mirror of https://github.com/ArduPilot/ardupilot
AP_Soaring: eliminate GCS_MAVLINK::send_statustext_all
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93e09c51d3
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@ -182,10 +182,10 @@ bool SoaringController::check_cruise_criteria()
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float alt = _vario.alt;
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if (soar_active && (AP_HAL::micros64() - _thermal_start_time_us) > ((unsigned)min_thermal_s * 1e6) && thermalability < McCready(alt)) {
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GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "Thermal weak, recommend quitting: W %f R %f th %f alt %f Mc %f\n", (double)_ekf.X[0], (double)_ekf.X[1], (double)thermalability, (double)alt, (double)McCready(alt));
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gcs().send_text(MAV_SEVERITY_INFO, "Thermal weak, recommend quitting: W %f R %f th %f alt %f Mc %f\n", (double)_ekf.X[0], (double)_ekf.X[1], (double)thermalability, (double)alt, (double)McCready(alt));
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return true;
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} else if (soar_active && (alt>alt_max || alt<alt_min)) {
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GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_ALERT, "Out of allowable altitude range, beginning cruise. Alt = %f\n", (double)alt);
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gcs().send_text(MAV_SEVERITY_ALERT, "Out of allowable altitude range, beginning cruise. Alt = %f\n", (double)alt);
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return true;
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}
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@ -272,10 +272,10 @@ void SoaringController::update_thermalling()
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// Print32_t filter info for debugging
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int32_t i;
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for (i = 0; i < 4; i++) {
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GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "%e ", (double)_ekf.P[i][i]);
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gcs().send_text(MAV_SEVERITY_INFO, "%e ", (double)_ekf.P[i][i]);
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}
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for (i = 0; i < 4; i++) {
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GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "%e ", (double)_ekf.X[i]);
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gcs().send_text(MAV_SEVERITY_INFO, "%e ", (double)_ekf.X[i]);
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}
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#endif
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@ -75,6 +75,6 @@ float Variometer::correct_netto_rate(float climb_rate,
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//float temp_netto = netto_rate;
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//float dVdt = SpdHgt_Controller->get_VXdot();
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//netto_rate = netto_rate + aspd*dVdt/GRAVITY_MSS;
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//GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "%f %f %f %f\n",temp_netto,dVdt,netto_rate,barometer.get_altitude());
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//gcs().send_text(MAV_SEVERITY_INFO, "%f %f %f %f\n",temp_netto,dVdt,netto_rate,barometer.get_altitude());
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return netto_rate;
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}
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