ardupilot/Tools/AP_Periph/airspeed.cpp

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#include "AP_Periph.h"
#ifdef HAL_PERIPH_ENABLE_AIRSPEED
/*
airspeed support
*/
#include <dronecan_msgs.h>
#ifndef AP_PERIPH_PROBE_CONTINUOUS
#define AP_PERIPH_PROBE_CONTINUOUS 0
#endif
/*
update CAN airspeed
*/
void AP_Periph_FW::can_airspeed_update(void)
{
if (!airspeed.enabled()) {
return;
}
#if AP_PERIPH_PROBE_CONTINUOUS
if (!airspeed.healthy()) {
uint32_t now = AP_HAL::millis();
static uint32_t last_probe_ms;
if (now - last_probe_ms >= 1000) {
last_probe_ms = now;
airspeed.allocate();
}
}
#endif
uint32_t now = AP_HAL::millis();
if (now - last_airspeed_update_ms < 50) {
// max 20Hz data
return;
}
last_airspeed_update_ms = now;
airspeed.update();
if (!airspeed.healthy()) {
// don't send any data
return;
}
const float press = airspeed.get_corrected_pressure();
float temp;
if (!airspeed.get_temperature(temp)) {
temp = nanf("");
} else {
temp = C_TO_KELVIN(temp);
}
uavcan_equipment_air_data_RawAirData pkt {};
// unfilled elements are NaN
pkt.static_pressure = nanf("");
pkt.static_pressure_sensor_temperature = nanf("");
pkt.differential_pressure_sensor_temperature = nanf("");
pkt.pitot_temperature = nanf("");
// populate the elements we have
pkt.differential_pressure = press;
pkt.static_air_temperature = temp;
// if a Pitot tube temperature sensor is available, use it
#if AP_TEMPERATURE_SENSOR_ENABLED
for (uint8_t i=0; i<temperature_sensor.num_instances(); i++) {
float temp_pitot;
if (temperature_sensor.get_source(i) == AP_TemperatureSensor_Params::Source::Pitot_tube && temperature_sensor.get_temperature(temp_pitot, i)) {
pkt.pitot_temperature = C_TO_KELVIN(temp_pitot);
break;
}
}
#endif
uint8_t buffer[UAVCAN_EQUIPMENT_AIR_DATA_RAWAIRDATA_MAX_SIZE] {};
uint16_t total_size = uavcan_equipment_air_data_RawAirData_encode(&pkt, buffer, !periph.canfdout());
canard_broadcast(UAVCAN_EQUIPMENT_AIR_DATA_RAWAIRDATA_SIGNATURE,
UAVCAN_EQUIPMENT_AIR_DATA_RAWAIRDATA_ID,
CANARD_TRANSFER_PRIORITY_LOW,
&buffer[0],
total_size);
}
#endif // HAL_PERIPH_ENABLE_AIRSPEED