PX4-Autopilot/src/modules/commander/baro_calibration.cpp
Roman Bapst dd2322d622
Added PerformanceModel for fixed wing (#22091)
* created a Performance Model for fixed wing vehicle
- added compensation for maximum climbrate, minimum sinkrate, minimum airspeed and trim airspeed based on weight ratio and air density
- added atmosphere lib to standard atmosphere calculations


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Signed-off-by: RomanBapst <bapstroman@gmail.com>
Co-authored-by: Thomas Stastny <thomas.stastny@auterion.com>
2023-11-21 17:13:50 +01:00

201 lines
6.3 KiB
C++

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/**
* @file baro_calibration.cpp
*
* Simple barometer calibration routine
*/
#include "baro_calibration.h"
#include "commander_helper.h"
#include "calibration_routines.h"
#include "calibration_messages.h"
#include <px4_platform_common/defines.h>
#include <px4_platform_common/posix.h>
#include <px4_platform_common/time.h>
#include <drivers/drv_hrt.h>
#include <matrix/math.hpp>
#include <lib/atmosphere/atmosphere.h>
#include <lib/sensor_calibration/Barometer.hpp>
#include <lib/sensor_calibration/Utilities.hpp>
#include <lib/systemlib/mavlink_log.h>
#include <lib/systemlib/err.h>
#include <uORB/Subscription.hpp>
#include <uORB/SubscriptionMultiArray.hpp>
#include <uORB/topics/sensor_baro.h>
#include <uORB/topics/sensor_gps.h>
using namespace matrix;
using namespace time_literals;
using namespace atmosphere;
static constexpr char sensor_name[] {"baro"};
static constexpr int MAX_SENSOR_COUNT = 4;
int do_baro_calibration(orb_advert_t *mavlink_log_pub)
{
calibration_log_info(mavlink_log_pub, CAL_QGC_STARTED_MSG, sensor_name);
// GPS (used for reference)
uORB::SubscriptionMultiArray<sensor_gps_s, 3> sensor_gps_subs{ORB_ID::sensor_gps};
float gps_altitude_sum = NAN;
int gps_altitude_sum_count = 0;
uORB::SubscriptionMultiArray<sensor_baro_s, MAX_SENSOR_COUNT> sensor_baro_subs{ORB_ID::sensor_baro};
calibration::Barometer calibration[MAX_SENSOR_COUNT] {};
uint64_t timestamp_sample_sum[MAX_SENSOR_COUNT] {0};
float data_sum[MAX_SENSOR_COUNT] {};
float temperature_sum[MAX_SENSOR_COUNT] {};
int data_sum_count[MAX_SENSOR_COUNT] {};
const hrt_abstime time_start_us = hrt_absolute_time();
while (hrt_elapsed_time(&time_start_us) < 3_s) {
for (int instance = 0; instance < MAX_SENSOR_COUNT; instance++) {
sensor_baro_s sensor_baro;
while (sensor_baro_subs[instance].update(&sensor_baro)) {
calibration[instance].set_device_id(sensor_baro.device_id);
// pressure corrected with offset (if available)
const float pressure_corrected = calibration[instance].Correct(sensor_baro.pressure);
timestamp_sample_sum[instance] += sensor_baro.timestamp_sample;
data_sum[instance] += pressure_corrected;
temperature_sum[instance] += sensor_baro.temperature;
data_sum_count[instance]++;
}
}
for (auto &gps_sub : sensor_gps_subs) {
sensor_gps_s sensor_gps;
if (gps_sub.update(&sensor_gps)) {
if ((hrt_elapsed_time(&sensor_gps.timestamp) < 1_s)
&& (sensor_gps.fix_type >= 2) && (sensor_gps.epv < 100)) {
float alt = (float)sensor_gps.altitude_msl_m;
if (PX4_ISFINITE(gps_altitude_sum)) {
gps_altitude_sum += alt;
gps_altitude_sum_count++;
} else {
gps_altitude_sum = alt;
gps_altitude_sum_count = 1;
}
}
}
}
px4_usleep(100_ms);
}
float gps_altitude = NAN;
if (PX4_ISFINITE(gps_altitude_sum) && (gps_altitude_sum_count > 0)) {
gps_altitude = gps_altitude_sum / gps_altitude_sum_count;
}
if (!PX4_ISFINITE(gps_altitude)) {
calibration_log_critical(mavlink_log_pub, CAL_QGC_FAILED_MSG, "GPS required for baro cal");
return PX4_ERROR;
}
bool param_save = false;
for (int instance = 0; instance < MAX_SENSOR_COUNT; instance++) {
if ((calibration[instance].device_id() != 0) && (data_sum_count[instance] > 0)) {
const float pressure_pa = data_sum[instance] / data_sum_count[instance];
const float temperature = temperature_sum[instance] / data_sum_count[instance];
float pressure_altitude = getAltitudeFromPressure(pressure_pa, temperature);
// Use GPS altitude as a reference to compute the baro bias measurement
const float baro_bias = pressure_altitude - gps_altitude;
float altitude = pressure_altitude - baro_bias;
// find pressure offset that aligns baro altitude with GPS via binary search
float front = -10000.f;
float middle = NAN;
float last = 10000.f;
float bias = NAN;
// perform a binary search
while (front <= last) {
middle = front + (last - front) / 2;
float altitude_calibrated = getAltitudeFromPressure(pressure_pa - middle, temperature);
if (altitude_calibrated > altitude + 0.1f) {
last = middle;
} else if (altitude_calibrated < altitude - 0.1f) {
front = middle;
} else {
bias = middle;
break;
}
}
if (PX4_ISFINITE(bias)) {
float offset = calibration[instance].BiasCorrectedSensorOffset(bias);
calibration[instance].set_offset(offset);
if (calibration[instance].ParametersSave(instance, true)) {
calibration[instance].PrintStatus();
param_save = true;
}
}
}
}
if (param_save) {
param_notify_changes();
}
calibration_log_info(mavlink_log_pub, CAL_QGC_DONE_MSG, sensor_name);
return PX4_OK;
}