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