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position_estimator_inav: accelerometer bias estimation for Z, default weights for GPS updated
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@@ -167,9 +167,9 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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int baro_init_num = 200;
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float baro_alt0 = 0.0f; /* to determine while start up */
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double lat_current = 0.0; //[°]] --> 47.0
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double lon_current = 0.0; //[°]] -->8.5
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double alt_current = 0.0; //[m] above MSL
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double lat_current = 0.0f; //[°] --> 47.0
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double lon_current = 0.0f; //[°] --> 8.5
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double alt_current = 0.0f; //[m] above MSL
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uint32_t accel_counter = 0;
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uint32_t baro_counter = 0;
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@@ -302,8 +302,12 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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hrt_abstime pub_last = hrt_absolute_time();
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uint32_t pub_interval = 4000; // limit publish rate to 250 Hz
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/* acceleration in NED frame */
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float accel_NED[3] = { 0.0f, 0.0f, -CONSTANTS_ONE_G };
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/* store error when sensor updates, but correct on each time step to avoid jumps in estimated value */
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float accel_corr[] = { 0.0f, 0.0f, 0.0f }; // N E D
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float accel_bias[] = { 0.0f, 0.0f, 0.0f }; // body frame
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float baro_corr = 0.0f; // D
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float gps_corr[2][2] = {
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{ 0.0f, 0.0f }, // N (pos, vel)
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@@ -369,9 +373,9 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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if (sensor.accelerometer_counter > accel_counter) {
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if (att.R_valid) {
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/* correct accel bias, now only for Z */
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sensor.accelerometer_m_s2[2] -= accel_bias[2];
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/* transform acceleration vector from body frame to NED frame */
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float accel_NED[3];
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for (int i = 0; i < 3; i++) {
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accel_NED[i] = 0.0f;
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@@ -425,7 +429,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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local_pos.home_timestamp = hrt_absolute_time();
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z_est[0] += sonar_corr;
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sonar_corr = 0.0f;
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sonar_corr_filtered = 0.0;
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sonar_corr_filtered = 0.0f;
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}
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}
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}
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@@ -470,6 +474,10 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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float dt = t_prev > 0 ? (t - t_prev) / 1000000.0f : 0.0f;
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t_prev = t;
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/* accel bias correction, now only for Z
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* not strictly correct, but stable and works */
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accel_bias[2] += (accel_NED[2] + CONSTANTS_ONE_G) * params.w_acc_bias * dt;
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/* inertial filter prediction for altitude */
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inertial_filter_predict(dt, z_est);
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@@ -44,10 +44,11 @@ PARAM_DEFINE_INT32(INAV_USE_GPS, 1);
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PARAM_DEFINE_FLOAT(INAV_W_ALT_BARO, 1.0f);
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PARAM_DEFINE_FLOAT(INAV_W_ALT_ACC, 50.0f);
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PARAM_DEFINE_FLOAT(INAV_W_ALT_SONAR, 3.0f);
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PARAM_DEFINE_FLOAT(INAV_W_POS_GPS_P, 4.0f);
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PARAM_DEFINE_FLOAT(INAV_W_POS_GPS_V, 0.0f);
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PARAM_DEFINE_FLOAT(INAV_W_POS_GPS_P, 1.0f);
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PARAM_DEFINE_FLOAT(INAV_W_POS_GPS_V, 2.0f);
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PARAM_DEFINE_FLOAT(INAV_W_POS_ACC, 10.0f);
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PARAM_DEFINE_FLOAT(INAV_W_POS_FLOW, 10.0f);
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PARAM_DEFINE_FLOAT(INAV_W_POS_FLOW, 0.0f);
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PARAM_DEFINE_FLOAT(INAV_W_ACC_BIAS, 0.0f);
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PARAM_DEFINE_FLOAT(INAV_FLOW_K, 1.0f);
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PARAM_DEFINE_FLOAT(INAV_SONAR_FILT, 0.02f);
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PARAM_DEFINE_FLOAT(INAV_SONAR_ERR, 0.5f);
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@@ -62,6 +63,7 @@ int parameters_init(struct position_estimator_inav_param_handles *h)
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h->w_pos_gps_v = param_find("INAV_W_POS_GPS_V");
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h->w_pos_acc = param_find("INAV_W_POS_ACC");
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h->w_pos_flow = param_find("INAV_W_POS_FLOW");
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h->w_acc_bias = param_find("INAV_W_ACC_BIAS");
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h->flow_k = param_find("INAV_FLOW_K");
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h->sonar_filt = param_find("INAV_SONAR_FILT");
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h->sonar_err = param_find("INAV_SONAR_ERR");
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@@ -79,6 +81,7 @@ int parameters_update(const struct position_estimator_inav_param_handles *h, str
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param_get(h->w_pos_gps_v, &(p->w_pos_gps_v));
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param_get(h->w_pos_acc, &(p->w_pos_acc));
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param_get(h->w_pos_flow, &(p->w_pos_flow));
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param_get(h->w_acc_bias, &(p->w_acc_bias));
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param_get(h->flow_k, &(p->flow_k));
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param_get(h->sonar_filt, &(p->sonar_filt));
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param_get(h->sonar_err, &(p->sonar_err));
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@@ -49,6 +49,7 @@ struct position_estimator_inav_params {
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float w_pos_gps_v;
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float w_pos_acc;
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float w_pos_flow;
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float w_acc_bias;
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float flow_k;
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float sonar_filt;
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float sonar_err;
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@@ -63,6 +64,7 @@ struct position_estimator_inav_param_handles {
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param_t w_pos_gps_v;
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param_t w_pos_acc;
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param_t w_pos_flow;
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param_t w_acc_bias;
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param_t flow_k;
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param_t sonar_filt;
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param_t sonar_err;
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