ardupilot/ArduCopterMega/sensors.pde

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void ReadSCP1000(void) {}
void init_pressure_ground(void)
{
for(int i = 0; i < 300; i++){ // We take some readings...
delay(20);
APM_BMP085.Read(); // Get initial data from absolute pressure sensor
abs_pressure_ground = (abs_pressure_ground * 9l + APM_BMP085.Press) / 10l;
ground_temperature = (ground_temperature * 9 + APM_BMP085.Temp) / 10;
}
abs_pressure = APM_BMP085.Press;
}
void read_barometer(void){
float x, scaling, temp;
APM_BMP085.Read(); // Get new data from absolute pressure sensor
//abs_pressure = (abs_pressure + APM_BMP085.Press) >> 1; // Small filtering
abs_pressure = ((float)abs_pressure * .9) + ((float)APM_BMP085.Press * .1); // large filtering
scaling = (float)abs_pressure_ground / (float)abs_pressure;
temp = ((float)ground_temperature / 10.f) + 273.15;
x = log(scaling) * temp * 29271.267f;
current_loc.alt = (long)(x / 10) + home.alt + baro_offset; // Pressure altitude in centimeters
}
// in M/S * 100
void read_airspeed(void)
{
}
#if BATTERY_EVENT == 1
void read_battery(void)
{
battery_voltage1 = BATTERY_VOLTAGE(analogRead(BATTERY_PIN1)) * .1 + battery_voltage1 * .9;
battery_voltage2 = BATTERY_VOLTAGE(analogRead(BATTERY_PIN2)) * .1 + battery_voltage2 * .9;
battery_voltage3 = BATTERY_VOLTAGE(analogRead(BATTERY_PIN3)) * .1 + battery_voltage3 * .9;
battery_voltage4 = BATTERY_VOLTAGE(analogRead(BATTERY_PIN4)) * .1 + battery_voltage4 * .9;
#if BATTERY_TYPE == 0
if(battery_voltage3 < LOW_VOLTAGE)
low_battery_event();
battery_voltage = battery_voltage3; // set total battery voltage, for telemetry stream
#endif
#if BATTERY_TYPE == 1
if(battery_voltage4 < LOW_VOLTAGE)
low_battery_event();
battery_voltage = battery_voltage4; // set total battery voltage, for telemetry stream
#endif
}
#endif