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Cleanup
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@@ -99,6 +99,12 @@
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#define BAT_VOL_LOWPASS_2 0.01f
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#define VOLTAGE_BATTERY_IGNORE_THRESHOLD_VOLTS 3.5f
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/**
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* HACK - true temperature is much less than indicated temperature in baro,
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* subtract 5 degrees in an attempt to account for the electrical upheating of the PCB
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*/
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#define PCB_TEMP_ESTIMATE_DEG 5.0f
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#define PPM_INPUT_TIMEOUT_INTERVAL 50000 /**< 50 ms timeout / 20 Hz */
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#define limit_minus_one_to_one(arg) (arg < -1.0f) ? -1.0f : ((arg > 1.0f) ? 1.0f : arg)
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@@ -913,15 +919,9 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw)
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raw.differential_pressure_pa = _diff_pres.differential_pressure_pa;
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raw.differential_pressure_counter++;
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float airspeed_true = calc_true_airspeed(_diff_pres.differential_pressure_pa + raw.baro_pres_mbar*1e2f,
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raw.baro_pres_mbar*1e2f, raw.baro_temp_celcius - 5.0f); //factor 1e2 for conversion from mBar to Pa
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// XXX HACK - true temperature is much less than indicated temperature in baro,
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// subtract 5 degrees in an attempt to account for the electrical upheating of the PCB
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float airspeed_indicated = calc_indicated_airspeed(_diff_pres.differential_pressure_pa);
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_airspeed.indicated_airspeed_m_s = airspeed_indicated;
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_airspeed.true_airspeed_m_s = airspeed_true;
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_airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_pa);
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_airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_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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/* announce the airspeed if needed, just publish else */
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if (_airspeed_pub > 0) {
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