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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-16 08:23:34 +08:00
Force update of offset, do not add offset in final value
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@@ -140,6 +140,16 @@ int do_airspeed_calibration(int mavlink_fd)
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if (isfinite(diff_pres_offset)) {
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int fd_scale = open(AIRSPEED_DEVICE_PATH, 0);
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airscale.offset_pa = diff_pres_offset;
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if (fd_scale > 0) {
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if (OK != ioctl(fd_scale, AIRSPEEDIOCSSCALE, (long unsigned int)&airscale)) {
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mavlink_log_critical(mavlink_fd, "airspeed offset update failed");
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}
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close(fd_scale);
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}
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if (param_set(param_find("SENS_DPRES_OFF"), &(diff_pres_offset))) {
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mavlink_log_critical(mavlink_fd, CAL_FAILED_SET_PARAMS_MSG);
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close(diff_pres_sub);
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@@ -182,20 +192,19 @@ int do_airspeed_calibration(int mavlink_fd)
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if (poll_ret) {
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orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres);
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float calibrated_pa = diff_pres.differential_pressure_raw_pa - diff_pres_offset;
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calibration_counter++;
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if (fabsf(calibrated_pa) < 50.0f) {
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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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(int)calibrated_pa);
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(int)diff_pres.differential_pressure_raw_pa);
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}
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continue;
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}
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/* do not allow negative values */
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if (calibrated_pa < 0.0f) {
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mavlink_log_critical(mavlink_fd, "%d Pa: swap static and dynamic ports!", (int)calibrated_pa);
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if (diff_pres.differential_pressure_raw_pa < 0.0f) {
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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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/* the user setup is wrong, wipe the calibration to force a proper re-calibration */
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@@ -217,7 +226,7 @@ int do_airspeed_calibration(int mavlink_fd)
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return ERROR;
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} else {
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mavlink_log_info(mavlink_fd, "positive pressure: OK (%d Pa)",
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(int)calibrated_pa);
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(int)diff_pres.differential_pressure_raw_pa);
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break;
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}
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@@ -668,8 +668,8 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
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struct airspeed_s airspeed;
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if (ret = orb_copy(ORB_ID(airspeed), fd, &airspeed) ||
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hrt_elapsed_time(&airspeed.timestamp) > 50 * 1000) {
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if ((ret = orb_copy(ORB_ID(airspeed), fd, &airspeed)) ||
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(hrt_elapsed_time(&airspeed.timestamp) > (50 * 1000))) {
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mavlink_log_critical(mavlink_fd, "ARM FAIL: AIRSPEED SENSOR MISSING");
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failed = true;
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goto system_eval;
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