mirror of
https://github.com/ArduPilot/ardupilot
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8caea96ab1
This makes it easier to setup the params. The ENABLE=2 value only takes effect at boot
425 lines
14 KiB
C++
425 lines
14 KiB
C++
/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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IMU temperature calibration handling
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*/
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#include "AP_InertialSensor.h"
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#if HAL_INS_TEMPERATURE_CAL_ENABLE
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#include <GCS_MAVLink/GCS.h>
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#include <AP_Logger/AP_Logger.h>
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// this scale factor ensures params are easy to work with in GUI parameter editors
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#define SCALE_FACTOR 1.0e6
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#define INV_SCALE_FACTOR 1.0e-6
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#define TEMP_RANGE_MIN 10
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extern const AP_HAL::HAL& hal;
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// temperature calibration parameters, per IMU
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const AP_Param::GroupInfo AP_InertialSensor::TCal::var_info[] = {
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// @Param: ENABLE
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// @DisplayName: Enable temperature calibration
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// @Description: Enable the use of temperature calibration parameters for this IMU. For automatic learning set to 2 and also set the INS_TCALn_TMAX to the target temperature, then reboot
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// @Values: 0:Disabled,1:Enabled,2:LearnCalibration
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// @User: Advanced
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// @RebootRequired: True
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AP_GROUPINFO_FLAGS("ENABLE", 1, AP_InertialSensor::TCal, enable, float(Enable::Disabled), AP_PARAM_FLAG_ENABLE),
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// @Param: TMIN
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// @DisplayName: Temperature calibration min
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// @Description: The minimum temperature that the calibration is valid for
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// @Range: -70 80
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// @Units: degC
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// @User: Advanced
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// @Calibration: 1
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AP_GROUPINFO("TMIN", 2, AP_InertialSensor::TCal, temp_min, 0),
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// @Param: TMAX
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// @DisplayName: Temperature calibration max
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// @Description: The maximum temperature that the calibration is valid for
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// @Range: -70 80
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// @Units: degC
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// @User: Advanced
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// @Calibration: 1
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AP_GROUPINFO("TMAX", 3, AP_InertialSensor::TCal, temp_max, 0),
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// @Param: ACC1_X
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// @DisplayName: Accelerometer 1st order temperature coefficient X axis
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// @Description: This is the 1st order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: ACC1_Y
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// @DisplayName: Accelerometer 1st order temperature coefficient Y axis
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// @Description: This is the 1st order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: ACC1_Z
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// @DisplayName: Accelerometer 1st order temperature coefficient Z axis
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// @Description: This is the 1st order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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AP_GROUPINFO("ACC1", 4, AP_InertialSensor::TCal, accel_coeff[0], 0),
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// @Param: ACC2_X
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// @DisplayName: Accelerometer 2nd order temperature coefficient X axis
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// @Description: This is the 2nd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: ACC2_Y
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// @DisplayName: Accelerometer 2nd order temperature coefficient Y axis
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// @Description: This is the 2nd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: ACC2_Z
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// @DisplayName: Accelerometer 2nd order temperature coefficient Z axis
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// @Description: This is the 2nd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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AP_GROUPINFO("ACC2", 5, AP_InertialSensor::TCal, accel_coeff[1], 0),
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// @Param: ACC3_X
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// @DisplayName: Accelerometer 3rd order temperature coefficient X axis
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// @Description: This is the 3rd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: ACC3_Y
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// @DisplayName: Accelerometer 3rd order temperature coefficient Y axis
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// @Description: This is the 3rd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: ACC3_Z
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// @DisplayName: Accelerometer 3rd order temperature coefficient Z axis
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// @Description: This is the 3rd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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AP_GROUPINFO("ACC3", 6, AP_InertialSensor::TCal, accel_coeff[2], 0),
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// @Param: GYR1_X
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// @DisplayName: Gyroscope 1st order temperature coefficient X axis
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// @Description: This is the 1st order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: GYR1_Y
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// @DisplayName: Gyroscope 1st order temperature coefficient Y axis
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// @Description: This is the 1st order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: GYR1_Z
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// @DisplayName: Gyroscope 1st order temperature coefficient Z axis
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// @Description: This is the 1st order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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AP_GROUPINFO("GYR1", 7, AP_InertialSensor::TCal, gyro_coeff[0], 0),
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// @Param: GYR2_X
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// @DisplayName: Gyroscope 2nd order temperature coefficient X axis
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// @Description: This is the 2nd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: GYR2_Y
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// @DisplayName: Gyroscope 2nd order temperature coefficient Y axis
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// @Description: This is the 2nd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: GYR2_Z
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// @DisplayName: Gyroscope 2nd order temperature coefficient Z axis
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// @Description: This is the 2nd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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AP_GROUPINFO("GYR2", 8, AP_InertialSensor::TCal, gyro_coeff[1], 0),
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// @Param: GYR3_X
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// @DisplayName: Gyroscope 3rd order temperature coefficient X axis
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// @Description: This is the 3rd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: GYR3_Y
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// @DisplayName: Gyroscope 3rd order temperature coefficient Y axis
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// @Description: This is the 3rd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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// @Param: GYR3_Z
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// @DisplayName: Gyroscope 3rd order temperature coefficient Z axis
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// @Description: This is the 3rd order temperature coefficient from a temperature calibration
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// @User: Advanced
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// @Calibration: 1
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AP_GROUPINFO("GYR3", 9, AP_InertialSensor::TCal, gyro_coeff[2], 0),
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AP_GROUPEND
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};
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/*
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evaluate a 3rd order polynomial (without the constant term) given a set of coefficients
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*/
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Vector3f AP_InertialSensor::TCal::polynomial_eval(float tdiff, const AP_Vector3f coeff[3]) const
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{
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// evaluate order 3 polynomial
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const Vector3f *c = (Vector3f *)&coeff[0];
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return (c[0] + (c[1] + c[2]*tdiff)*tdiff)*tdiff*INV_SCALE_FACTOR;
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}
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/*
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correct a single sensor for the current temperature
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*/
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void AP_InertialSensor::TCal::correct_sensor(float temperature, float cal_temp, const AP_Vector3f coeff[3], Vector3f &v) const
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{
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if (enable != Enable::Enabled) {
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return;
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}
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temperature = constrain_float(temperature, temp_min, temp_max);
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cal_temp = constrain_float(cal_temp, temp_min, temp_max);
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const float tmid = (temp_max + temp_min)*0.5;
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if (tmid <= 0) {
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return;
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}
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// get the polynomial correction for the difference between the
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// current temperature and the mid temperature
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v -= polynomial_eval(temperature - tmid, coeff);
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// we need to add the correction for the temperature
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// difference between the tmid, which is the reference used for
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// the calibration process, and the cal_temp, which is the
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// temperature that the offsets and scale factors was setup for
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v += polynomial_eval(cal_temp - tmid, coeff);
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}
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void AP_InertialSensor::TCal::correct_accel(float temperature, float cal_temp, Vector3f &accel) const
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{
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correct_sensor(temperature, cal_temp, accel_coeff, accel);
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}
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void AP_InertialSensor::TCal::correct_gyro(float temperature, float cal_temp, Vector3f &gyro) const
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{
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correct_sensor(temperature, cal_temp, gyro_coeff, gyro);
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}
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void AP_InertialSensor::TCal::sitl_apply_accel(float temperature, Vector3f &accel) const
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{
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Vector3f v;
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correct_sensor(temperature, 0.5*(temp_max+temp_min), accel_coeff, v);
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accel -= v;
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}
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void AP_InertialSensor::TCal::sitl_apply_gyro(float temperature, Vector3f &gyro) const
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{
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Vector3f v;
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correct_sensor(temperature, 0.5*(temp_max+temp_min), gyro_coeff, v);
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gyro -= v;
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}
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AP_InertialSensor::TCal::Learn::Learn(TCal &_tcal, float _start_temp) :
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start_temp(_start_temp),
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tcal(_tcal)
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{
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reset(_start_temp);
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}
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/*
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update polyfit with new sample
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*/
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void AP_InertialSensor::TCal::Learn::add_sample(const Vector3f &sample, float temperature, struct LearnState &st)
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{
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temperature = st.temp_filter.apply(temperature);
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st.sum += sample;
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st.sum_count++;
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if (st.sum_count < 100 ||
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temperature - st.last_temp < 0.5) {
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// wait for more data
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return;
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}
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st.sum /= st.sum_count;
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const uint8_t si = &st - &state[0];
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const float T = (temperature + st.last_temp) * 0.5;
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if (si == 0) {
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// we use the first accel sample as the zero baseline
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if (accel_start.is_zero()) {
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accel_start = st.sum;
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start_temp = T;
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}
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st.sum -= accel_start;
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}
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const float tmid = 0.5 * (tcal.temp_max + start_temp);
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const float tdiff = T - tmid;
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AP::logger().Write("TCLR", "TimeUS,I,Si,Temp,TDiff,X,Y,Z",
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"s#------",
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"F0000000",
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"QBBfffff",
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AP_HAL::micros64(),
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instance(),
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si,
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T,
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tdiff,
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st.sum.x, st.sum.y, st.sum.z);
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st.pfit[0].update(tdiff, st.sum.x);
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st.pfit[1].update(tdiff, st.sum.y);
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st.pfit[2].update(tdiff, st.sum.z);
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st.sum.zero();
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st.sum_count = 0;
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st.last_temp = temperature;
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if (!is_equal(start_tmax,tcal.temp_max.get())) {
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// user has changed the TMAX. This will give a bad result for
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// online learning as the reference temperature (tmid) will
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// change, so we need to start again
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reset(T);
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return;
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}
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if (temperature >= tcal.temp_max &&
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temperature - start_temp >= TEMP_RANGE_MIN) {
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finish_calibration(temperature);
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}
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}
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/*
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update accel temperature compensation learning
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*/
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void AP_InertialSensor::TCal::update_accel_learning(const Vector3f &accel, float temperature)
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{
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if (enable != Enable::LearnCalibration) {
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return;
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}
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if (learn == nullptr && hal.scheduler->is_system_initialized()) {
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learn = new Learn(*this, temperature);
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if (learn) {
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GCS_SEND_TEXT(MAV_SEVERITY_WARNING, "TCAL[%u]: started calibration t=%.1fC tmax=%.1fC",
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instance()+1,
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temperature, temp_max.get());
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AP_Notify::events.initiated_temp_cal = 1;
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}
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}
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if (learn != nullptr) {
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AP_Notify::flags.temp_cal_running = true;
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learn->add_sample(accel, temperature, learn->state[0]);
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}
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}
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/*
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update gyro temperature compensation learning
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*/
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void AP_InertialSensor::TCal::update_gyro_learning(const Vector3f &gyro, float temperature)
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{
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if (enable != Enable::LearnCalibration) {
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return;
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}
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if (learn != nullptr) {
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learn->add_sample(gyro, temperature, learn->state[1]);
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}
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}
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/*
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reset calibration
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*/
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void AP_InertialSensor::TCal::Learn::reset(float temperature)
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{
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memset(state, 0, sizeof(state));
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start_tmax = tcal.temp_max;
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accel_start.zero();
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for (uint8_t i=0; i<2; i++) {
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state[i].temp_filter.set_cutoff_frequency(1000, 0.5);
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state[i].temp_filter.reset(temperature);
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state[i].last_temp = temperature;
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}
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start_tmax = tcal.temp_max;
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}
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/*
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finish and save calibration
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*/
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void AP_InertialSensor::TCal::Learn::finish_calibration(float temperature)
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{
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Vector3f coefficients[3];
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for (uint8_t i=0; i<3; i++) {
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float p[4];
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if (!state[0].pfit[i].get_polynomial(p)) {
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GCS_SEND_TEXT(MAV_SEVERITY_WARNING, "TCAL[%u]: failed accel fit axis %u", instance()+1, i);
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AP_Notify::events.temp_cal_failed = 1;
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tcal.enable.set_and_save(int8_t(TCal::Enable::Disabled));
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return;
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}
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for (uint8_t k=0; k<3; k++) {
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coefficients[k][i] = p[2-k] * SCALE_FACTOR;
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}
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}
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for (uint8_t k=0; k<3; k++) {
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tcal.accel_coeff[k].set_and_save(coefficients[k]);
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}
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for (uint8_t i=0; i<3; i++) {
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float p[4];
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if (!state[1].pfit[i].get_polynomial(p)) {
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GCS_SEND_TEXT(MAV_SEVERITY_WARNING, "TCAL[%u]: failed gyro fit axis %u", tcal.instance()+1, i);
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AP_Notify::events.temp_cal_failed = 1;
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tcal.enable.set_and_save(int8_t(TCal::Enable::Disabled));
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return;
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}
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for (uint8_t k=0; k<3; k++) {
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coefficients[k][i] = p[2-k] * SCALE_FACTOR;
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}
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}
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for (uint8_t k=0; k<3; k++) {
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tcal.gyro_coeff[k].set_and_save(coefficients[k]);
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}
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tcal.temp_min.set_and_save(start_temp);
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GCS_SEND_TEXT(MAV_SEVERITY_WARNING, "TCAL[%u]: completed calibration tmin=%.1f tmax=%.1f",
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instance()+1,
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tcal.temp_min.get(), tcal.temp_max.get());
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tcal.enable.set_and_save(int8_t(TCal::Enable::Enabled));
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}
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uint8_t AP_InertialSensor::TCal::instance(void) const
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{
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return AP::ins().tcal_instance(*this);
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}
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#endif // HAL_INS_TEMPERATURE_CAL_ENABLE
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