mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-06-01 02:55:07 +08:00
cleanup checks of range finder data
Signed-off-by: RomanBapst <bapstroman@gmail.com>
This commit is contained in:
committed by
Paul Riseborough
parent
4d37065f1b
commit
00f49e62c2
@@ -46,6 +46,7 @@ add_library(ecl_EKF
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terrain_estimator.cpp
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terrain_estimator.cpp
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vel_pos_fusion.cpp
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vel_pos_fusion.cpp
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gps_yaw_fusion.cpp
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gps_yaw_fusion.cpp
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range_finder_checks.cpp
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)
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)
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add_dependencies(ecl_EKF prebuild_targets)
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add_dependencies(ecl_EKF prebuild_targets)
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+16
-97
@@ -118,9 +118,9 @@ void Ekf::controlFusionModes()
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// Get range data from buffer and check validity
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// Get range data from buffer and check validity
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_range_data_ready = _range_buffer.pop_first_older_than(_imu_sample_delayed.time_us, &_range_sample_delayed);
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_range_data_ready = _range_buffer.pop_first_older_than(_imu_sample_delayed.time_us, &_range_sample_delayed);
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checkRangeDataValidity();
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updateRangeDataValidity();
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if (_range_data_ready && !_rng_hgt_faulty) {
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if (_range_data_ready && _rng_hgt_valid) {
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// correct the range data for position offset relative to the IMU
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// correct the range data for position offset relative to the IMU
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Vector3f pos_offset_body = _params.rng_pos_body - _params.imu_pos_body;
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Vector3f pos_offset_body = _params.rng_pos_body - _params.imu_pos_body;
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Vector3f pos_offset_earth = _R_to_earth * pos_offset_body;
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Vector3f pos_offset_earth = _R_to_earth * pos_offset_body;
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@@ -910,23 +910,25 @@ void Ekf::controlHeightSensorTimeouts()
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// handle the case we are using range finder for height
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// handle the case we are using range finder for height
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if (_control_status.flags.rng_hgt) {
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if (_control_status.flags.rng_hgt) {
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// check if range finder data is available
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const rangeSample &rng_init = _range_buffer.get_newest();
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bool rng_data_available = ((_time_last_imu - rng_init.time_us) < 2 * RNG_MAX_INTERVAL);
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// check if baro data is available
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// check if baro data is available
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const baroSample &baro_init = _baro_buffer.get_newest();
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const baroSample &baro_init = _baro_buffer.get_newest();
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bool baro_data_available = ((_time_last_imu - baro_init.time_us) < 2 * BARO_MAX_INTERVAL);
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bool baro_data_available = ((_time_last_imu - baro_init.time_us) < 2 * BARO_MAX_INTERVAL);
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// reset to baro if we have no range data and baro data is available
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// reset to baro if we have no range data and baro data is available
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bool reset_to_baro = !rng_data_available && baro_data_available;
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bool reset_to_baro = !_rng_hgt_valid && baro_data_available;
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// reset to range data if it is available
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if (_rng_hgt_valid) {
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bool reset_to_rng = rng_data_available;
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if (reset_to_baro) {
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// reset the height mode
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setControlRangeHeight();
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// request a reset
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reset_height = true;
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ECL_WARN_TIMESTAMPED("EKF rng hgt timeout - reset to rng hgt");
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} else if (reset_to_baro) {
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// set height sensor health
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// set height sensor health
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_rng_hgt_faulty = true;
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_baro_hgt_faulty = false;
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_baro_hgt_faulty = false;
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// reset the height mode
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// reset the height mode
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@@ -936,17 +938,6 @@ void Ekf::controlHeightSensorTimeouts()
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reset_height = true;
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reset_height = true;
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ECL_WARN_TIMESTAMPED("EKF rng hgt timeout - reset to baro");
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ECL_WARN_TIMESTAMPED("EKF rng hgt timeout - reset to baro");
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} else if (reset_to_rng) {
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// set height sensor health
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_rng_hgt_faulty = false;
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// reset the height mode
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setControlRangeHeight();
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// request a reset
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reset_height = true;
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ECL_WARN_TIMESTAMPED("EKF rng hgt timeout - reset to rng hgt");
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} else {
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} else {
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// we have nothing to reset to
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// we have nothing to reset to
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reset_height = false;
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reset_height = false;
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@@ -1016,7 +1007,7 @@ void Ekf::controlHeightFusion()
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if (_params.vdist_sensor_type == VDIST_SENSOR_BARO) {
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if (_params.vdist_sensor_type == VDIST_SENSOR_BARO) {
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if (_range_aid_mode_selected && _range_data_ready && !_rng_hgt_faulty) {
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if (_range_aid_mode_selected && _range_data_ready && _rng_hgt_valid) {
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setControlRangeHeight();
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setControlRangeHeight();
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_fuse_height = true;
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_fuse_height = true;
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@@ -1062,7 +1053,7 @@ void Ekf::controlHeightFusion()
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}
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}
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// set the height data source to range if requested
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// set the height data source to range if requested
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if ((_params.vdist_sensor_type == VDIST_SENSOR_RANGE) && !_rng_hgt_faulty) {
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if ((_params.vdist_sensor_type == VDIST_SENSOR_RANGE) && _rng_hgt_valid) {
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setControlRangeHeight();
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setControlRangeHeight();
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_fuse_height = _range_data_ready;
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_fuse_height = _range_data_ready;
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@@ -1098,7 +1089,7 @@ void Ekf::controlHeightFusion()
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// Determine if GPS should be used as the height source
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// Determine if GPS should be used as the height source
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if (_params.vdist_sensor_type == VDIST_SENSOR_GPS) {
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if (_params.vdist_sensor_type == VDIST_SENSOR_GPS) {
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if (_range_aid_mode_selected && _range_data_ready && !_rng_hgt_faulty) {
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if (_range_aid_mode_selected && _range_data_ready && _rng_hgt_valid) {
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setControlRangeHeight();
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setControlRangeHeight();
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_fuse_height = true;
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_fuse_height = true;
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@@ -1161,7 +1152,7 @@ void Ekf::controlHeightFusion()
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}
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}
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if ((_time_last_imu - _time_last_hgt_fuse) > 2 * RNG_MAX_INTERVAL && _control_status.flags.rng_hgt
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if ((_time_last_imu - _time_last_hgt_fuse) > 2 * RNG_MAX_INTERVAL && _control_status.flags.rng_hgt
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&& (!_range_data_ready || _rng_hgt_faulty)) {
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&& (!_range_data_ready || !_rng_hgt_valid)) {
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// If we are supposed to be using range finder data as the primary height sensor, have missed or rejected measurements
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// If we are supposed to be using range finder data as the primary height sensor, have missed or rejected measurements
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// and are on the ground, then synthesise a measurement at the expected on ground value
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// and are on the ground, then synthesise a measurement at the expected on ground value
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@@ -1210,78 +1201,6 @@ void Ekf::checkRangeAidSuitability()
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}
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}
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}
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}
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void Ekf::checkRangeDataValidity()
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{
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// check if out of date
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if ((_imu_sample_delayed.time_us - _range_sample_delayed .time_us) > 2 * RNG_MAX_INTERVAL) {
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_rng_hgt_faulty = true;
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return;
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}
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// Don't allow faulty flag to clear unless range data is continuous
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if (_rng_hgt_faulty && !_range_data_continuous) {
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return;
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}
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// Don't run the checks after this unless we have retrieved new data from the buffer
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if (!_range_data_ready) {
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return;
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} else {
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// reset fault status when we get new data
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_rng_hgt_faulty = (_range_sample_delayed.quality == 0);
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}
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// Check if excessively tilted
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if (_R_rng_to_earth_2_2 < _params.range_cos_max_tilt) {
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_rng_hgt_faulty = true;
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return;
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}
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// Check if out of range
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if ((_range_sample_delayed.rng > _rng_valid_max_val)
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|| (_range_sample_delayed.rng < _rng_valid_min_val)) {
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if (_control_status.flags.in_air) {
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_rng_hgt_faulty = true;
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return;
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} else {
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// Range finders can fail to provide valid readings when resting on the ground
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// or being handled by the user, which prevents use of as a primary height sensor.
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// To work around this issue, we replace out of range data with the expected on ground value.
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_range_sample_delayed.rng = _params.rng_gnd_clearance;
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return;
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}
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}
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// Check for "stuck" range finder measurements when range was not valid for certain period
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// This handles a failure mode observed with some lidar sensors
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if (((_range_sample_delayed.time_us - _time_last_rng_ready) > (uint64_t)10e6) &&
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_control_status.flags.in_air) {
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// require a variance of rangefinder values to check for "stuck" measurements
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if (_rng_stuck_max_val - _rng_stuck_min_val > _params.range_stuck_threshold) {
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_time_last_rng_ready = _range_sample_delayed.time_us;
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_rng_stuck_min_val = 0.0f;
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_rng_stuck_max_val = 0.0f;
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_control_status.flags.rng_stuck = false;
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} else {
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if (_range_sample_delayed.rng > _rng_stuck_max_val) {
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_rng_stuck_max_val = _range_sample_delayed.rng;
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}
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if (_rng_stuck_min_val < 0.1f || _range_sample_delayed.rng < _rng_stuck_min_val) {
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_rng_stuck_min_val = _range_sample_delayed.rng;
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}
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_control_status.flags.rng_stuck = true;
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_rng_hgt_faulty = true;
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}
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} else {
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_time_last_rng_ready = _range_sample_delayed.time_us;
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}
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}
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void Ekf::controlAirDataFusion()
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void Ekf::controlAirDataFusion()
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{
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{
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// control activation and initialisation/reset of wind states required for airspeed fusion
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// control activation and initialisation/reset of wind states required for airspeed fusion
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@@ -464,8 +464,9 @@ private:
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// height sensor status
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// height sensor status
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bool _baro_hgt_faulty{false}; ///< true if valid baro data is unavailable for use
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bool _baro_hgt_faulty{false}; ///< true if valid baro data is unavailable for use
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bool _gps_hgt_intermittent{false}; ///< true if gps height into the buffer is intermittent
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bool _gps_hgt_intermittent{false}; ///< true if gps height into the buffer is intermittent
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bool _rng_hgt_faulty{false}; ///< true if valid range finder height data is unavailable for use
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bool _rng_hgt_valid{false}; ///< true if range finder sample retrieved from buffer is valid
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int _primary_hgt_source{VDIST_SENSOR_BARO}; ///< specifies primary source of height data
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int _primary_hgt_source{VDIST_SENSOR_BARO}; ///< specifies primary source of height data
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uint64_t _time_bad_rng_signal_quality{0}; ///< timestamp at which range finder signal quality was 0 (used for hysteresis)
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// imu fault status
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// imu fault status
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uint64_t _time_bad_vert_accel{0}; ///< last time a bad vertical accel was detected (uSec)
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uint64_t _time_bad_vert_accel{0}; ///< last time a bad vertical accel was detected (uSec)
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@@ -648,7 +649,7 @@ private:
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bool isRangeAidSuitable() { return _is_range_aid_suitable; }
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bool isRangeAidSuitable() { return _is_range_aid_suitable; }
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// check for "stuck" range finder measurements when rng was not valid for certain period
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// check for "stuck" range finder measurements when rng was not valid for certain period
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void checkRangeDataValidity();
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void updateRangeDataValidity();
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// return the square of two floating point numbers - used in auto coded sections
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// return the square of two floating point numbers - used in auto coded sections
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static constexpr float sq(float var) { return var * var; }
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static constexpr float sq(float var) { return var * var; }
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@@ -697,7 +698,7 @@ private:
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void resetWindStates();
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void resetWindStates();
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// check that the range finder data is continuous
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// check that the range finder data is continuous
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void checkRangeDataContinuity();
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void updateRangeDataContinuity();
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// Increase the yaw error variance of the quaternions
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// Increase the yaw error variance of the quaternions
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// Argument is additional yaw variance in rad**2
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// Argument is additional yaw variance in rad**2
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@@ -0,0 +1,144 @@
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/****************************************************************************
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*
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* Copyright (c) 2019 Estimation and Control Library (ECL). All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name ECL nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file range_finder_checks.cpp
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* Perform checks on range finder data in order to evaluate validity.
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*
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*
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*/
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#include "ekf.h"
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#define RNG_BAD_SIG_HYST (uint64_t)3e6 // range finder data needs to have 3 seconds of non-zero signal quality to be valid
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// check that the range finder data is continuous
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void Ekf::updateRangeDataContinuity()
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{
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// update range data continuous flag (1Hz ie 2000 ms)
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/* Timing in micro seconds */
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/* Apply a 2.0 sec low pass filter to the time delta from the last range finder updates */
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float alpha = 0.5f * _dt_update;
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_dt_last_range_update_filt_us = _dt_last_range_update_filt_us * (1.0f - alpha) + alpha *
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(_imu_sample_delayed.time_us - _range_sample_delayed.time_us);
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_dt_last_range_update_filt_us = fminf(_dt_last_range_update_filt_us, 4e6f);
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if (_dt_last_range_update_filt_us < 2e6f) {
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_range_data_continuous = true;
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} else {
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_range_data_continuous = false;
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}
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}
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void Ekf::updateRangeDataValidity()
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{
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updateRangeDataContinuity();
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// check if out of date
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if ((_imu_sample_delayed.time_us - _range_sample_delayed .time_us) > 2 * RNG_MAX_INTERVAL) {
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_rng_hgt_valid = false;
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return;
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}
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// Don't allow faulty flag to clear unless range data is continuous
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if (!_rng_hgt_valid && !_range_data_continuous) {
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return;
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}
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// Don't run the checks after this unless we have retrieved new data from the buffer
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if (!_range_data_ready) {
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return;
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}
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if (_range_sample_delayed.quality == 0) {
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_time_bad_rng_signal_quality = _imu_sample_delayed.time_us;
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_rng_hgt_valid = false;
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} else if (_time_bad_rng_signal_quality > 0 && _imu_sample_delayed.time_us - _time_bad_rng_signal_quality > RNG_BAD_SIG_HYST) {
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_time_bad_rng_signal_quality = 0;
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_rng_hgt_valid = true;
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}
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// Check if excessively tilted
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||||||
|
if (_R_rng_to_earth_2_2 < _params.range_cos_max_tilt) {
|
||||||
|
_rng_hgt_valid = false;
|
||||||
|
return;
|
||||||
|
}
|
||||||
|
|
||||||
|
// Check if out of range
|
||||||
|
if ((_range_sample_delayed.rng > _rng_valid_max_val)
|
||||||
|
|| (_range_sample_delayed.rng < _rng_valid_min_val)) {
|
||||||
|
if (_control_status.flags.in_air) {
|
||||||
|
_rng_hgt_valid = false;
|
||||||
|
return;
|
||||||
|
} else {
|
||||||
|
// Range finders can fail to provide valid readings when resting on the ground
|
||||||
|
// or being handled by the user, which prevents use of as a primary height sensor.
|
||||||
|
// To work around this issue, we replace out of range data with the expected on ground value.
|
||||||
|
_range_sample_delayed.rng = _params.rng_gnd_clearance;
|
||||||
|
return;
|
||||||
|
}
|
||||||
|
}
|
||||||
|
|
||||||
|
// Check for "stuck" range finder measurements when range was not valid for certain period
|
||||||
|
// This handles a failure mode observed with some lidar sensors
|
||||||
|
if (((_range_sample_delayed.time_us - _time_last_rng_ready) > (uint64_t)10e6) &&
|
||||||
|
_control_status.flags.in_air) {
|
||||||
|
|
||||||
|
// require a variance of rangefinder values to check for "stuck" measurements
|
||||||
|
if (_rng_stuck_max_val - _rng_stuck_min_val > _params.range_stuck_threshold) {
|
||||||
|
_time_last_rng_ready = _range_sample_delayed.time_us;
|
||||||
|
_rng_stuck_min_val = 0.0f;
|
||||||
|
_rng_stuck_max_val = 0.0f;
|
||||||
|
_control_status.flags.rng_stuck = false;
|
||||||
|
|
||||||
|
} else {
|
||||||
|
if (_range_sample_delayed.rng > _rng_stuck_max_val) {
|
||||||
|
_rng_stuck_max_val = _range_sample_delayed.rng;
|
||||||
|
}
|
||||||
|
|
||||||
|
if (_rng_stuck_min_val < 0.1f || _range_sample_delayed.rng < _rng_stuck_min_val) {
|
||||||
|
_rng_stuck_min_val = _range_sample_delayed.rng;
|
||||||
|
}
|
||||||
|
|
||||||
|
_control_status.flags.rng_stuck = true;
|
||||||
|
_rng_hgt_valid = false;
|
||||||
|
}
|
||||||
|
|
||||||
|
} else {
|
||||||
|
_time_last_rng_ready = _range_sample_delayed.time_us;
|
||||||
|
}
|
||||||
|
}
|
||||||
@@ -56,7 +56,7 @@ bool Ekf::initHagl()
|
|||||||
_terrain_var = sq(_params.rng_gnd_clearance);
|
_terrain_var = sq(_params.rng_gnd_clearance);
|
||||||
initialized = true;
|
initialized = true;
|
||||||
|
|
||||||
} else if (!_rng_hgt_faulty
|
} else if (_rng_hgt_valid
|
||||||
&& (_time_last_imu - latest_measurement.time_us) < (uint64_t)2e5
|
&& (_time_last_imu - latest_measurement.time_us) < (uint64_t)2e5
|
||||||
&& _R_rng_to_earth_2_2 > _params.range_cos_max_tilt) {
|
&& _R_rng_to_earth_2_2 > _params.range_cos_max_tilt) {
|
||||||
// if we have a fresh measurement, use it to initialise the terrain estimator
|
// if we have a fresh measurement, use it to initialise the terrain estimator
|
||||||
@@ -87,9 +87,6 @@ bool Ekf::initHagl()
|
|||||||
|
|
||||||
void Ekf::runTerrainEstimator()
|
void Ekf::runTerrainEstimator()
|
||||||
{
|
{
|
||||||
// Perform a continuity check on range finder data
|
|
||||||
checkRangeDataContinuity();
|
|
||||||
|
|
||||||
// Perform initialisation check and
|
// Perform initialisation check and
|
||||||
// on ground, continuously reset the terrain estimator
|
// on ground, continuously reset the terrain estimator
|
||||||
if (!_terrain_initialised || !_control_status.flags.in_air) {
|
if (!_terrain_initialised || !_control_status.flags.in_air) {
|
||||||
@@ -110,7 +107,7 @@ void Ekf::runTerrainEstimator()
|
|||||||
_terrain_var = math::constrain(_terrain_var, 0.0f, 1e4f);
|
_terrain_var = math::constrain(_terrain_var, 0.0f, 1e4f);
|
||||||
|
|
||||||
// Fuse range finder data if available
|
// Fuse range finder data if available
|
||||||
if (_range_data_ready && !_rng_hgt_faulty) {
|
if (_range_data_ready && _rng_hgt_valid) {
|
||||||
fuseHagl();
|
fuseHagl();
|
||||||
|
|
||||||
// update range sensor angle parameters in case they have changed
|
// update range sensor angle parameters in case they have changed
|
||||||
@@ -321,19 +318,3 @@ void Ekf::getHaglInnovVar(float *hagl_innov_var)
|
|||||||
{
|
{
|
||||||
memcpy(hagl_innov_var, &_hagl_innov_var, sizeof(_hagl_innov_var));
|
memcpy(hagl_innov_var, &_hagl_innov_var, sizeof(_hagl_innov_var));
|
||||||
}
|
}
|
||||||
|
|
||||||
// check that the range finder data is continuous
|
|
||||||
void Ekf::checkRangeDataContinuity()
|
|
||||||
{
|
|
||||||
// update range data continuous flag (1Hz ie 2000 ms)
|
|
||||||
/* Timing in micro seconds */
|
|
||||||
|
|
||||||
/* Apply a 2.0 sec low pass filter to the time delta from the last range finder updates */
|
|
||||||
float alpha = 0.5f * _dt_update;
|
|
||||||
_dt_last_range_update_filt_us = _dt_last_range_update_filt_us * (1.0f - alpha) + alpha *
|
|
||||||
(_imu_sample_delayed.time_us - _range_sample_delayed.time_us);
|
|
||||||
|
|
||||||
_dt_last_range_update_filt_us = fminf(_dt_last_range_update_filt_us, 4e6f);
|
|
||||||
|
|
||||||
_range_data_continuous = (_dt_last_range_update_filt_us < 2e6f);
|
|
||||||
}
|
|
||||||
|
|||||||
Reference in New Issue
Block a user