forked from Archive/PX4-Autopilot
Update gps interface
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a19c29e708
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@ -67,7 +67,7 @@ struct gps_message {
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float epv; ///< GPS vertical position accuracy in m
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float sacc; ///< GPS speed accuracy in m/s
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float vel_m_s; ///< GPS ground speed (m/sec)
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float vel_ned[3]; ///< GPS ground speed NED - TODO: make Vector3f
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Vector3f vel_ned; ///< GPS ground speed NED - TODO: make Vector3f
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bool vel_ned_valid; ///< GPS ground speed is valid
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uint8_t nsats; ///< number of satellites used
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float pdop; ///< position dilution of precision
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@ -182,7 +182,7 @@ void EstimatorInterface::setMagData(uint64_t time_usec, float (&data)[3])
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}
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}
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void EstimatorInterface::setGpsData(uint64_t time_usec, const gps_message &gps)
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void EstimatorInterface::setGpsData(const gps_message &gps)
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{
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if (!_initialised || _gps_buffer_fail) {
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return;
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@ -202,15 +202,17 @@ void EstimatorInterface::setGpsData(uint64_t time_usec, const gps_message &gps)
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// limit data rate to prevent data being lost
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bool need_gps = (_params.fusion_mode & MASK_USE_GPS) || (_params.vdist_sensor_type == VDIST_SENSOR_GPS);
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if (((time_usec - _time_last_gps) > _min_obs_interval_us) && need_gps && gps.fix_type > 2) {
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// TODO: remove checks that are not timing related
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if (((gps.time_usec - _time_last_gps) > _min_obs_interval_us) && need_gps && gps.fix_type > 2) {
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_time_last_gps = gps.time_usec;
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gpsSample gps_sample_new;
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gps_sample_new.time_us = gps.time_usec - _params.gps_delay_ms * 1000;
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gps_sample_new.time_us -= FILTER_UPDATE_PERIOD_MS * 1000 / 2;
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_time_last_gps = time_usec;
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gps_sample_new.time_us = math::max(gps_sample_new.time_us, _imu_sample_delayed.time_us);
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gps_sample_new.vel = Vector3f(gps.vel_ned);
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gps_sample_new.vel = gps.vel_ned;
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_gps_speed_valid = gps.vel_ned_valid;
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gps_sample_new.sacc = gps.sacc;
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@ -179,7 +179,7 @@ public:
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void setMagData(uint64_t time_usec, float (&data)[3]);
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void setGpsData(uint64_t time_usec, const gps_message &gps);
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void setGpsData(const gps_message &gps);
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void setBaroData(uint64_t time_usec, float data);
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@ -175,7 +175,7 @@ bool Ekf::gps_is_good(const gps_message &gps)
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_gps_check_fail_status.flags.vdrift = (_gps_drift_metrics[1] > _params.req_vdrift);
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// Check the magnitude of the filtered horizontal GPS velocity
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Vector2f gps_velNE = matrix::constrain(Vector2f(gps.vel_ned[0], gps.vel_ned[1]), // TODO: when vel_ned vector3f use .xy()
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Vector2f gps_velNE = matrix::constrain(Vector2f(gps.vel_ned.xy()),
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-10.0f * _params.req_hdrift,
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10.0f * _params.req_hdrift);
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_gps_velNE_filt = gps_velNE * filter_coef + _gps_velNE_filt * (1.0f - filter_coef);
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@ -204,7 +204,7 @@ bool Ekf::gps_is_good(const gps_message &gps)
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// Check the filtered difference between GPS and EKF vertical velocity
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float vz_diff_limit = 10.0f * _params.req_vdrift;
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float vertVel = fminf(fmaxf((gps.vel_ned[2] - _state.vel(2)), -vz_diff_limit), vz_diff_limit);
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float vertVel = fminf(fmaxf((gps.vel_ned(2) - _state.vel(2)), -vz_diff_limit), vz_diff_limit);
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_gps_velD_diff_filt = vertVel * filter_coef + _gps_velD_diff_filt * (1.0f - filter_coef);
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_gps_check_fail_status.flags.vspeed = (fabsf(_gps_velD_diff_filt) > _params.req_vdrift);
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@ -16,7 +16,7 @@ Gps::~Gps()
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void Gps::send(uint64_t time)
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{
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_gps_data.time_usec = time;
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_ekf->setGpsData(time, _gps_data);
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_ekf->setGpsData(_gps_data);
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}
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void Gps::setData(const gps_message& gps)
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@ -41,9 +41,7 @@ void Gps::setLongitude(int32_t lon)
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void Gps::setVelocity(const Vector3f& vel)
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{
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_gps_data.vel_ned[0] = vel(0);
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_gps_data.vel_ned[1] = vel(1);
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_gps_data.vel_ned[2] = vel(2);
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_gps_data.vel_ned = vel;
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}
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void Gps::stepHeightByMeters(float hgt_change)
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@ -79,9 +77,7 @@ gps_message Gps::getDefaultGpsData()
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gps_data.epv = 0.8f;
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gps_data.sacc = 0.2f;
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gps_data.vel_m_s = 0.0;
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gps_data.vel_ned[0] = 0.0f;
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gps_data.vel_ned[1] = 0.0f;
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gps_data.vel_ned[2] = 0.0f;
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gps_data.vel_ned.setZero();
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gps_data.vel_ned_valid = 1;
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gps_data.nsats = 16;
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gps_data.pdop = 0.0f;
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