forked from Archive/PX4-Autopilot
Make instructions in commander more obvious for airspeed calibration
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@ -180,15 +180,16 @@ int do_airspeed_calibration(int mavlink_fd)
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return ERROR;
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}
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mavlink_log_critical(mavlink_fd, "Stored offset of %d Pa", (int)diff_pres_offset);
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mavlink_log_critical(mavlink_fd, "Offset of %d Pa, create airflow now!", (int)diff_pres_offset);
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/* wait 500 ms to ensure parameter propagated through the system */
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usleep(500 * 1000);
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calibration_counter = 0;
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const int maxcount = 3000;
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/* just take a few samples and make sure pitot tubes are not reversed, timeout after ~30 seconds */
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while (calibration_counter < 1500) {
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while (calibration_counter < maxcount) {
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/* wait blocking for new data */
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struct pollfd fds[1];
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@ -204,7 +205,7 @@ int do_airspeed_calibration(int mavlink_fd)
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if (fabsf(diff_pres.differential_pressure_raw_pa) < 50.0f) {
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if (calibration_counter % 100 == 0) {
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mavlink_log_critical(mavlink_fd, "Create airflow on pitot (%d Pa, #h101)",
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mavlink_log_critical(mavlink_fd, "Missing airflow! (%d, wanted: 50 Pa, #h101)",
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(int)diff_pres.differential_pressure_raw_pa);
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}
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continue;
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@ -212,6 +213,8 @@ int do_airspeed_calibration(int mavlink_fd)
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/* do not allow negative values */
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if (diff_pres.differential_pressure_raw_pa < 0.0f) {
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mavlink_log_info(mavlink_fd, "negative pressure: ERROR (%d Pa)",
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(int)diff_pres.differential_pressure_raw_pa);
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mavlink_log_critical(mavlink_fd, "%d Pa: swap static and dynamic ports!", (int)diff_pres.differential_pressure_raw_pa);
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close(diff_pres_sub);
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@ -246,6 +249,12 @@ int do_airspeed_calibration(int mavlink_fd)
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}
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}
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if (calibration_counter == maxcount) {
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mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
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close(diff_pres_sub);
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return ERROR;
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}
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mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 100);
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mavlink_log_info(mavlink_fd, CAL_DONE_MSG, sensor_name);
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