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OP-1150 add code to calculate the thermal calibration coefficients for baro, gyro and accel

This commit is contained in:
Alessio Morale 2014-01-08 00:01:00 +01:00
parent 78f77e8d3f
commit ecaaf84a79
3 changed files with 202 additions and 0 deletions

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/**
******************************************************************************
*
* @file thermalcalibration.h
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2014.
*
* @brief Thermal calibration algorithms
* @see The GNU Public License (GPL) Version 3
* @defgroup
* @{
*
*****************************************************************************/
/*
* This program is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 3 of the License, or
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
* for more details.
*
* You should have received a copy of the GNU General Public License along
* with this program; if not, write to the Free Software Foundation, Inc.,
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
*/
#include "thermalcalibration.h"
#include "QDebug"
using namespace OpenPilot;
bool ThermalCalibration::BarometerCalibration(Eigen::VectorXf pressure, Eigen::VectorXf temperature, float *result)
{
// assume the nearest reading to 20°C as the "zero bias" point
int index20deg = searchReferenceValue(20.0f, temperature);
qDebug() << "Ref zero is " << index20deg << " T: " << temperature[index20deg] << " P:" << pressure[index20deg];
float refZero = pressure[index20deg];
pressure.array() -= refZero;
qDebug() << "Rebased zero is " << pressure[index20deg];
Eigen::VectorXf solution(BARO_PRESSURE_POLY_DEGREE + 1);
if(!CalibrationUtils::PolynomialCalibration(temperature, pressure, BARO_PRESSURE_POLY_DEGREE, solution)){
return false;
}
copyToArray(result, solution, BARO_PRESSURE_POLY_DEGREE + 1);
return true;
}
bool ThermalCalibration::AccelerometerCalibration(Eigen::VectorXf samplesX, Eigen::VectorXf samplesY, Eigen::VectorXf samplesZ, Eigen::VectorXf temperature, float *result)
{
Eigen::VectorXf solution(ACCEL_X_POLY_DEGREE + 1);
if(!CalibrationUtils::PolynomialCalibration(temperature, samplesX, ACCEL_X_POLY_DEGREE, solution)){
return false;
}
result[0] = solution[1];
solution.resize(ACCEL_Y_POLY_DEGREE + 1);
if(!CalibrationUtils::PolynomialCalibration(temperature, samplesY, ACCEL_Y_POLY_DEGREE, solution)){
return false;
}
result[1] = solution[1];
solution.resize(ACCEL_Z_POLY_DEGREE + 1);
if(!CalibrationUtils::PolynomialCalibration(temperature, samplesZ, ACCEL_Z_POLY_DEGREE, solution)){
return false;
}
result[2] = solution[1];
return true;
}
bool ThermalCalibration::GyroscopeCalibration(Eigen::VectorXf samplesX, Eigen::VectorXf samplesY, Eigen::VectorXf samplesZ, Eigen::VectorXf temperature, float *result)
{
Eigen::VectorXf solution(GYRO_X_POLY_DEGREE + 1);
if(!CalibrationUtils::PolynomialCalibration(temperature, samplesX, GYRO_X_POLY_DEGREE, solution)){
return false;
}
result[0] = solution[1];
std::cout << solution << std::endl << std::endl;
solution.resize(GYRO_Y_POLY_DEGREE + 1);
if(!CalibrationUtils::PolynomialCalibration(temperature, samplesY, GYRO_Y_POLY_DEGREE, solution)){
return false;
}
result[1] = solution[1];
std::cout << solution << std::endl << std::endl;
solution.resize(GYRO_Z_POLY_DEGREE + 1);
if(!CalibrationUtils::PolynomialCalibration(temperature, samplesZ, GYRO_Z_POLY_DEGREE, solution)){
return false;
}
result[2] = solution[1];
result[3] = solution[2];
std::cout << solution << std::endl;
return true;
}
void ThermalCalibration::copyToArray(float *result, Eigen::VectorXf solution, int elements)
{
for(int i = 0; i < elements; i++){
result[i] = solution[i];
}
}
int ThermalCalibration::searchReferenceValue(float value, Eigen::VectorXf values){
for(int i = 0; i < values.size(); i++){
if(!(values[i] < value)){
return i;
}
}
return values.size() - 1;
}
ThermalCalibration::ThermalCalibration()
{
}

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/**
******************************************************************************
*
* @file thermalcalibration.c
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2014.
*
* @brief Barometer, Gyroscope and Accelerometer thermal calibration algorithms
* @see The GNU Public License (GPL) Version 3
* @defgroup
* @{
*
*****************************************************************************/
/*
* This program is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 3 of the License, or
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
* for more details.
*
* You should have received a copy of the GNU General Public License along
* with this program; if not, write to the Free Software Foundation, Inc.,
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
*/
#ifndef THERMALCALIBRATION_H
#define THERMALCALIBRATION_H
#include "calibrationutils.h"
namespace OpenPilot {
class ThermalCalibration {
static const int GYRO_X_POLY_DEGREE = 1;
static const int GYRO_Y_POLY_DEGREE = 1;
static const int GYRO_Z_POLY_DEGREE = 2;
static const int ACCEL_X_POLY_DEGREE = 1;
static const int ACCEL_Y_POLY_DEGREE = 1;
static const int ACCEL_Z_POLY_DEGREE = 1;
static const int BARO_PRESSURE_POLY_DEGREE = 3;
public:
/**
* @brief produce the calibration polinomial coefficients from pressure and temperature samples
* @param pressure Pressure samples
* @param temperature Temperature samples
* @param result Polinomial coefficients to be sent to board (x0, x1, x2, x3)
* @return
*/
static bool BarometerCalibration(Eigen::VectorXf pressure, Eigen::VectorXf temperature, float *result);
/**
* @brief AccelerometerCalibration produce the calibration polinomial coefficients from accelerometer axis and temperature samples
* @param pressure
* @param temperature
* @param result a float[3] array containing value to populate calibration settings (x,y,z)
* @return
*/
static bool AccelerometerCalibration(Eigen::VectorXf samplesX, Eigen::VectorXf samplesY, Eigen::VectorXf samplesZ, Eigen::VectorXf temperature, float *result);
/**
* @brief GyroscopeCalibration produce the calibration polinomial coefficients from gyroscopes axis and temperature samples
* @param samplesX
* @param samplesY
* @param samplesZ
* @param temperature
* @param result a float[4] array containing value to populate calibration settings (x,y,z1, z2)
* @return
*/
static bool GyroscopeCalibration(Eigen::VectorXf samplesX, Eigen::VectorXf samplesY, Eigen::VectorXf samplesZ, Eigen::VectorXf temperature, float *result);
private:
static void copyToArray(float *result, Eigen::VectorXf solution, int elements);
ThermalCalibration();
static int searchReferenceValue(float value, Eigen::VectorXf values);
};
}
#endif // THERMALCALIBRATION_H

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@ -41,6 +41,7 @@ HEADERS += configplugin.h \
dblspindelegate.h \
configrevohwwidget.h \
calibration/calibrationutils.h \
calibration/thermalcalibration.h
SOURCES += configplugin.cpp \
configgadgetwidget.cpp \
@ -75,6 +76,7 @@ SOURCES += configplugin.cpp \
dblspindelegate.cpp \
configrevohwwidget.cpp \
calibration/calibrationutils.cpp \
calibration/thermalcalibration.cpp
FORMS += airframe.ui \
airframe_ccpm.ui \