forked from Archive/PX4-Autopilot
INAV: Removed all references to land detector logic
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@ -246,9 +246,6 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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float baro_offset = 0.0f; // baro offset for reference altitude, initialized on start, then adjusted
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float surface_offset = 0.0f; // ground level offset from reference altitude
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float surface_offset_rate = 0.0f; // surface offset change rate
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//float alt_avg = 0.0f;
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//bool landed = true;
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//hrt_abstime landed_time = 0;
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hrt_abstime accel_timestamp = 0;
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hrt_abstime baro_timestamp = 0;
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@ -1068,39 +1065,6 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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inertial_filter_correct(-y_est[1], dt, y_est, 1, params.w_xy_res_v);
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}
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/*
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// detect land
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alt_avg += (- z_est[0] - alt_avg) * dt / params.land_t;
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float alt_disp2 = - z_est[0] - alt_avg;
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alt_disp2 = alt_disp2 * alt_disp2;
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float land_disp2 = params.land_disp * params.land_disp;
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// get actual thrust output
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float thrust = armed.armed ? actuator.control[3] : 0.0f;
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if (landed) {
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if (alt_disp2 > land_disp2 || thrust > params.land_thr) {
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landed = false;
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landed_time = 0;
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}
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} else {
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if (alt_disp2 < land_disp2 && thrust < params.land_thr) {
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if (landed_time == 0) {
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landed_time = t; // land detected first time
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} else {
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if (t > landed_time + params.land_t * 1000000.0f) {
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landed = true;
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landed_time = 0;
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}
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}
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} else {
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landed_time = 0;
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}
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}
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*/
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if (verbose_mode) {
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/* print updates rate */
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if (t > updates_counter_start + updates_counter_len) {
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@ -1151,7 +1115,6 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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local_pos.vy = y_est[1];
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local_pos.z = z_est[0];
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local_pos.vz = z_est[1];
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local_pos.landed = false;
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local_pos.yaw = att.yaw;
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local_pos.dist_bottom_valid = dist_bottom_valid;
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local_pos.eph = eph;
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