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https://github.com/ArduPilot/ardupilot
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uncrustify ArduPlane/sensors.pde
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956b101189
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@ -15,7 +15,7 @@ static LowPassFilterInt32 altitude_filter(0.3);
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// above the calibration altitude
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static int32_t read_barometer(void)
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{
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barometer.read();
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barometer.read();
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return altitude_filter.apply(barometer.get_altitude() * 100.0);
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}
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@ -23,7 +23,7 @@ static int32_t read_barometer(void)
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static void read_airspeed(void)
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{
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airspeed.read();
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calc_airspeed_errors();
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calc_airspeed_errors();
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}
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static void zero_airspeed(void)
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@ -34,24 +34,24 @@ static void zero_airspeed(void)
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static void read_battery(void)
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{
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if(g.battery_monitoring == 0) {
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battery_voltage1 = 0;
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return;
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}
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if(g.battery_monitoring == 3 || g.battery_monitoring == 4) {
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static AP_AnalogSource_Arduino bat_pin(BATTERY_PIN_1);
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battery_voltage1 = BATTERY_VOLTAGE(bat_pin.read_average());
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if(g.battery_monitoring == 0) {
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battery_voltage1 = 0;
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return;
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}
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if(g.battery_monitoring == 4) {
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if(g.battery_monitoring == 3 || g.battery_monitoring == 4) {
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static AP_AnalogSource_Arduino bat_pin(BATTERY_PIN_1);
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battery_voltage1 = BATTERY_VOLTAGE(bat_pin.read_average());
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}
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if(g.battery_monitoring == 4) {
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static AP_AnalogSource_Arduino current_pin(CURRENT_PIN_1);
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current_amps1 = CURRENT_AMPS(current_pin.read_average());
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current_total1 += current_amps1 * (float)delta_ms_medium_loop * 0.0002778; // .0002778 is 1/3600 (conversion to hours)
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}
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#if BATTERY_EVENT == ENABLED
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if(battery_voltage1 < LOW_VOLTAGE) low_battery_event();
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if(g.battery_monitoring == 4 && current_total1 > g.pack_capacity) low_battery_event();
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#endif
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current_amps1 = CURRENT_AMPS(current_pin.read_average());
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current_total1 += current_amps1 * (float)delta_ms_medium_loop * 0.0002778; // .0002778 is 1/3600 (conversion to hours)
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}
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#if BATTERY_EVENT == ENABLED
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if(battery_voltage1 < LOW_VOLTAGE) low_battery_event();
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if(g.battery_monitoring == 4 && current_total1 > g.pack_capacity) low_battery_event();
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#endif
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}
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