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Merge branch 'airspeed_filter_fixes' into paul_estimator_numeric
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commit
a0ceeee9ef
@ -176,11 +176,14 @@ ETSAirspeed::collect()
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_max_differential_pressure_pa = diff_pres_pa;
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}
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// XXX we may want to smooth out the readings to remove noise.
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differential_pressure_s report;
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report.timestamp = hrt_absolute_time();
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report.error_count = perf_event_count(_comms_errors);
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report.differential_pressure_pa = (float)diff_pres_pa;
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// XXX we may want to smooth out the readings to remove noise.
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report.differential_pressure_filtered_pa = (float)diff_pres_pa;
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report.temperature = -1000.0f;
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report.voltage = 0;
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report.max_differential_pressure_pa = _max_differential_pressure_pa;
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@ -1033,10 +1033,12 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw)
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raw.differential_pressure_timestamp = _diff_pres.timestamp;
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raw.differential_pressure_filtered_pa = _diff_pres.differential_pressure_filtered_pa;
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float air_temperature_celcius = (_diff_pres.temperature > -300.0f) ? _diff_pres.temperature : (raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
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_airspeed.timestamp = _diff_pres.timestamp;
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_airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_filtered_pa);
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_airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_filtered_pa + raw.baro_pres_mbar * 1e2f,
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raw.baro_pres_mbar * 1e2f, raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
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raw.baro_pres_mbar * 1e2f, air_temperature_celcius);
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/* announce the airspeed if needed, just publish else */
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if (_airspeed_pub > 0) {
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@ -1244,6 +1246,8 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
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_diff_pres.timestamp = t;
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_diff_pres.differential_pressure_pa = diff_pres_pa;
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_diff_pres.differential_pressure_filtered_pa = diff_pres_pa;
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_diff_pres.temperature = -1000.0f;
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_diff_pres.voltage = voltage;
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/* announce the airspeed if needed, just publish else */
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@ -58,7 +58,7 @@ struct differential_pressure_s {
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float differential_pressure_filtered_pa; /**< Low pass filtered differential pressure reading */
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float max_differential_pressure_pa; /**< Maximum differential pressure reading */
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float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
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float temperature; /**< Temperature provided by sensor */
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float temperature; /**< Temperature provided by sensor, -1000.0f if unknown */
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};
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