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Merge pull request #2667 from mhkabir/vis_yaw
External heading support for AttitudeEstimatorQ (Vision/Mocap)
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@@ -56,6 +56,8 @@
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#include <uORB/topics/vehicle_attitude.h>
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#include <uORB/topics/vehicle_control_mode.h>
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#include <uORB/topics/vehicle_global_position.h>
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#include <uORB/topics/vision_position_estimate.h>
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#include <uORB/topics/att_pos_mocap.h>
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#include <uORB/topics/parameter_update.h>
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#include <drivers/drv_hrt.h>
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@@ -117,22 +119,27 @@ private:
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int _sensors_sub = -1;
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int _params_sub = -1;
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int _vision_sub = -1;
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int _mocap_sub = -1;
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int _global_pos_sub = -1;
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orb_advert_t _att_pub = nullptr;
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struct {
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param_t w_acc;
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param_t w_mag;
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param_t w_ext_hdg;
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param_t w_gyro_bias;
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param_t mag_decl;
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param_t mag_decl_auto;
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param_t acc_comp;
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param_t bias_max;
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param_t vibe_thresh;
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param_t ext_hdg_mode;
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} _params_handles; /**< handles for interesting parameters */
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float _w_accel = 0.0f;
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float _w_mag = 0.0f;
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float _w_ext_hdg = 0.0f;
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float _w_gyro_bias = 0.0f;
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float _mag_decl = 0.0f;
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bool _mag_decl_auto = false;
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@@ -140,11 +147,18 @@ private:
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float _bias_max = 0.0f;
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float _vibration_warning_threshold = 1.0f;
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hrt_abstime _vibration_warning_timestamp = 0;
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int _ext_hdg_mode = 0;
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Vector<3> _gyro;
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Vector<3> _accel;
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Vector<3> _mag;
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vision_position_estimate_s _vision = {};
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Vector<3> _vision_hdg;
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att_pos_mocap_s _mocap = {};
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Vector<3> _mocap_hdg;
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Quaternion _q;
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Vector<3> _rates;
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Vector<3> _gyro_bias;
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@@ -168,6 +182,7 @@ private:
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bool _data_good = false;
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bool _failsafe = false;
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bool _vibration_warning = false;
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bool _ext_hdg_good = false;
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int _mavlink_fd = -1;
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@@ -196,12 +211,14 @@ AttitudeEstimatorQ::AttitudeEstimatorQ() :
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_params_handles.w_acc = param_find("ATT_W_ACC");
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_params_handles.w_mag = param_find("ATT_W_MAG");
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_params_handles.w_ext_hdg = param_find("ATT_W_EXT_HDG");
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_params_handles.w_gyro_bias = param_find("ATT_W_GYRO_BIAS");
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_params_handles.mag_decl = param_find("ATT_MAG_DECL");
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_params_handles.mag_decl_auto = param_find("ATT_MAG_DECL_A");
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_params_handles.acc_comp = param_find("ATT_ACC_COMP");
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_params_handles.bias_max = param_find("ATT_BIAS_MAX");
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_params_handles.vibe_thresh = param_find("ATT_VIBE_THRESH");
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_params_handles.ext_hdg_mode = param_find("ATT_EXT_HDG_M");
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}
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/**
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@@ -269,6 +286,10 @@ void AttitudeEstimatorQ::task_main_trampoline(int argc, char *argv[])
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void AttitudeEstimatorQ::task_main()
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{
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_sensors_sub = orb_subscribe(ORB_ID(sensor_combined));
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_vision_sub = orb_subscribe(ORB_ID(vision_position_estimate));
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_mocap_sub = orb_subscribe(ORB_ID(att_pos_mocap));
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_params_sub = orb_subscribe(ORB_ID(parameter_update));
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_global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
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@@ -374,6 +395,47 @@ void AttitudeEstimatorQ::task_main()
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}
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}
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// Update vision and motion capture heading
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bool vision_updated = false;
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orb_check(_vision_sub, &vision_updated);
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bool mocap_updated = false;
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orb_check(_mocap_sub, &mocap_updated);
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if (vision_updated) {
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orb_copy(ORB_ID(vision_position_estimate), _vision_sub, &_vision);
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math::Quaternion q(_vision.q);
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math::Matrix<3, 3> Rvis = q.to_dcm();
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math::Vector<3> v(1.0f, 0.0f, 0.4f);
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// Rvis is Rwr (robot respect to world) while v is respect to world.
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// Hence Rvis must be transposed having (Rwr)' * Vw
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// Rrw * Vw = vn. This way we have consistency
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_vision_hdg = Rvis.transposed() * v;
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}
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if (mocap_updated) {
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orb_copy(ORB_ID(att_pos_mocap), _mocap_sub, &_mocap);
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math::Quaternion q(_mocap.q);
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math::Matrix<3, 3> Rmoc = q.to_dcm();
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math::Vector<3> v(1.0f, 0.0f, 0.4f);
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// Rmoc is Rwr (robot respect to world) while v is respect to world.
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// Hence Rmoc must be transposed having (Rwr)' * Vw
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// Rrw * Vw = vn. This way we have consistency
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_mocap_hdg = Rmoc.transposed() * v;
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}
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// Check for timeouts on data
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if (_ext_hdg_mode == 1) {
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_ext_hdg_good = _vision.timestamp_boot > 0 && (hrt_elapsed_time(&_vision.timestamp_boot) < 500000);
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} else if (_ext_hdg_mode == 2) {
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_ext_hdg_good = _mocap.timestamp_boot > 0 && (hrt_elapsed_time(&_mocap.timestamp_boot) < 500000);
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}
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bool gpos_updated;
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orb_check(_global_pos_sub, &gpos_updated);
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@@ -478,6 +540,7 @@ void AttitudeEstimatorQ::update_parameters(bool force)
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param_get(_params_handles.w_acc, &_w_accel);
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param_get(_params_handles.w_mag, &_w_mag);
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param_get(_params_handles.w_ext_hdg, &_w_ext_hdg);
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param_get(_params_handles.w_gyro_bias, &_w_gyro_bias);
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float mag_decl_deg = 0.0f;
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param_get(_params_handles.mag_decl, &mag_decl_deg);
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@@ -490,6 +553,7 @@ void AttitudeEstimatorQ::update_parameters(bool force)
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_acc_comp = acc_comp_int != 0;
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param_get(_params_handles.bias_max, &_bias_max);
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param_get(_params_handles.vibe_thresh, &_vibration_warning_threshold);
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param_get(_params_handles.ext_hdg_mode, &_ext_hdg_mode);
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}
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}
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@@ -545,12 +609,34 @@ bool AttitudeEstimatorQ::update(float dt)
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// Angular rate of correction
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Vector<3> corr;
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// Magnetometer correction
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// Project mag field vector to global frame and extract XY component
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Vector<3> mag_earth = _q.conjugate(_mag);
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float mag_err = _wrap_pi(atan2f(mag_earth(1), mag_earth(0)) - _mag_decl);
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// Project magnetometer correction to body frame
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corr += _q.conjugate_inversed(Vector<3>(0.0f, 0.0f, -mag_err)) * _w_mag;
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if (_ext_hdg_mode > 0 && _ext_hdg_good) {
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if (_ext_hdg_mode == 1) {
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// Vision heading correction
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// Project heading to global frame and extract XY component
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Vector<3> vision_hdg_earth = _q.conjugate(_vision_hdg);
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float vision_hdg_err = _wrap_pi(atan2f(vision_hdg_earth(1), vision_hdg_earth(0)));
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// Project correction to body frame
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corr += _q.conjugate_inversed(Vector<3>(0.0f, 0.0f, -vision_hdg_err)) * _w_ext_hdg;
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}
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if (_ext_hdg_mode == 2) {
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// Mocap heading correction
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// Project heading to global frame and extract XY component
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Vector<3> mocap_hdg_earth = _q.conjugate(_mocap_hdg);
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float mocap_hdg_err = _wrap_pi(atan2f(mocap_hdg_earth(1), mocap_hdg_earth(0)));
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// Project correction to body frame
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corr += _q.conjugate_inversed(Vector<3>(0.0f, 0.0f, -mocap_hdg_err)) * _w_ext_hdg;
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}
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}
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if (_ext_hdg_mode == 0 || !_ext_hdg_good) {
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// Magnetometer correction
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// Project mag field vector to global frame and extract XY component
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Vector<3> mag_earth = _q.conjugate(_mag);
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float mag_err = _wrap_pi(atan2f(mag_earth(1), mag_earth(0)) - _mag_decl);
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// Project magnetometer correction to body frame
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corr += _q.conjugate_inversed(Vector<3>(0.0f, 0.0f, -mag_err)) * _w_mag;
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}
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// Accelerometer correction
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// Project 'k' unit vector of earth frame to body frame
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@@ -61,6 +61,15 @@ PARAM_DEFINE_FLOAT(ATT_W_ACC, 0.2f);
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*/
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PARAM_DEFINE_FLOAT(ATT_W_MAG, 0.1f);
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/**
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* Complimentary filter external heading weight
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*
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* @group Attitude Q estimator
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* @min 0
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* @max 1
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*/
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PARAM_DEFINE_FLOAT(ATT_W_EXT_HDG, 0.1f);
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/**
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* Complimentary filter gyroscope bias weight
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*
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@@ -93,6 +102,17 @@ PARAM_DEFINE_FLOAT(ATT_MAG_DECL, 0.0f);
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*/
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PARAM_DEFINE_INT32(ATT_MAG_DECL_A, 1);
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/**
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* External heading usage mode (from Motion capture/Vision)
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* Set to 1 to use heading estimate from vision.
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* Set to 2 to use heading from motion capture.
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*
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* @group Attitude Q estimator
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* @min 0
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* @max 2
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*/
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PARAM_DEFINE_INT32(ATT_EXT_HDG_M, 0);
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/**
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* Enable acceleration compensation based on GPS
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* velocity.
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