ardupilot/ArduCopter/sensors.pde

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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
// Sensors are not available in HIL_MODE_ATTITUDE
#if HIL_MODE != HIL_MODE_ATTITUDE
static void ReadSCP1000(void) {}
#if CONFIG_SONAR == ENABLED
static void init_sonar(void)
{
#if CONFIG_SONAR_SOURCE == SONAR_SOURCE_ADC
sonar.calculate_scaler(g.sonar_type, 3.3);
#else
sonar.calculate_scaler(g.sonar_type, 5.0);
#endif
}
#endif
static void init_barometer(void)
{
#if HIL_MODE == HIL_MODE_SENSORS
gcs_update(); // look for inbound hil packets for initialization
#endif
ground_temperature = barometer.get_temperature();
int i;
// We take some readings...
for(i = 0; i < 60; i++){
delay(20);
// get new data from absolute pressure sensor
barometer.read();
//Serial.printf("init %ld, %d, -, %ld, %ld\n", barometer.RawTemp, barometer.Temp, barometer.RawPress, barometer.Press);
}
for(i = 0; i < 40; i++){
delay(20);
#if HIL_MODE == HIL_MODE_SENSORS
gcs_update(); // look for inbound hil packets
#endif
// Get initial data from absolute pressure sensor
barometer.read();
ground_pressure = baro_filter.apply(barometer.get_pressure());
//Serial.printf("t: %ld, p: %d\n", ground_pressure, ground_temperature);
/*Serial.printf("init %d, %d, -, %d, %d, -, %d, %d\n",
barometer.RawTemp,
barometer.Temp,
barometer.RawPress,
barometer.Press,
ground_temperature,
ground_pressure);*/
}
// save our ground temp
ground_temperature = barometer.get_temperature();
}
static void reset_baro(void)
{
ground_pressure = baro_filter.apply(barometer.get_pressure());
ground_temperature = barometer.get_temperature();
}
static int32_t read_barometer(void)
{
float x, scaling, temp;
barometer.read();
float abs_pressure = baro_filter.apply(barometer.get_pressure());
//Serial.printf("%ld, %ld, %ld, %ld\n", barometer.RawTemp, barometer.RawPress, barometer.Press, abs_pressure);
scaling = (float)ground_pressure / abs_pressure;
temp = ((float)ground_temperature / 10.0f) + 273.15f;
x = log(scaling) * temp * 29271.267f;
return (x / 10);
}
#endif // HIL_MODE != HIL_MODE_ATTITUDE
static void init_compass()
{
compass.set_orientation(MAG_ORIENTATION); // set compass's orientation on aircraft
if (!compass.init() || !compass.read()) {
// make sure we don't pass a broken compass to DCM
Serial.println_P(PSTR("COMPASS INIT ERROR"));
return;
}
ahrs.set_compass(&compass);
compass.null_offsets_enable();
}
static void init_optflow()
{
#ifdef OPTFLOW_ENABLED
if( optflow.init(false) == false ) {
g.optflow_enabled = false;
SendDebug("\nFailed to Init OptFlow ");
}
optflow.set_orientation(OPTFLOW_ORIENTATION); // set optical flow sensor's orientation on aircraft
optflow.set_frame_rate(2000); // set minimum update rate (which should lead to maximum low light performance
optflow.set_resolution(OPTFLOW_RESOLUTION); // set optical flow sensor's resolution
optflow.set_field_of_view(OPTFLOW_FOV); // set optical flow sensor's field of view
// setup timed read of sensor
//timer_scheduler.register_process(&AP_OpticalFlow::read);
#endif
}
static void read_battery(void)
{
if(g.battery_monitoring == 0){
battery_voltage1 = 0;
return;
}
if(g.battery_monitoring == 3 || g.battery_monitoring == 4)
battery_voltage1 = BATTERY_VOLTAGE(analogRead(BATTERY_PIN_1)) * .1 + battery_voltage1 * .9;
if(g.battery_monitoring == 4) {
current_amps1 = CURRENT_AMPS(analogRead(CURRENT_PIN_1)) * .1 + current_amps1 * .9; //reads power sensor current pin
current_total1 += current_amps1 * 0.02778; // called at 100ms on average, .0002778 is 1/3600 (conversion to hours)
}
#if BATTERY_EVENT == ENABLED
//if(battery_voltage < g.low_voltage)
// low_battery_event();
if((battery_voltage1 < g.low_voltage) || (g.battery_monitoring == 4 && current_total1 > g.pack_capacity)){
low_battery_event();
#if COPTER_LEDS == ENABLED
if ( bitRead(g.copter_leds_mode, 3) ){ // Only Activate if a battery is connected to avoid alarm on USB only
if (battery_voltage1 > 1){
piezo_on();
}else{
piezo_off();
}
}
}else if ( bitRead(g.copter_leds_mode, 3) ){
piezo_off();
#endif // COPTER_LEDS
}
#endif //BATTERY_EVENT
}
//v: 10.9453, a: 17.4023, mah: 8.2