/**************************************************************************** * * Copyright (c) 2013-2016 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ /** * @file accelerometer_calibration.cpp * * Implementation of accelerometer calibration. * * Transform acceleration vector to true orientation, scale and offset * * ===== Model ===== * accel_corr = accel_T * (accel_raw - accel_offs) * * accel_corr[3] - fully corrected acceleration vector in body frame * accel_T[3][3] - accelerometers transform matrix, rotation and scaling transform * accel_raw[3] - raw acceleration vector * accel_offs[3] - acceleration offset vector * * ===== Calibration ===== * * Reference vectors * accel_corr_ref[6][3] = [ g 0 0 ] // nose up * | -g 0 0 | // nose down * | 0 g 0 | // left side down * | 0 -g 0 | // right side down * | 0 0 g | // on back * [ 0 0 -g ] // level * accel_raw_ref[6][3] * * accel_corr_ref[i] = accel_T * (accel_raw_ref[i] - accel_offs), i = 0...5 * * 6 reference vectors * 3 axes = 18 equations * 9 (accel_T) + 3 (accel_offs) = 12 unknown constants * * Find accel_offs * * accel_offs[i] = (accel_raw_ref[i*2][i] + accel_raw_ref[i*2+1][i]) / 2 * * Find accel_T * * 9 unknown constants * need 9 equations -> use 3 of 6 measurements -> 3 * 3 = 9 equations * * accel_corr_ref[i*2] = accel_T * (accel_raw_ref[i*2] - accel_offs), i = 0...2 * * Solve separate system for each row of accel_T: * * accel_corr_ref[j*2][i] = accel_T[i] * (accel_raw_ref[j*2] - accel_offs), j = 0...2 * * A * x = b * * x = [ accel_T[0][i] ] * | accel_T[1][i] | * [ accel_T[2][i] ] * * b = [ accel_corr_ref[0][i] ] // One measurement per side is enough * | accel_corr_ref[2][i] | * [ accel_corr_ref[4][i] ] * * a[i][j] = accel_raw_ref[i][j] - accel_offs[j], i = 0;2;4, j = 0...2 * * Matrix A is common for all three systems: * A = [ a[0][0] a[0][1] a[0][2] ] * | a[2][0] a[2][1] a[2][2] | * [ a[4][0] a[4][1] a[4][2] ] * * x = A^-1 * b * * accel_T = A^-1 * g * g = 9.80665 * * ===== Rotation ===== * * Calibrating using model: * accel_corr = accel_T_r * (rot * accel_raw - accel_offs_r) * * Actual correction: * accel_corr = rot * accel_T * (accel_raw - accel_offs) * * Known: accel_T_r, accel_offs_r, rot * Unknown: accel_T, accel_offs * * Solution: * accel_T_r * (rot * accel_raw - accel_offs_r) = rot * accel_T * (accel_raw - accel_offs) * rot^-1 * accel_T_r * (rot * accel_raw - accel_offs_r) = accel_T * (accel_raw - accel_offs) * rot^-1 * accel_T_r * rot * accel_raw - rot^-1 * accel_T_r * accel_offs_r = accel_T * accel_raw - accel_T * accel_offs) * => accel_T = rot^-1 * accel_T_r * rot * => accel_offs = rot^-1 * accel_offs_r * * @author Anton Babushkin */ // FIXME: Can some of these headers move out with detect_ move? #include "accelerometer_calibration.h" #include "calibration_messages.h" #include "calibration_routines.h" #include "commander_helper.h" #include #include #include #include #include #include //#include #include #include #include #include #include #include #include #include #include #include #include #include #include /* oddly, ERROR is not defined for c++ */ #ifdef ERROR # undef ERROR #endif static const int ERROR = -1; static const char *sensor_name = "accel"; static int32_t device_id[max_accel_sens]; static int device_prio_max = 0; static int32_t device_id_primary = 0; calibrate_return do_accel_calibration_measurements(orb_advert_t *mavlink_log_pub, float (&accel_offs)[max_accel_sens][3], float (&accel_T)[max_accel_sens][3][3], unsigned *active_sensors); calibrate_return read_accelerometer_avg(int (&subs)[max_accel_sens], float (&accel_avg)[max_accel_sens][detect_orientation_side_count][3], unsigned orient, unsigned samples_num); int mat_invert3(float src[3][3], float dst[3][3]); calibrate_return calculate_calibration_values(unsigned sensor, float (&accel_ref)[max_accel_sens][detect_orientation_side_count][3], float (&accel_T)[max_accel_sens][3][3], float (&accel_offs)[max_accel_sens][3], float g); /// Data passed to calibration worker routine typedef struct { orb_advert_t *mavlink_log_pub; unsigned done_count; int subs[max_accel_sens]; float accel_ref[max_accel_sens][detect_orientation_side_count][3]; } accel_worker_data_t; int do_accel_calibration(orb_advert_t *mavlink_log_pub) { #if !defined(__PX4_QURT) && !defined(__PX4_POSIX_EAGLE) && !defined(__PX4_POSIX_RPI) && !defined(__PX4_POSIX_BEBOP) int fd; #endif calibration_log_info(mavlink_log_pub, CAL_QGC_STARTED_MSG, sensor_name); struct accel_calibration_s accel_scale; accel_scale.x_offset = 0.0f; accel_scale.x_scale = 1.0f; accel_scale.y_offset = 0.0f; accel_scale.y_scale = 1.0f; accel_scale.z_offset = 0.0f; accel_scale.z_scale = 1.0f; int res = OK; char str[30]; /* reset all sensors */ for (unsigned s = 0; s < max_accel_sens; s++) { #if !defined(__PX4_QURT) && !defined(__PX4_POSIX_EAGLE) && !defined(__PX4_POSIX_RPI) && !defined(__PX4_POSIX_BEBOP) sprintf(str, "%s%u", ACCEL_BASE_DEVICE_PATH, s); /* reset all offsets to zero and all scales to one */ fd = px4_open(str, 0); if (fd < 0) { continue; } device_id[s] = px4_ioctl(fd, DEVIOCGDEVICEID, 0); res = px4_ioctl(fd, ACCELIOCSSCALE, (long unsigned int)&accel_scale); px4_close(fd); if (res != OK) { calibration_log_critical(mavlink_log_pub, CAL_ERROR_RESET_CAL_MSG, s); } #else (void)sprintf(str, "CAL_ACC%u_XOFF", s); res = param_set(param_find(str), &accel_scale.x_offset); if (res != OK) { PX4_ERR("unable to reset %s", str); } (void)sprintf(str, "CAL_ACC%u_YOFF", s); res = param_set(param_find(str), &accel_scale.y_offset); if (res != OK) { PX4_ERR("unable to reset %s", str); } (void)sprintf(str, "CAL_ACC%u_ZOFF", s); res = param_set(param_find(str), &accel_scale.z_offset); if (res != OK) { PX4_ERR("unable to reset %s", str); } (void)sprintf(str, "CAL_ACC%u_XSCALE", s); res = param_set(param_find(str), &accel_scale.x_scale); if (res != OK) { PX4_ERR("unable to reset %s", str); } (void)sprintf(str, "CAL_ACC%u_YSCALE", s); res = param_set(param_find(str), &accel_scale.y_scale); if (res != OK) { PX4_ERR("unable to reset %s", str); } (void)sprintf(str, "CAL_ACC%u_ZSCALE", s); res = param_set(param_find(str), &accel_scale.z_scale); if (res != OK) { PX4_ERR("unable to reset %s", str); } #endif } float accel_offs[max_accel_sens][3]; float accel_T[max_accel_sens][3][3]; unsigned active_sensors; /* measure and calculate offsets & scales */ if (res == OK) { calibrate_return cal_return = do_accel_calibration_measurements(mavlink_log_pub, accel_offs, accel_T, &active_sensors); if (cal_return == calibrate_return_cancelled) { // Cancel message already displayed, nothing left to do return ERROR; } else if (cal_return == calibrate_return_ok) { res = OK; } else { res = ERROR; } } if (res != OK) { if (active_sensors == 0) { calibration_log_critical(mavlink_log_pub, CAL_ERROR_SENSOR_MSG); } return ERROR; } /* measurements completed successfully, rotate calibration values */ param_t board_rotation_h = param_find("SENS_BOARD_ROT"); int32_t board_rotation_int; param_get(board_rotation_h, &(board_rotation_int)); enum Rotation board_rotation_id = (enum Rotation)board_rotation_int; math::Matrix<3, 3> board_rotation; get_rot_matrix(board_rotation_id, &board_rotation); math::Matrix<3, 3> board_rotation_t = board_rotation.transposed(); for (unsigned i = 0; i < active_sensors; i++) { /* handle individual sensors, one by one */ math::Vector<3> accel_offs_vec(accel_offs[i]); math::Vector<3> accel_offs_rotated = board_rotation_t * accel_offs_vec; math::Matrix<3, 3> accel_T_mat(accel_T[i]); math::Matrix<3, 3> accel_T_rotated = board_rotation_t * accel_T_mat * board_rotation; accel_scale.x_offset = accel_offs_rotated(0); accel_scale.x_scale = accel_T_rotated(0, 0); accel_scale.y_offset = accel_offs_rotated(1); accel_scale.y_scale = accel_T_rotated(1, 1); accel_scale.z_offset = accel_offs_rotated(2); accel_scale.z_scale = accel_T_rotated(2, 2); bool failed = false; failed = failed || (OK != param_set_no_notification(param_find("CAL_ACC_PRIME"), &(device_id_primary))); PX4_DEBUG("found offset %d: x: %.6f, y: %.6f, z: %.6f", i, (double)accel_scale.x_offset, (double)accel_scale.y_offset, (double)accel_scale.z_offset); PX4_DEBUG("found scale %d: x: %.6f, y: %.6f, z: %.6f", i, (double)accel_scale.x_scale, (double)accel_scale.y_scale, (double)accel_scale.z_scale); /* set parameters */ (void)sprintf(str, "CAL_ACC%u_XOFF", i); failed |= (OK != param_set_no_notification(param_find(str), &(accel_scale.x_offset))); (void)sprintf(str, "CAL_ACC%u_YOFF", i); failed |= (OK != param_set_no_notification(param_find(str), &(accel_scale.y_offset))); (void)sprintf(str, "CAL_ACC%u_ZOFF", i); failed |= (OK != param_set_no_notification(param_find(str), &(accel_scale.z_offset))); (void)sprintf(str, "CAL_ACC%u_XSCALE", i); failed |= (OK != param_set_no_notification(param_find(str), &(accel_scale.x_scale))); (void)sprintf(str, "CAL_ACC%u_YSCALE", i); failed |= (OK != param_set_no_notification(param_find(str), &(accel_scale.y_scale))); (void)sprintf(str, "CAL_ACC%u_ZSCALE", i); failed |= (OK != param_set_no_notification(param_find(str), &(accel_scale.z_scale))); (void)sprintf(str, "CAL_ACC%u_ID", i); failed |= (OK != param_set_no_notification(param_find(str), &(device_id[i]))); if (failed) { calibration_log_critical(mavlink_log_pub, CAL_ERROR_SET_PARAMS_MSG, i); return ERROR; } #if !defined(__PX4_QURT) && !defined(__PX4_POSIX_EAGLE) && !defined(__PX4_POSIX_RPI) && !defined(__PX4_POSIX_BEBOP) sprintf(str, "%s%u", ACCEL_BASE_DEVICE_PATH, i); fd = px4_open(str, 0); if (fd < 0) { calibration_log_critical(mavlink_log_pub, CAL_QGC_FAILED_MSG, "sensor does not exist"); res = ERROR; } else { res = px4_ioctl(fd, ACCELIOCSSCALE, (long unsigned int)&accel_scale); px4_close(fd); } if (res != OK) { calibration_log_critical(mavlink_log_pub, CAL_ERROR_APPLY_CAL_MSG, i); } #endif } if (res == OK) { /* auto-save to EEPROM */ res = param_save_default(); if (res != OK) { calibration_log_critical(mavlink_log_pub, CAL_ERROR_SAVE_PARAMS_MSG); } /* if there is a any preflight-check system response, let the barrage of messages through */ usleep(200000); calibration_log_info(mavlink_log_pub, CAL_QGC_DONE_MSG, sensor_name); } else { calibration_log_critical(mavlink_log_pub, CAL_QGC_FAILED_MSG, sensor_name); } /* give this message enough time to propagate */ usleep(600000); return res; } static calibrate_return accel_calibration_worker(detect_orientation_return orientation, int cancel_sub, void* data) { const unsigned samples_num = 750; accel_worker_data_t* worker_data = (accel_worker_data_t*)(data); calibration_log_info(worker_data->mavlink_log_pub, "[cal] Hold still, measuring %s side", detect_orientation_str(orientation)); read_accelerometer_avg(worker_data->subs, worker_data->accel_ref, orientation, samples_num); calibration_log_info(worker_data->mavlink_log_pub, "[cal] %s side result: [%8.4f %8.4f %8.4f]", detect_orientation_str(orientation), (double)worker_data->accel_ref[0][orientation][0], (double)worker_data->accel_ref[0][orientation][1], (double)worker_data->accel_ref[0][orientation][2]); worker_data->done_count++; calibration_log_info(worker_data->mavlink_log_pub, CAL_QGC_PROGRESS_MSG, 17 * worker_data->done_count); return calibrate_return_ok; } calibrate_return do_accel_calibration_measurements(orb_advert_t *mavlink_log_pub, float (&accel_offs)[max_accel_sens][3], float (&accel_T)[max_accel_sens][3][3], unsigned *active_sensors) { calibrate_return result = calibrate_return_ok; *active_sensors = 0; accel_worker_data_t worker_data; worker_data.mavlink_log_pub = mavlink_log_pub; worker_data.done_count = 0; bool data_collected[detect_orientation_side_count] = { false, false, false, false, false, false }; // Initialize subs to error condition so we know which ones are open and which are not for (size_t i=0; i device_prio_max) { device_prio_max = prio; device_id_primary = device_id[i]; } } else { calibration_log_critical(mavlink_log_pub, "[cal] Accel #%u no device id, abort", i); result = calibrate_return_error; break; } } if (result == calibrate_return_ok) { int cancel_sub = calibrate_cancel_subscribe(); result = calibrate_from_orientation(mavlink_log_pub, cancel_sub, data_collected, accel_calibration_worker, &worker_data, false /* normal still */); calibrate_cancel_unsubscribe(cancel_sub); } /* close all subscriptions */ for (unsigned i = 0; i < max_accel_sens; i++) { if (worker_data.subs[i] >= 0) { /* figure out which sensors were active */ struct accel_report arp = {}; (void)orb_copy(ORB_ID(sensor_accel), worker_data.subs[i], &arp); if (arp.timestamp != 0 && timestamps[i] != arp.timestamp) { (*active_sensors)++; } px4_close(worker_data.subs[i]); } } if (result == calibrate_return_ok) { /* calculate offsets and transform matrix */ for (unsigned i = 0; i < (*active_sensors); i++) { result = calculate_calibration_values(i, worker_data.accel_ref, accel_T, accel_offs, CONSTANTS_ONE_G); if (result != calibrate_return_ok) { calibration_log_critical(mavlink_log_pub, "[cal] ERROR: calibration calculation error"); break; } } } return result; } /* * Read specified number of accelerometer samples, calculate average and dispersion. */ calibrate_return read_accelerometer_avg(int (&subs)[max_accel_sens], float (&accel_avg)[max_accel_sens][detect_orientation_side_count][3], unsigned orient, unsigned samples_num) { /* get total sensor board rotation matrix */ param_t board_rotation_h = param_find("SENS_BOARD_ROT"); param_t board_offset_x = param_find("SENS_BOARD_X_OFF"); param_t board_offset_y = param_find("SENS_BOARD_Y_OFF"); param_t board_offset_z = param_find("SENS_BOARD_Z_OFF"); float board_offset[3]; param_get(board_offset_x, &board_offset[0]); param_get(board_offset_y, &board_offset[1]); param_get(board_offset_z, &board_offset[2]); math::Matrix<3, 3> board_rotation_offset; board_rotation_offset.from_euler(M_DEG_TO_RAD_F * board_offset[0], M_DEG_TO_RAD_F * board_offset[1], M_DEG_TO_RAD_F * board_offset[2]); int32_t board_rotation_int; param_get(board_rotation_h, &(board_rotation_int)); enum Rotation board_rotation_id = (enum Rotation)board_rotation_int; math::Matrix<3, 3> board_rotation; get_rot_matrix(board_rotation_id, &board_rotation); /* combine board rotation with offset rotation */ board_rotation = board_rotation_offset * board_rotation; px4_pollfd_struct_t fds[max_accel_sens]; for (unsigned i = 0; i < max_accel_sens; i++) { fds[i].fd = subs[i]; fds[i].events = POLLIN; } unsigned counts[max_accel_sens] = { 0 }; float accel_sum[max_accel_sens][3]; memset(accel_sum, 0, sizeof(accel_sum)); unsigned errcount = 0; /* use the first sensor to pace the readout, but do per-sensor counts */ while (counts[0] < samples_num) { int poll_ret = px4_poll(&fds[0], max_accel_sens, 1000); if (poll_ret > 0) { for (unsigned s = 0; s < max_accel_sens; s++) { bool changed; orb_check(subs[s], &changed); if (changed) { struct accel_report arp; orb_copy(ORB_ID(sensor_accel), subs[s], &arp); accel_sum[s][0] += arp.x; accel_sum[s][1] += arp.y; accel_sum[s][2] += arp.z; counts[s]++; } } } else { errcount++; continue; } if (errcount > samples_num / 10) { return calibrate_return_error; } } // rotate sensor measurements from body frame into sensor frame using board rotation matrix for (unsigned i = 0; i < max_accel_sens; i++) { math::Vector<3> accel_sum_vec(&accel_sum[i][0]); accel_sum_vec = board_rotation * accel_sum_vec; memcpy(&accel_sum[i][0], &accel_sum_vec.data[0], sizeof(accel_sum[i])); } for (unsigned s = 0; s < max_accel_sens; s++) { for (unsigned i = 0; i < 3; i++) { accel_avg[s][orient][i] = accel_sum[s][i] / counts[s]; } } return calibrate_return_ok; } int mat_invert3(float src[3][3], float dst[3][3]) { float det = src[0][0] * (src[1][1] * src[2][2] - src[1][2] * src[2][1]) - src[0][1] * (src[1][0] * src[2][2] - src[1][2] * src[2][0]) + src[0][2] * (src[1][0] * src[2][1] - src[1][1] * src[2][0]); if (fabsf(det) < FLT_EPSILON) { return ERROR; // Singular matrix } dst[0][0] = (src[1][1] * src[2][2] - src[1][2] * src[2][1]) / det; dst[1][0] = (src[1][2] * src[2][0] - src[1][0] * src[2][2]) / det; dst[2][0] = (src[1][0] * src[2][1] - src[1][1] * src[2][0]) / det; dst[0][1] = (src[0][2] * src[2][1] - src[0][1] * src[2][2]) / det; dst[1][1] = (src[0][0] * src[2][2] - src[0][2] * src[2][0]) / det; dst[2][1] = (src[0][1] * src[2][0] - src[0][0] * src[2][1]) / det; dst[0][2] = (src[0][1] * src[1][2] - src[0][2] * src[1][1]) / det; dst[1][2] = (src[0][2] * src[1][0] - src[0][0] * src[1][2]) / det; dst[2][2] = (src[0][0] * src[1][1] - src[0][1] * src[1][0]) / det; return OK; } calibrate_return calculate_calibration_values(unsigned sensor, float (&accel_ref)[max_accel_sens][detect_orientation_side_count][3], float (&accel_T)[max_accel_sens][3][3], float (&accel_offs)[max_accel_sens][3], float g) { /* calculate offsets */ for (unsigned i = 0; i < 3; i++) { accel_offs[sensor][i] = (accel_ref[sensor][i * 2][i] + accel_ref[sensor][i * 2 + 1][i]) / 2; } /* fill matrix A for linear equations system*/ float mat_A[3][3]; memset(mat_A, 0, sizeof(mat_A)); for (unsigned i = 0; i < 3; i++) { for (unsigned j = 0; j < 3; j++) { float a = accel_ref[sensor][i * 2][j] - accel_offs[sensor][j]; mat_A[i][j] = a; } } /* calculate inverse matrix for A */ float mat_A_inv[3][3]; if (mat_invert3(mat_A, mat_A_inv) != OK) { return calibrate_return_error; } /* copy results to accel_T */ for (unsigned i = 0; i < 3; i++) { for (unsigned j = 0; j < 3; j++) { /* simplify matrices mult because b has only one non-zero element == g at index i */ accel_T[sensor][j][i] = mat_A_inv[j][i] * g; } } return calibrate_return_ok; } int do_level_calibration(orb_advert_t *mavlink_log_pub) { const unsigned cal_time = 5; const unsigned cal_hz = 100; unsigned settle_time = 30; bool success = false; int att_sub = orb_subscribe(ORB_ID(vehicle_attitude)); struct vehicle_attitude_s att; memset(&att, 0, sizeof(att)); calibration_log_info(mavlink_log_pub, CAL_QGC_STARTED_MSG, "level"); param_t roll_offset_handle = param_find("SENS_BOARD_X_OFF"); param_t pitch_offset_handle = param_find("SENS_BOARD_Y_OFF"); param_t board_rot_handle = param_find("SENS_BOARD_ROT"); // save old values if calibration fails float roll_offset_current; float pitch_offset_current; int32_t board_rot_current = 0; param_get(roll_offset_handle, &roll_offset_current); param_get(pitch_offset_handle, &pitch_offset_current); param_get(board_rot_handle, &board_rot_current); // give attitude some time to settle if there have been changes to the board rotation parameters if (board_rot_current == 0 && fabsf(roll_offset_current) < FLT_EPSILON && fabsf(pitch_offset_current) < FLT_EPSILON ) { settle_time = 0; } float zero = 0.0f; param_set(roll_offset_handle, &zero); param_set(pitch_offset_handle, &zero); px4_pollfd_struct_t fds[1]; fds[0].fd = att_sub; fds[0].events = POLLIN; float roll_mean = 0.0f; float pitch_mean = 0.0f; unsigned counter = 0; // sleep for some time hrt_abstime start = hrt_absolute_time(); while(hrt_elapsed_time(&start) < settle_time * 1000000) { calibration_log_info(mavlink_log_pub, CAL_QGC_PROGRESS_MSG, (int)(90*hrt_elapsed_time(&start)/1e6f/(float)settle_time)); sleep(settle_time / 10); } start = hrt_absolute_time(); // average attitude for 5 seconds while(hrt_elapsed_time(&start) < cal_time * 1000000) { int pollret = px4_poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100); if (pollret <= 0) { // attitude estimator is not running calibration_log_critical(mavlink_log_pub, "attitude estimator not running - check system boot"); calibration_log_critical(mavlink_log_pub, CAL_QGC_FAILED_MSG, "level"); goto out; } orb_copy(ORB_ID(vehicle_attitude), att_sub, &att); roll_mean += att.roll; pitch_mean += att.pitch; counter++; } calibration_log_info(mavlink_log_pub, CAL_QGC_PROGRESS_MSG, 100); if (counter > (cal_time * cal_hz / 2 )) { roll_mean /= counter; pitch_mean /= counter; } else { calibration_log_info(mavlink_log_pub, "not enough measurements taken"); success = false; goto out; } if (fabsf(roll_mean) > 0.8f ) { calibration_log_critical(mavlink_log_pub, "excess roll angle"); } else if (fabsf(pitch_mean) > 0.8f ) { calibration_log_critical(mavlink_log_pub, "excess pitch angle"); } else { roll_mean *= (float)M_RAD_TO_DEG; pitch_mean *= (float)M_RAD_TO_DEG; param_set(roll_offset_handle, &roll_mean); param_set(pitch_offset_handle, &pitch_mean); success = true; } out: if (success) { calibration_log_info(mavlink_log_pub, CAL_QGC_DONE_MSG, "level"); return 0; } else { // set old parameters param_set(roll_offset_handle, &roll_offset_current); param_set(pitch_offset_handle, &pitch_offset_current); calibration_log_critical(mavlink_log_pub, CAL_QGC_FAILED_MSG, "level"); return 1; } }