mirror of https://github.com/ArduPilot/ardupilot
76 lines
1.8 KiB
C++
76 lines
1.8 KiB
C++
#include <AP_HAL/AP_HAL.h>
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#if CONFIG_HAL_BOARD_SUBTYPE == HAL_BOARD_SUBTYPE_LINUX_QFLIGHT
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#include <unistd.h>
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#include <stdio.h>
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#include "AP_Baro_qflight.h"
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#include <AP_HAL_Linux/qflight/qflight_util.h>
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#include <AP_HAL_Linux/qflight/qflight_dsp.h>
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extern const AP_HAL::HAL& hal;
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/*
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constructor - opens the QFLIGHT drivers
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*/
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AP_Baro_QFLIGHT::AP_Baro_QFLIGHT(AP_Baro &baro) :
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AP_Baro_Backend(baro)
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{
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instance = _frontend.register_sensor();
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hal.scheduler->register_timer_process(FUNCTOR_BIND_MEMBER(&AP_Baro_QFLIGHT::timer_update, void));
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hal.scheduler->delay(100);
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}
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// Read the sensor
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void AP_Baro_QFLIGHT::timer_update(void)
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{
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uint32_t now = AP_HAL::millis();
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if (now - last_check_ms < 25) {
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return;
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}
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last_check_ms = now;
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if (barobuf == nullptr) {
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barobuf = QFLIGHT_RPC_ALLOCATE(DSPBuffer::BARO);
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if (barobuf == nullptr) {
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AP_HAL::panic("Unable to allocate baro buffer");
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}
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}
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int ret = qflight_get_baro_data((uint8_t *)barobuf, sizeof(*barobuf));
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if (ret != 0) {
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return;
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}
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if (!_sem->take(0)) {
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return;
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}
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for (uint16_t i=0; i<barobuf->num_samples; i++) {
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DSPBuffer::BARO::BUF &b = barobuf->buf[i];
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pressure_sum += b.pressure_pa;
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temperature_sum += b.temperature_C;
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sum_count++;
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}
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_sem->give();
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}
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// Read the sensor
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void AP_Baro_QFLIGHT::update(void)
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{
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if (!_sem->take_nonblocking()) {
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return;
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}
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if (sum_count > 0) {
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_copy_to_frontend(instance,
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pressure_sum/sum_count,
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temperature_sum/sum_count);
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sum_count = 0;
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pressure_sum = 0;
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temperature_sum = 0;
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}
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_sem->give();
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}
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#endif // CONFIG_HAL_BOARD_SUBTYPE
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