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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-19 00:03:35 +08:00
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+18
-11
@@ -187,6 +187,7 @@ private:
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float mag_scale[3];
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float accel_offset[3];
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float accel_scale[3];
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float airspeed_offset;
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int rc_type;
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@@ -235,6 +236,7 @@ private:
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param_t accel_scale[3];
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param_t mag_offset[3];
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param_t mag_scale[3];
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param_t airspeed_offset;
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param_t rc_map_roll;
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param_t rc_map_pitch;
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@@ -480,6 +482,9 @@ Sensors::Sensors() :
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_parameter_handles.mag_scale[1] = param_find("SENS_MAG_YSCALE");
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_parameter_handles.mag_scale[2] = param_find("SENS_MAG_ZSCALE");
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/*Airspeed offset */
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_parameter_handles.airspeed_offset = param_find("SENS_VAIR_OFF");
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_parameter_handles.battery_voltage_scaling = param_find("BAT_V_SCALING");
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/* fetch initial parameter values */
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@@ -687,6 +692,9 @@ Sensors::parameters_update()
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param_get(_parameter_handles.mag_scale[1], &(_parameters.mag_scale[1]));
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param_get(_parameter_handles.mag_scale[2], &(_parameters.mag_scale[2]));
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/* Airspeed offset */
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param_get(_parameter_handles.airspeed_offset, &(_parameters.airspeed_offset));
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/* scaling of ADC ticks to battery voltage */
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if (param_get(_parameter_handles.battery_voltage_scaling, &(_parameters.battery_voltage_scaling)) != OK) {
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warnx("Failed updating voltage scaling param");
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@@ -993,7 +1001,7 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
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/* look for battery channel */
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for (unsigned i = 0; i < sizeof(buf_adc) / sizeof(buf_adc[0]); i++) {
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if (ret >= (int)sizeof(buf_adc[0])) {
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if (ADC_BATTERY_VOLTAGE_CHANNEL == buf_adc[i].am_channel) {
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@@ -1025,8 +1033,7 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
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} else if (ADC_AIRSPEED_VOLTAGE_CHANNEL == buf_adc[i].am_channel) {
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/* calculate airspeed, raw is the difference from */
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float voltage = buf_adc[i].am_data / 4096.0f;
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float voltage = (float)(buf_adc[i].am_data ) * 3.3f / 4096.0f * 2.0f; //V_ref/4096 * (voltage divider factor)
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/**
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* The voltage divider pulls the signal down, only act on
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@@ -1034,24 +1041,24 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
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*/
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if (voltage > 0.4f) {
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float pres_raw = fabsf(voltage - (3.3f / 2.0f));
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float pres_mbar = pres_raw * (3.3f / 5.0f) * 10.0f;
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float diff_pres_pa = (voltage - _parameters.airspeed_offset) * 1000.0f; //for MPXV7002DP sensor
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float airspeed_true = calc_true_airspeed(pres_mbar + _barometer.pressure,
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_barometer.pressure, _barometer.temperature - 5.0f);
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float airspeed_true = calc_true_airspeed(diff_pres_pa + _barometer.pressure*1e2f,
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_barometer.pressure*1e2f, _barometer.temperature - 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(pres_mbar + _barometer.pressure,
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_barometer.pressure, _barometer.temperature - 5.0f);
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// XXX HACK
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float airspeed_indicated = calc_indicated_airspeed(diff_pres_pa);
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//printf("voltage: %.4f, diff_pres_pa %.4f, baro press %.4f Pa, v_ind %.4f, v_true %.4f\n", (double)voltage, (double)diff_pres_pa, (double)_barometer.pressure*1e2f, (double)airspeed_indicated, (double)airspeed_true);
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_differential_pressure.timestamp = hrt_absolute_time();
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_differential_pressure.static_pressure_mbar = _barometer.pressure;
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_differential_pressure.differential_pressure_mbar = pres_mbar;
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_differential_pressure.differential_pressure_mbar = diff_pres_pa*1e-2f;
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_differential_pressure.temperature_celcius = _barometer.temperature;
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_differential_pressure.indicated_airspeed_m_s = airspeed_indicated;
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_differential_pressure.true_airspeed_m_s = airspeed_true;
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_differential_pressure.voltage = voltage;
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/* announce the airspeed if needed, just publish else */
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if (_airspeed_pub > 0) {
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