 0.0f;
float delta_PosE = 0.0f;
// Calculate time lapsed since last update, limit to prevent numerical errors and calculate a lowpass filter coefficient
const float filt_time_const = 10.0f;
float dt = fminf(fmaxf(float(_time_last_imu - _gps_pos_prev.timestamp) * 1e-6f, 0.001f), filt_time_const);
float filter_coef = dt / filt_time_const;
// The following checks are only valid when the vehicle is at rest
double lat = gps->lat * 1.0e-7;
double lon = gps->lon * 1.0e-7;
if (!_control_status.flags.in_air && _vehicle_at_rest) {
// Calculate position movement since last measurement
float delta_posN = 0.0f;
float delta_PosE = 0.0f;
// calculate position movement since last GPS fix
if (_gps_pos_prev.timestamp > 0) {
map_projection_project(&_gps_pos_prev, lat, lon, &delta_posN, &delta_PosE);
// calculate position movement since last GPS fix
if (_gps_pos_prev.timestamp > 0) {
map_projection_project(&_gps_pos_prev, lat, lon, &delta_posN, &delta_PosE);
} else {
// no previous position has been set
map_projection_init_timestamped(&_gps_pos_prev, lat, lon, _time_last_imu);
_gps_alt_prev = 1e-3f * (float)gps->alt;
}
// Calculate time lapsed since last update, limit to prevent numerical errors and calculate the lowpass filter coefficient
const float filt_time_const = 10.0f;
float dt = fminf(fmaxf(float(_time_last_imu - _gps_pos_prev.timestamp) * 1e-6f, 0.001f), filt_time_const);
float filter_coef = dt / filt_time_const;
} else {
// no previous position has been set
map_projection_init_timestamped(&_gps_pos_prev, lat, lon, _time_last_imu);
_gps_alt_prev = 1e-3f * (float)gps->alt;
// save GPS fix for next time
map_projection_init_timestamped(&_gps_pos_prev, lat, lon, _time_last_imu);
}
// Calculate the horizontal drift velocity components and limit to 10x the threshold
float vel_limit = 10.0f * _params.req_hdrift;
float velN = fminf(fmaxf(delta_posN / dt, -vel_limit), vel_limit);
float velE = fminf(fmaxf(delta_PosE / dt, -vel_limit), vel_limit);
// Calculate the horizontal drift velocity components and limit to 10x the threshold
float vel_limit = 10.0f * _params.req_hdrift;
float velN = fminf(fmaxf(delta_posN / dt, -vel_limit), vel_limit);
float velE = fminf(fmaxf(delta_PosE / dt, -vel_limit), vel_limit);
// Apply a low pass filter
_gpsDriftVelN = velN * filter_coef + _gpsDriftVelN * (1.0f - filter_coef);
_gpsDriftVelE = velE * filter_coef + _gpsDriftVelE * (1.0f - filter_coef);
// Apply a low pass filter
_gpsDriftVelN = velN * filter_coef + _gpsDriftVelN * (1.0f - filter_coef);
_gpsDriftVelE = velE * filter_coef + _gpsDriftVelE * (1.0f - filter_coef);
// Calculate the horizontal drift speed and fail if too high
// This check can only be used if the vehicle is stationary during alignment
if (!_control_status.flags.in_air) {
// Calculate the horizontal drift speed and fail if too high
float drift_speed = sqrtf(_gpsDriftVelN * _gpsDriftVelN + _gpsDriftVelE * _gpsDriftVelE);
_gps_check_fail_status.flags.hdrift = (drift_speed > _params.req_hdrift);
} else {
_gps_check_fail_status.flags.hdrift = false;
}
// Calculate the vertical drift velocity and limit to 10x the threshold
float vz_drift_limit = 10.0f * _params.req_vdrift;
float gps_alt_m = 1e-3f * (float)gps->alt;
float velD = math::constrain(((_gps_alt_prev - gps_alt_m) / dt), -vz_drift_limit, vz_drift_limit);
// Calculate the vertical drift velocity and limit to 10x the threshold
vel_limit = 10.0f * _params.req_vdrift;
float gps_alt_m = 1e-3f * (float)gps->alt;
float velD = math::constrain(((_gps_alt_prev - gps_alt_m) / dt), -vel_limit, vel_limit);
_gps_alt_prev = gps_alt_m;
// Apply a low pass filter to the vertical velocity
_gps_drift_velD = velD * filter_coef + _gps_drift_velD * (1.0f - filter_coef);
// Apply a low pass filter to the vertical velocity
_gps_drift_velD = velD * filter_coef + _gps_drift_velD * (1.0f - filter_coef);
// Fail if the vertical drift speed is too high
// This check can only be used if the vehicle is stationary during alignment
if (!_control_status.flags.in_air) {
// Fail if the vertical drift speed is too high
_gps_check_fail_status.flags.vdrift = (fabsf(_gps_drift_velD) > _params.req_vdrift);
} else {
_gps_check_fail_status.flags.vdrift = false;
}
// Check the magnitude of the filtered horizontal GPS velocity
// This check can only be used if the vehicle is stationary during alignment
if (!_control_status.flags.in_air) {
vel_limit = 10.0f * _params.req_hdrift;
float gps_velN = fminf(fmaxf(gps->vel_ned[0], -vel_limit), vel_limit);
float gps_velE = fminf(fmaxf(gps->vel_ned[1], -vel_limit), vel_limit);
// Check the magnitude of the filtered horizontal GPS velocity
float vxy_drift_limit = 10.0f * _params.req_hdrift;
float gps_velN = fminf(fmaxf(gps->vel_ned[0], -vxy_drift_limit), vxy_drift_limit);
float gps_velE = fminf(fmaxf(gps->vel_ned[1], -vxy_drift_limit), vxy_drift_limit);
_gps_velN_filt = gps_velN * filter_coef + _gps_velN_filt * (1.0f - filter_coef);
_gps_velE_filt = gps_velE * filter_coef + _gps_velE_filt * (1.0f - filter_coef);
float horiz_speed = sqrtf(_gps_velN_filt * _gps_velN_filt + _gps_velE_filt * _gps_velE_filt);
_gps_check_fail_status.flags.hspeed = (horiz_speed > _params.req_hdrift);
} else {
} else if (_control_status.flags.in_air) {
// These checks are always declared as passed when flying
// If on ground and moving, the last result before movemenent commenced is kept
_gps_check_fail_status.flags.hdrift = false;
_gps_check_fail_status.flags.vdrift = false;
_gps_check_fail_status.flags.hspeed = false;
}
// save GPS fix for next time
map_projection_init_timestamped(&_gps_pos_prev, lat, lon, _time_last_imu);
_gps_alt_prev = 1e-3f * (float)gps->alt;
// Check the filtered difference between GPS and EKF vertical velocity
vel_limit = 10.0f * _params.req_vdrift;
float vertVel = fminf(fmaxf((gps->vel_ned[2] - _state.vel(2)), -vel_limit), vel_limit);
float vz_diff_limit = 10.0f * _params.req_vdrift;
float vertVel = fminf(fmaxf((gps->vel_ned[2] - _state.vel(2)), -vz_diff_limit), vz_diff_limit);
_gps_velD_diff_filt = vertVel * filter_coef + _gps_velD_diff_filt * (1.0f - filter_coef);
_gps_check_fail_status.flags.vspeed = (fabsf(_gps_velD_diff_filt) > _params.req_vdrift);

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