mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-07-09 00:40:36 +08:00
@@ -164,11 +164,6 @@ int do_accel_calibration(int mavlink_fd)
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mavlink_and_console_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
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mavlink_and_console_log_info(mavlink_fd, "You need to put the system on all six sides");
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sleep(3);
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mavlink_and_console_log_info(mavlink_fd, "Follow the instructions on the screen");
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sleep(5);
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struct accel_scale accel_scale = {
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0.0f,
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1.0f,
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@@ -352,7 +347,7 @@ int do_accel_calibration_measurements(int mavlink_fd, float (&accel_offs)[max_se
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(!data_collected[4]) ? "up " : "");
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/* allow user enough time to read the message */
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sleep(3);
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sleep(1);
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int orient = detect_orientation(mavlink_fd, subs);
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@@ -365,7 +360,7 @@ int do_accel_calibration_measurements(int mavlink_fd, float (&accel_offs)[max_se
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/* inform user about already handled side */
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if (data_collected[orient]) {
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mavlink_and_console_log_info(mavlink_fd, "%s side done, rotate to a different side", orientation_strs[orient]);
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sleep(3);
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sleep(1);
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continue;
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}
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@@ -374,7 +369,7 @@ int do_accel_calibration_measurements(int mavlink_fd, float (&accel_offs)[max_se
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read_accelerometer_avg(subs, accel_ref, orient, samples_num);
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mavlink_and_console_log_info(mavlink_fd, "%s side done, rotate to a different side", orientation_strs[orient]);
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usleep(100000);
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mavlink_and_console_log_info(mavlink_fd, "result for %s side: [ %.2f %.2f %.2f ]", orientation_strs[orient],
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mavlink_and_console_log_info(mavlink_fd, "result for %s side: [ %8.4f %8.4f %8.4f ]", orientation_strs[orient],
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(double)accel_ref[0][orient][0],
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(double)accel_ref[0][orient][1],
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(double)accel_ref[0][orient][2]);
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@@ -399,13 +394,6 @@ int do_accel_calibration_measurements(int mavlink_fd, float (&accel_offs)[max_se
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for (unsigned i = 0; i < (*active_sensors); i++) {
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res = calculate_calibration_values(i, accel_ref, accel_T, accel_offs, CONSTANTS_ONE_G);
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/* verbose output on the console */
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printf("accel_T transformation matrix:\n");
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for (unsigned j = 0; j < 3; j++) {
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printf(" %8.4f %8.4f %8.4f\n", (double)accel_T[i][j][0], (double)accel_T[i][j][1], (double)accel_T[i][j][2]);
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}
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printf("\n");
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if (res != OK) {
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mavlink_and_console_log_critical(mavlink_fd, "ERROR: calibration values calculation error");
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break;
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@@ -635,7 +623,6 @@ int read_accelerometer_avg(int (&subs)[max_sens], float (&accel_avg)[max_sens][6
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for (unsigned s = 0; s < max_sens; s++) {
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for (unsigned i = 0; i < 3; i++) {
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accel_avg[s][orient][i] = accel_sum[s][i] / counts[s];
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warnx("input: s:%u, axis: %u, orient: %u cnt: %u -> %8.4f", s, i, orient, counts[s], (double)accel_avg[s][orient][i]);
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}
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}
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@@ -278,7 +278,7 @@ int commander_main(int argc, char *argv[])
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daemon_task = task_spawn_cmd("commander",
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SCHED_DEFAULT,
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SCHED_PRIORITY_MAX - 40,
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3200,
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3400,
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commander_thread_main,
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(argv) ? (char * const *)&argv[2] : (char * const *)NULL);
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@@ -967,19 +967,6 @@ int commander_thread_main(int argc, char *argv[])
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int ret;
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pthread_attr_t commander_low_prio_attr;
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pthread_attr_init(&commander_low_prio_attr);
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pthread_attr_setstacksize(&commander_low_prio_attr, 2000);
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struct sched_param param;
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(void)pthread_attr_getschedparam(&commander_low_prio_attr, ¶m);
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/* low priority */
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param.sched_priority = SCHED_PRIORITY_DEFAULT - 50;
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(void)pthread_attr_setschedparam(&commander_low_prio_attr, ¶m);
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pthread_create(&commander_low_prio_thread, &commander_low_prio_attr, commander_low_prio_loop, NULL);
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pthread_attr_destroy(&commander_low_prio_attr);
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/* Start monitoring loop */
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unsigned counter = 0;
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unsigned stick_off_counter = 0;
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@@ -1144,6 +1131,20 @@ int commander_thread_main(int argc, char *argv[])
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bool main_state_changed = false;
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bool failsafe_old = false;
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/* initialize low priority thread */
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pthread_attr_t commander_low_prio_attr;
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pthread_attr_init(&commander_low_prio_attr);
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pthread_attr_setstacksize(&commander_low_prio_attr, 2100);
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struct sched_param param;
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(void)pthread_attr_getschedparam(&commander_low_prio_attr, ¶m);
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/* low priority */
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param.sched_priority = SCHED_PRIORITY_DEFAULT - 50;
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(void)pthread_attr_setschedparam(&commander_low_prio_attr, ¶m);
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pthread_create(&commander_low_prio_thread, &commander_low_prio_attr, commander_low_prio_loop, NULL);
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pthread_attr_destroy(&commander_low_prio_attr);
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while (!thread_should_exit) {
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if (mavlink_fd < 0 && counter % (1000000 / MAVLINK_OPEN_INTERVAL) == 0) {
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@@ -231,7 +231,7 @@ int led_init()
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/* then try RGB LEDs, this can fail on FMUv1*/
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rgbleds = open(RGBLED0_DEVICE_PATH, 0);
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if (rgbleds == -1) {
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if (rgbleds < 0) {
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warnx("No RGB LED found at " RGBLED0_DEVICE_PATH);
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}
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@@ -240,50 +240,64 @@ int led_init()
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void led_deinit()
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{
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close(leds);
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if (leds >= 0) {
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close(leds);
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}
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if (rgbleds != -1) {
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if (rgbleds >= 0) {
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close(rgbleds);
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}
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}
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int led_toggle(int led)
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{
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if (leds < 0) {
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return leds;
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}
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return ioctl(leds, LED_TOGGLE, led);
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}
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int led_on(int led)
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{
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if (leds < 0) {
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return leds;
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}
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return ioctl(leds, LED_ON, led);
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}
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int led_off(int led)
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{
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if (leds < 0) {
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return leds;
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}
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return ioctl(leds, LED_OFF, led);
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}
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void rgbled_set_color(rgbled_color_t color)
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{
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if (rgbleds != -1) {
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ioctl(rgbleds, RGBLED_SET_COLOR, (unsigned long)color);
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if (rgbleds < 0) {
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return;
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}
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ioctl(rgbleds, RGBLED_SET_COLOR, (unsigned long)color);
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}
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void rgbled_set_mode(rgbled_mode_t mode)
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{
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if (rgbleds != -1) {
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ioctl(rgbleds, RGBLED_SET_MODE, (unsigned long)mode);
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if (rgbleds < 0) {
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return;
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}
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ioctl(rgbleds, RGBLED_SET_MODE, (unsigned long)mode);
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}
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void rgbled_set_pattern(rgbled_pattern_t *pattern)
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{
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if (rgbleds != -1) {
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ioctl(rgbleds, RGBLED_SET_PATTERN, (unsigned long)pattern);
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if (rgbleds < 0) {
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return;
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}
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ioctl(rgbleds, RGBLED_SET_PATTERN, (unsigned long)pattern);
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}
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float battery_remaining_estimate_voltage(float voltage, float discharged, float throttle_normalized)
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@@ -73,16 +73,17 @@ int do_gyro_calibration(int mavlink_fd)
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/* wait for the user to respond */
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sleep(2);
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struct gyro_scale gyro_scale[max_gyros] = { {
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struct gyro_scale gyro_scale_zero = {
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0.0f,
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1.0f,
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0.0f,
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1.0f,
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0.0f,
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1.0f,
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}
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};
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struct gyro_scale gyro_scale[max_gyros];
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int res = OK;
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/* store board ID */
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@@ -97,7 +98,7 @@ int do_gyro_calibration(int mavlink_fd)
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for (unsigned s = 0; s < max_gyros; s++) {
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/* ensure all scale fields are initialized tha same as the first struct */
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(void)memcpy(&gyro_scale[s], &gyro_scale[0], sizeof(gyro_scale[0]));
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(void)memcpy(&gyro_scale[s], &gyro_scale_zero, sizeof(gyro_scale[0]));
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sprintf(str, "%s%u", GYRO_BASE_DEVICE_PATH, s);
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/* reset all offsets to zero and all scales to one */
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@@ -109,7 +110,7 @@ int do_gyro_calibration(int mavlink_fd)
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device_id[s] = ioctl(fd, DEVIOCGDEVICEID, 0);
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res = ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gyro_scale);
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res = ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gyro_scale_zero);
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close(fd);
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if (res != OK) {
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@@ -120,6 +121,8 @@ int do_gyro_calibration(int mavlink_fd)
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unsigned calibration_counter[max_gyros] = { 0 };
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const unsigned calibration_count = 5000;
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struct gyro_report gyro_report_0 = {};
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if (res == OK) {
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/* determine gyro mean values */
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unsigned poll_errcount = 0;
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@@ -140,7 +143,7 @@ int do_gyro_calibration(int mavlink_fd)
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while (calibration_counter[0] < calibration_count) {
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/* wait blocking for new data */
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int poll_ret = poll(fds, 1, 1000);
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int poll_ret = poll(&fds[0], max_gyros, 1000);
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if (poll_ret > 0) {
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@@ -150,6 +153,11 @@ int do_gyro_calibration(int mavlink_fd)
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if (changed) {
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orb_copy(ORB_ID(sensor_gyro), sub_sensor_gyro[s], &gyro_report);
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if (s == 0) {
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orb_copy(ORB_ID(sensor_gyro), sub_sensor_gyro[s], &gyro_report_0);
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}
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gyro_scale[s].x_offset += gyro_report.x;
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gyro_scale[s].y_offset += gyro_report.y;
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gyro_scale[s].z_offset += gyro_report.z;
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@@ -183,8 +191,20 @@ int do_gyro_calibration(int mavlink_fd)
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if (res == OK) {
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/* check offsets */
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if (!isfinite(gyro_scale[0].x_offset) || !isfinite(gyro_scale[0].y_offset) || !isfinite(gyro_scale[0].z_offset)) {
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mavlink_log_critical(mavlink_fd, "ERROR: offset is NaN");
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float xdiff = gyro_report_0.x - gyro_scale[0].x_offset;
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float ydiff = gyro_report_0.y - gyro_scale[0].y_offset;
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float zdiff = gyro_report_0.z - gyro_scale[0].z_offset;
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/* maximum allowable calibration error in radians */
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const float maxoff = 0.01f;
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if (!isfinite(gyro_scale[0].x_offset) ||
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!isfinite(gyro_scale[0].y_offset) ||
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!isfinite(gyro_scale[0].z_offset) ||
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fabsf(xdiff) > maxoff ||
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fabsf(ydiff) > maxoff ||
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fabsf(zdiff) > maxoff) {
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mavlink_log_critical(mavlink_fd, "ERROR: Calibration failed");
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res = ERROR;
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}
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}
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@@ -214,6 +234,7 @@ int do_gyro_calibration(int mavlink_fd)
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int fd = open(str, 0);
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if (fd < 0) {
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failed = true;
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continue;
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}
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@@ -226,7 +247,7 @@ int do_gyro_calibration(int mavlink_fd)
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}
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if (failed) {
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mavlink_log_critical(mavlink_fd, "ERROR: failed to set offset params");
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mavlink_and_console_log_critical(mavlink_fd, "ERROR: failed to set offset params");
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res = ERROR;
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}
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}
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@@ -164,9 +164,9 @@ int calibrate_instance(int mavlink_fd, unsigned s, unsigned device_id)
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const unsigned int calibration_maxcount = 240;
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unsigned int calibration_counter;
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float *x = NULL;
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float *y = NULL;
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float *z = NULL;
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float *x = new float[calibration_maxcount];
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float *y = new float[calibration_maxcount];
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float *z = new float[calibration_maxcount];
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char str[30];
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int res = OK;
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@@ -174,24 +174,20 @@ int calibrate_instance(int mavlink_fd, unsigned s, unsigned device_id)
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/* allocate memory */
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mavlink_and_console_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 20);
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x = reinterpret_cast<float *>(malloc(sizeof(float) * calibration_maxcount));
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y = reinterpret_cast<float *>(malloc(sizeof(float) * calibration_maxcount));
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z = reinterpret_cast<float *>(malloc(sizeof(float) * calibration_maxcount));
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if (x == NULL || y == NULL || z == NULL) {
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if (x == nullptr || y == nullptr || z == nullptr) {
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mavlink_and_console_log_critical(mavlink_fd, "ERROR: out of memory");
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/* clean up */
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if (x != NULL) {
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free(x);
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if (x != nullptr) {
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delete x;
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}
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if (y != NULL) {
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free(y);
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if (y != nullptr) {
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delete y;
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}
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if (z != NULL) {
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free(z);
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if (z != nullptr) {
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delete z;
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}
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res = ERROR;
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@@ -274,16 +270,16 @@ int calibrate_instance(int mavlink_fd, unsigned s, unsigned device_id)
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}
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}
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if (x != NULL) {
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free(x);
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if (x != nullptr) {
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delete x;
|
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}
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|
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if (y != NULL) {
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free(y);
|
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if (y != nullptr) {
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delete y;
|
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}
|
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|
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if (z != NULL) {
|
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free(z);
|
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if (z != nullptr) {
|
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delete z;
|
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}
|
||||
|
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if (res == OK) {
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|
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@@ -52,5 +52,5 @@ MODULE_STACKSIZE = 5000
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|
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MAXOPTIMIZATION = -Os
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|
||||
EXTRACXXFLAGS = -Wframe-larger-than=2000
|
||||
EXTRACXXFLAGS = -Wframe-larger-than=2200
|
||||
|
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|
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@@ -784,14 +784,14 @@ void AttitudePositionEstimatorEKF::publishAttitude()
|
||||
_att.pitch = euler(1);
|
||||
_att.yaw = euler(2);
|
||||
|
||||
_att.rollspeed = _ekf->angRate.x - _ekf->states[10] / _ekf->dtIMU;
|
||||
_att.pitchspeed = _ekf->angRate.y - _ekf->states[11] / _ekf->dtIMU;
|
||||
_att.yawspeed = _ekf->angRate.z - _ekf->states[12] / _ekf->dtIMU;
|
||||
_att.rollspeed = _ekf->angRate.x - _ekf->states[10] / _ekf->dtIMUfilt;
|
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_att.pitchspeed = _ekf->angRate.y - _ekf->states[11] / _ekf->dtIMUfilt;
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||||
_att.yawspeed = _ekf->angRate.z - _ekf->states[12] / _ekf->dtIMUfilt;
|
||||
|
||||
// gyro offsets
|
||||
_att.rate_offsets[0] = _ekf->states[10] / _ekf->dtIMU;
|
||||
_att.rate_offsets[1] = _ekf->states[11] / _ekf->dtIMU;
|
||||
_att.rate_offsets[2] = _ekf->states[12] / _ekf->dtIMU;
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_att.rate_offsets[0] = _ekf->states[10] / _ekf->dtIMUfilt;
|
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_att.rate_offsets[1] = _ekf->states[11] / _ekf->dtIMUfilt;
|
||||
_att.rate_offsets[2] = _ekf->states[12] / _ekf->dtIMUfilt;
|
||||
|
||||
/* lazily publish the attitude only once available */
|
||||
if (_att_pub > 0) {
|
||||
@@ -1069,7 +1069,7 @@ void AttitudePositionEstimatorEKF::print_status()
|
||||
// 16-18: Earth Magnetic Field Vector - gauss (North, East, Down)
|
||||
// 19-21: Body Magnetic Field Vector - gauss (X,Y,Z)
|
||||
|
||||
printf("dtIMU: %8.6f IMUmsec: %d\n", (double)_ekf->dtIMU, (int)IMUmsec);
|
||||
printf("dtIMU: %8.6f filt: %8.6f IMUmsec: %d\n", (double)_ekf->dtIMU, (double)_ekf->dtIMUfilt, (int)IMUmsec);
|
||||
printf("baro alt: %8.4f GPS alt: %8.4f\n", (double)_baro.altitude, (double)(_gps.alt / 1e3f));
|
||||
printf("baro ref offset: %8.4f baro GPS offset: %8.4f\n", (double)_baro_ref_offset,
|
||||
(double)_baro_gps_offset);
|
||||
|
||||
@@ -218,7 +218,7 @@ PARAM_DEFINE_FLOAT(PE_ACC_PNOISE, 0.25f);
|
||||
* @max 0.00001
|
||||
* @group Position Estimator
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(PE_GBIAS_PNOISE, 1e-07f);
|
||||
PARAM_DEFINE_FLOAT(PE_GBIAS_PNOISE, 1e-06f);
|
||||
|
||||
/**
|
||||
* Accelerometer bias estimate process noise
|
||||
@@ -230,7 +230,7 @@ PARAM_DEFINE_FLOAT(PE_GBIAS_PNOISE, 1e-07f);
|
||||
* @max 0.001
|
||||
* @group Position Estimator
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(PE_ABIAS_PNOISE, 0.00005f);
|
||||
PARAM_DEFINE_FLOAT(PE_ABIAS_PNOISE, 0.0002f);
|
||||
|
||||
/**
|
||||
* Magnetometer earth frame offsets process noise
|
||||
|
||||
@@ -210,10 +210,10 @@ void AttPosEKF::InitialiseParameters()
|
||||
|
||||
yawVarScale = 1.0f;
|
||||
windVelSigma = 0.1f;
|
||||
dAngBiasSigma = 5.0e-7f;
|
||||
dVelBiasSigma = 1e-4f;
|
||||
magEarthSigma = 3.0e-4f;
|
||||
magBodySigma = 3.0e-4f;
|
||||
dAngBiasSigma = 1.0e-6;
|
||||
dVelBiasSigma = 0.0002f;
|
||||
magEarthSigma = 0.0003f;
|
||||
magBodySigma = 0.0003f;
|
||||
|
||||
vneSigma = 0.2f;
|
||||
vdSigma = 0.3f;
|
||||
@@ -414,9 +414,10 @@ void AttPosEKF::CovariancePrediction(float dt)
|
||||
// calculate covariance prediction process noise
|
||||
for (uint8_t i= 0; i<4; i++) processNoise[i] = 1.0e-9f;
|
||||
for (uint8_t i= 4; i<10; i++) processNoise[i] = 1.0e-9f;
|
||||
for (uint8_t i=10; i<=12; i++) processNoise[i] = dt * dAngBiasSigma;
|
||||
// scale gyro bias noise when on ground to allow for faster bias estimation
|
||||
for (uint8_t i=10; i<=12; i++) processNoise[i] = dt * dAngBiasSigma;
|
||||
float gyroBiasScale = (_onGround) ? 2.0f : 1.0f;
|
||||
|
||||
for (uint8_t i=10; i<=12; i++) processNoise[i] = dt * dAngBiasSigma * gyroBiasScale;
|
||||
processNoise[13] = dVelBiasSigma;
|
||||
if (!inhibitWindStates) {
|
||||
for (uint8_t i=14; i<=15; i++) processNoise[i] = dt * windVelSigma;
|
||||
@@ -2706,6 +2707,11 @@ void AttPosEKF::ConstrainStates()
|
||||
// 16-18: Earth Magnetic Field Vector - gauss (North, East, Down)
|
||||
// 19-21: Body Magnetic Field Vector - gauss (X,Y,Z)
|
||||
|
||||
// Constrain dtIMUfilt
|
||||
if (!isfinite(dtIMUfilt) || (fabsf(dtIMU - dtIMUfilt) > 0.01f)) {
|
||||
dtIMUfilt = dtIMU;
|
||||
}
|
||||
|
||||
// Constrain quaternion
|
||||
for (size_t i = 0; i <= 3; i++) {
|
||||
states[i] = ConstrainFloat(states[i], -1.0f, 1.0f);
|
||||
@@ -2727,11 +2733,11 @@ void AttPosEKF::ConstrainStates()
|
||||
|
||||
// Angle bias limit - set to 8 degrees / sec
|
||||
for (size_t i = 10; i <= 12; i++) {
|
||||
states[i] = ConstrainFloat(states[i], -0.12f * dtIMU, 0.12f * dtIMU);
|
||||
states[i] = ConstrainFloat(states[i], -0.16f * dtIMUfilt, 0.16f * dtIMUfilt);
|
||||
}
|
||||
|
||||
// Constrain delta velocity bias
|
||||
states[13] = ConstrainFloat(states[13], -1.0f * dtIMU, 1.0f * dtIMU);
|
||||
states[13] = ConstrainFloat(states[13], -1.0f * dtIMUfilt, 1.0f * dtIMUfilt);
|
||||
|
||||
// Wind velocity limits - assume 120 m/s max velocity
|
||||
for (size_t i = 14; i <= 15; i++) {
|
||||
@@ -2795,8 +2801,8 @@ bool AttPosEKF::GyroOffsetsDiverged()
|
||||
|
||||
// Protect against division by zero
|
||||
if (delta_len > 0.0f) {
|
||||
float cov_mag = ConstrainFloat((P[10][10] + P[11][11] + P[12][12]), 1e-12f, 1e-8f);
|
||||
delta_len_scaled = (5e-7 / (double)cov_mag) * (double)delta_len / (double)dtIMU;
|
||||
float cov_mag = ConstrainFloat((P[10][10] + P[11][11] + P[12][12]), 1e-12f, 1e-2f);
|
||||
delta_len_scaled = (5e-7 / (double)cov_mag) * (double)delta_len / (double)dtIMUfilt;
|
||||
}
|
||||
|
||||
bool diverged = (delta_len_scaled > 1.0f);
|
||||
|
||||
Reference in New Issue
Block a user