本文整理汇总了C++中AP_Baro类的典型用法代码示例。如果您正苦于以下问题：C++ AP_Baro类的具体用法？C++ AP_Baro怎么用？C++ AP_Baro使用的例子？那么, 这里精选的类代码示例或许可以为您提供帮助。
在下文中一共展示了AP_Baro类的9个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于系统推荐出更棒的C++代码示例。
示例1: send_sensor_offsets
void GCS_MAVLINK::send_sensor_offsets(const AP_InertialSensor &ins, const Compass &compass, AP_Baro &barometer)
{
// run this message at a much lower rate - otherwise it
// pointlessly wastes quite a lot of bandwidth
static uint8_t counter;
if (counter++ < 10) {
return;
}
counter = 0;
const Vector3f &mag_offsets = compass.get_offsets(0);
const Vector3f &accel_offsets = ins.get_accel_offsets(0);
const Vector3f &gyro_offsets = ins.get_gyro_offsets(0);
mavlink_msg_sensor_offsets_send(chan,
mag_offsets.x,
mag_offsets.y,
mag_offsets.z,
compass.get_declination(),
barometer.get_pressure(),
barometer.get_temperature()*100,
gyro_offsets.x,
gyro_offsets.y,
gyro_offsets.z,
accel_offsets.x,
accel_offsets.y,
accel_offsets.z);
}示例2: send_scaled_pressure
void GCS_MAVLINK::send_scaled_pressure(AP_Baro &barometer)
{
float pressure = barometer.get_pressure();
mavlink_msg_scaled_pressure_send(
chan,
hal.scheduler->millis(),
pressure*0.01f, // hectopascal
(pressure - barometer.get_ground_pressure())*0.01f, // hectopascal
barometer.get_temperature()*100); // 0.01 degrees C
}示例3: send_scaled_pressure
void GCS_MAVLINK::send_scaled_pressure(AP_Baro &barometer)
{
uint32_t now = hal.scheduler->millis();
float pressure = barometer.get_pressure(0);
mavlink_msg_scaled_pressure_send(
chan,
now,
pressure*0.01f, // hectopascal
(pressure - barometer.get_ground_pressure(0))*0.01f, // hectopascal
barometer.get_temperature(0)*100); // 0.01 degrees C
#if BARO_MAX_INSTANCES > 1
if (barometer.num_instances() > 1) {
pressure = barometer.get_pressure(1);
mavlink_msg_scaled_pressure2_send(
chan,
now,
pressure*0.01f, // hectopascal
(pressure - barometer.get_ground_pressure(1))*0.01f, // hectopascal
barometer.get_temperature(1)*100); // 0.01 degrees C
}
#endif
}示例4: send_scaled_pressure
void GCS_MAVLINK::send_scaled_pressure(AP_Baro &barometer)
{
uint32_t now = AP_HAL::millis();
float pressure = barometer.get_pressure(0);
mavlink_msg_scaled_pressure_send(
chan,
now,
pressure*0.01f, // hectopascal
(pressure - barometer.get_ground_pressure(0))*0.01f, // hectopascal
barometer.get_temperature(0)*100); // 0.01 degrees C
if (barometer.num_instances() > 1) {
pressure = barometer.get_pressure(1);
mavlink_msg_scaled_pressure2_send(
chan,
now,
pressure*0.01f, // hectopascal
(pressure - barometer.get_ground_pressure(1))*0.01f, // hectopascal
barometer.get_temperature(1)*100); // 0.01 degrees C
}
if (barometer.num_instances() > 2) {
pressure = barometer.get_pressure(2);
mavlink_msg_scaled_pressure3_send(
chan,
now,
pressure*0.01f, // hectopascal
(pressure - barometer.get_ground_pressure(2))*0.01f, // hectopascal
barometer.get_temperature(2)*100); // 0.01 degrees C
}
}示例5: setup
void ReplayVehicle::setup(void)
{
load_parameters();
// we pass zero log structures, as we will be outputting the log
// structures we need manually, to prevent FMT duplicates
dataflash.Init(log_structure, 0);
dataflash.StartNewLog();
ahrs.set_compass(&compass);
ahrs.set_fly_forward(true);
ahrs.set_wind_estimation(true);
ahrs.set_correct_centrifugal(true);
ahrs.set_ekf_use(true);
EKF2.set_enable(true);
printf("Starting disarmed\n");
hal.util->set_soft_armed(false);
barometer.init();
barometer.setHIL(0);
barometer.update();
compass.init();
ins.set_hil_mode();
}示例6: setup
void setup()
{
hal.console->println("Barometer library test");
hal.scheduler->delay(1000);
barometer.init();
barometer.calibrate();
timer = hal.scheduler->micros();
}示例7: loop
void loop()
{
// run accumulate() at 50Hz and update() at 10Hz
if((hal.scheduler->micros() - timer) > 20*1000UL) {
timer = hal.scheduler->micros();
barometer.accumulate();
if (counter++ < 5) {
return;
}
counter = 0;
barometer.update();
uint32_t read_time = hal.scheduler->micros() - timer;
float alt = barometer.get_altitude();
if (!barometer.healthy()) {
hal.console->println("not healthy");
return;
}
hal.console->print("Pressure:");
hal.console->print(barometer.get_pressure());
hal.console->print(" Temperature:");
hal.console->print(barometer.get_temperature());
hal.console->print(" Altitude:");
hal.console->print(alt);
hal.console->printf(" climb=%.2f t=%u",
barometer.get_climb_rate(),
(unsigned)read_time);
hal.console->println();
} else {
hal.scheduler->delay(1);
}
}示例8: setup
void setup(void)
{
serial_manager.init();
ins.init(100);
baro.init();
ahrs.init();
gps.init(NULL, serial_manager);
}示例9: setup
void ReplayVehicle::setup(void) {
dataflash.Init(log_structure, sizeof(log_structure)/sizeof(log_structure[0]));
dataflash.StartNewLog();
ahrs.set_compass(&compass);
ahrs.set_fly_forward(true);
ahrs.set_wind_estimation(true);
ahrs.set_correct_centrifugal(true);
ahrs.set_ekf_use(true);
printf("Starting disarmed\n");
hal.util->set_soft_armed(false);
barometer.init();
barometer.setHIL(0);
barometer.update();
compass.init();
ins.set_hil_mode();
}