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ardupilot/libraries/AC_AutoTune/AC_AutoTune_Multi.cpp

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/*
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, see <http://www.gnu.org/licenses/>.
*/
/*
support for autotune of multirotors. Based on original autotune code from ArduCopter, written by Leonard Hall
Converted to a library by Andrew Tridgell
*/
#define AUTOTUNE_FFI_RATIO_FOR_TESTING 0.5f // I is set 2x smaller than VFF during testing
#define AUTOTUNE_FFI_RATIO_FINAL 0.5f // I is set 0.5x VFF after testing
#define AUTOTUNE_PI_RATIO_FINAL 1.0f // I is set 1x P after testing
#define AUTOTUNE_YAW_PI_RATIO_FINAL 0.1f // I is set 1x P after testing
#define AUTOTUNE_RD_STEP 0.05f // minimum increment when increasing/decreasing Rate D term
#define AUTOTUNE_RP_STEP 0.05f // minimum increment when increasing/decreasing Rate P term
#define AUTOTUNE_SP_STEP 0.05f // minimum increment when increasing/decreasing Stab P term
#define AUTOTUNE_PI_RATIO_FOR_TESTING 0.1f // I is set 10x smaller than P during testing
#define AUTOTUNE_RD_MAX 0.200f // maximum Rate D value
#define AUTOTUNE_RLPF_MIN 1.0f // minimum Rate Yaw filter value
#define AUTOTUNE_RLPF_MAX 5.0f // maximum Rate Yaw filter value
#define AUTOTUNE_RP_MIN 0.01f // minimum Rate P value
#define AUTOTUNE_RP_MAX 2.0f // maximum Rate P value
#define AUTOTUNE_SP_MAX 20.0f // maximum Stab P value
#define AUTOTUNE_SP_MIN 0.5f // maximum Stab P value
#define AUTOTUNE_D_UP_DOWN_MARGIN 0.2f // The margin below the target that we tune D in
#include "AC_AutoTune_Multi.h"
// constructor
AC_AutoTune_Multi::AC_AutoTune_Multi()
{
tune_seq[0] = RD_UP;
tune_seq[1] = RD_DOWN;
tune_seq[2] = RP_UP;
tune_seq[3] = SP_DOWN;
tune_seq[4] = SP_UP;
tune_seq[5] = TUNE_COMPLETE;
}
void AC_AutoTune_Multi::do_gcs_announcements()
{
const uint32_t now = AP_HAL::millis();
if (now - announce_time < AUTOTUNE_ANNOUNCE_INTERVAL_MS) {
return;
}
float tune_rp = 0.0f;
float tune_rd = 0.0f;
float tune_sp = 0.0f;
float tune_accel = 0.0f;
char axis_char = '?';
switch (axis) {
case ROLL:
tune_rp = tune_roll_rp;
tune_rd = tune_roll_rd;
tune_sp = tune_roll_sp;
tune_accel = tune_roll_accel;
axis_char = 'R';
break;
case PITCH:
tune_rp = tune_pitch_rp;
tune_rd = tune_pitch_rd;
tune_sp = tune_pitch_sp;
tune_accel = tune_pitch_accel;
axis_char = 'P';
break;
case YAW:
tune_rp = tune_yaw_rp;
tune_rd = tune_yaw_rLPF;
tune_sp = tune_yaw_sp;
tune_accel = tune_yaw_accel;
axis_char = 'Y';
break;
}
gcs().send_text(MAV_SEVERITY_INFO, "AutoTune: (%c) %s", axis_char, type_string());
send_step_string();
if (!is_zero(lean_angle)) {
gcs().send_text(MAV_SEVERITY_INFO, "AutoTune: lean=%f target=%f", (double)lean_angle, (double)target_angle);
}
if (!is_zero(rotation_rate)) {
gcs().send_text(MAV_SEVERITY_INFO, "AutoTune: rotation=%f target=%f", (double)(rotation_rate*0.01f), (double)(target_rate*0.01f));
}
switch (tune_type) {
case RD_UP:
case RD_DOWN:
case RP_UP:
case RP_DOWN:
gcs().send_text(MAV_SEVERITY_INFO, "AutoTune: p=%f d=%f", (double)tune_rp, (double)tune_rd);
break;
case RFF_UP:
case RFF_DOWN:
break;
case SP_DOWN:
case SP_UP:
gcs().send_text(MAV_SEVERITY_INFO, "AutoTune: p=%f accel=%f", (double)tune_sp, (double)tune_accel);
break;
case MAX_GAINS:
case TUNE_COMPLETE:
break;
}
gcs().send_text(MAV_SEVERITY_INFO, "AutoTune: success %u/%u", counter, AUTOTUNE_SUCCESS_COUNT);
announce_time = now;
}
void AC_AutoTune_Multi::test_init()
{
twitch_test_init();
}
void AC_AutoTune_Multi::test_run(AxisType test_axis, const float dir_sign)
{
twitch_test_run(test_axis, dir_sign);
}
// load_test_gains - load the to-be-tested gains for a single axis
// called by control_attitude() just before it beings testing a gain (i.e. just before it twitches)
void AC_AutoTune_Multi::load_test_gains()
{
AC_AutoTune::load_test_gains();
switch (axis) {
case ROLL:
attitude_control->get_rate_roll_pid().kI(tune_roll_rp*0.01f);
attitude_control->get_rate_roll_pid().ff(0.0f);
attitude_control->get_rate_roll_pid().filt_T_hz(0.0f);
attitude_control->get_rate_roll_pid().slew_limit(0.0f);
break;
case PITCH:
attitude_control->get_rate_pitch_pid().kI(tune_pitch_rp*0.01f);
attitude_control->get_rate_pitch_pid().ff(0.0f);
attitude_control->get_rate_pitch_pid().filt_T_hz(0.0f);
attitude_control->get_rate_pitch_pid().slew_limit(0.0f);
break;
case YAW:
attitude_control->get_rate_yaw_pid().kI(tune_yaw_rp*0.01f);
attitude_control->get_rate_yaw_pid().kD(0.0f);
attitude_control->get_rate_yaw_pid().ff(0.0f);
attitude_control->get_rate_yaw_pid().filt_T_hz(0.0f);
attitude_control->get_rate_yaw_pid().slew_limit(0.0f);
break;
}
}
// save_tuning_gains - save the final tuned gains for each axis
// save discovered gains to eeprom if autotuner is enabled (i.e. switch is in the high position)
void AC_AutoTune_Multi::save_tuning_gains()
{
AC_AutoTune::save_tuning_gains();
// sanity check the rate P values
if ((axes_completed & AUTOTUNE_AXIS_BITMASK_ROLL) && roll_enabled() && !is_zero(tune_roll_rp)) {
// rate roll gains
attitude_control->get_rate_roll_pid().ff(orig_roll_rff);
attitude_control->get_rate_roll_pid().filt_T_hz(orig_roll_fltt);
attitude_control->get_rate_roll_pid().slew_limit(orig_roll_smax);
attitude_control->get_rate_roll_pid().kI(tune_roll_rp*AUTOTUNE_PI_RATIO_FINAL);
attitude_control->get_rate_roll_pid().save_gains();
// resave pids to originals in case the autotune is run again
orig_roll_rff = attitude_control->get_rate_roll_pid().ff();
orig_roll_ri = attitude_control->get_rate_roll_pid().kI();
}
if ((axes_completed & AUTOTUNE_AXIS_BITMASK_PITCH) && pitch_enabled() && !is_zero(tune_pitch_rp)) {
// rate pitch gains
attitude_control->get_rate_pitch_pid().ff(orig_pitch_rff);
attitude_control->get_rate_pitch_pid().filt_T_hz(orig_pitch_fltt);
attitude_control->get_rate_pitch_pid().slew_limit(orig_pitch_smax);
attitude_control->get_rate_pitch_pid().kI(tune_pitch_rp*AUTOTUNE_PI_RATIO_FINAL);
attitude_control->get_rate_pitch_pid().save_gains();
// resave pids to originals in case the autotune is run again
orig_pitch_rff = attitude_control->get_rate_pitch_pid().ff();
orig_pitch_ri = attitude_control->get_rate_pitch_pid().kI();
}
if ((axes_completed & AUTOTUNE_AXIS_BITMASK_YAW) && yaw_enabled() && !is_zero(tune_yaw_rp)) {
// rate yaw gains
attitude_control->get_rate_yaw_pid().kD(0.0f);
attitude_control->get_rate_yaw_pid().ff(orig_yaw_rff);
attitude_control->get_rate_yaw_pid().filt_T_hz(orig_yaw_fltt);
attitude_control->get_rate_yaw_pid().slew_limit(orig_yaw_smax);
attitude_control->get_rate_yaw_pid().filt_E_hz(tune_yaw_rLPF);
attitude_control->get_rate_yaw_pid().kI(tune_yaw_rp*AUTOTUNE_YAW_PI_RATIO_FINAL);
attitude_control->get_rate_yaw_pid().save_gains();
// resave pids to originals in case the autotune is run again
orig_yaw_rd = attitude_control->get_rate_yaw_pid().kD();
orig_yaw_rLPF = attitude_control->get_rate_yaw_pid().filt_E_hz();
orig_yaw_rff = attitude_control->get_rate_yaw_pid().ff();
orig_yaw_ri = attitude_control->get_rate_yaw_pid().kI();
}
// update GCS and log save gains event
update_gcs(AUTOTUNE_MESSAGE_SAVED_GAINS);
AP::logger().Write_Event(LogEvent::AUTOTUNE_SAVEDGAINS);
reset();
}
// update gains for the rate p up tune type
void AC_AutoTune_Multi::updating_rate_p_up_all(AxisType test_axis)
{
switch (test_axis) {
case ROLL:
updating_rate_p_up_d_down(tune_roll_rd, min_d, AUTOTUNE_RD_STEP, tune_roll_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
case PITCH:
updating_rate_p_up_d_down(tune_pitch_rd, min_d, AUTOTUNE_RD_STEP, tune_pitch_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
case YAW:
updating_rate_p_up_d_down(tune_yaw_rLPF, AUTOTUNE_RLPF_MIN, AUTOTUNE_RD_STEP, tune_yaw_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
}
}
// update gains for the rate d up tune type
void AC_AutoTune_Multi::updating_rate_d_up_all(AxisType test_axis)
{
switch (test_axis) {
case ROLL:
updating_rate_d_up(tune_roll_rd, min_d, AUTOTUNE_RD_MAX, AUTOTUNE_RD_STEP, tune_roll_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
case PITCH:
updating_rate_d_up(tune_pitch_rd, min_d, AUTOTUNE_RD_MAX, AUTOTUNE_RD_STEP, tune_pitch_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
case YAW:
updating_rate_d_up(tune_yaw_rLPF, AUTOTUNE_RLPF_MIN, AUTOTUNE_RLPF_MAX, AUTOTUNE_RD_STEP, tune_yaw_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
}
}
// update gains for the rate d down tune type
void AC_AutoTune_Multi::updating_rate_d_down_all(AxisType test_axis)
{
switch (test_axis) {
case ROLL:
updating_rate_d_down(tune_roll_rd, min_d, AUTOTUNE_RD_STEP, tune_roll_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
case PITCH:
updating_rate_d_down(tune_pitch_rd, min_d, AUTOTUNE_RD_STEP, tune_pitch_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
case YAW:
updating_rate_d_down(tune_yaw_rLPF, AUTOTUNE_RLPF_MIN, AUTOTUNE_RD_STEP, tune_yaw_rp, AUTOTUNE_RP_MIN, AUTOTUNE_RP_MAX, AUTOTUNE_RP_STEP, target_rate, test_rate_min, test_rate_max);
break;
}
}
// update gains for the angle p up tune type
void AC_AutoTune_Multi::updating_angle_p_up_all(AxisType test_axis)
{
switch (test_axis) {
case ROLL:
updating_angle_p_up(tune_roll_sp, AUTOTUNE_SP_MAX, AUTOTUNE_SP_STEP, target_angle, test_angle_max, test_rate_min, test_rate_max);
break;
case PITCH:
updating_angle_p_up(tune_pitch_sp, AUTOTUNE_SP_MAX, AUTOTUNE_SP_STEP, target_angle, test_angle_max, test_rate_min, test_rate_max);
break;
case YAW:
updating_angle_p_up(tune_yaw_sp, AUTOTUNE_SP_MAX, AUTOTUNE_SP_STEP, target_angle, test_angle_max, test_rate_min, test_rate_max);
break;
}
}
// update gains for the angle p down tune type
void AC_AutoTune_Multi::updating_angle_p_down_all(AxisType test_axis)
{
switch (test_axis) {
case ROLL:
updating_angle_p_down(tune_roll_sp, AUTOTUNE_SP_MIN, AUTOTUNE_SP_STEP, target_angle, test_angle_max, test_rate_min, test_rate_max);
break;
case PITCH:
updating_angle_p_down(tune_pitch_sp, AUTOTUNE_SP_MIN, AUTOTUNE_SP_STEP, target_angle, test_angle_max, test_rate_min, test_rate_max);
break;
case YAW:
updating_angle_p_down(tune_yaw_sp, AUTOTUNE_SP_MIN, AUTOTUNE_SP_STEP, target_angle, test_angle_max, test_rate_min, test_rate_max);
break;
}
}
// updating_rate_d_up - increase D and adjust P to optimize the D term for a little bounce back
// optimize D term while keeping the maximum just below the target by adjusting P
void AC_AutoTune_Multi::updating_rate_d_up(float &tune_d, float tune_d_min, float tune_d_max, float tune_d_step_ratio, float &tune_p, float tune_p_min, float tune_p_max, float tune_p_step_ratio, float rate_target, float meas_rate_min, float meas_rate_max)
{
if (meas_rate_max > rate_target) {
// if maximum measurement was higher than target
// reduce P gain (which should reduce maximum)
tune_p -= tune_p*tune_p_step_ratio;
if (tune_p < tune_p_min) {
// P gain is at minimum so start reducing D
tune_p = tune_p_min;
tune_d -= tune_d*tune_d_step_ratio;
if (tune_d <= tune_d_min) {
// We have reached minimum D gain so stop tuning
tune_d = tune_d_min;
counter = AUTOTUNE_SUCCESS_COUNT;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
}
} else if ((meas_rate_max < rate_target*(1.0f-AUTOTUNE_D_UP_DOWN_MARGIN)) && (tune_p <= tune_p_max)) {
// we have not achieved a high enough maximum to get a good measurement of bounce back.
// increase P gain (which should increase maximum)
tune_p += tune_p*tune_p_step_ratio;
if (tune_p >= tune_p_max) {
tune_p = tune_p_max;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
} else {
// we have a good measurement of bounce back
if (meas_rate_max-meas_rate_min > meas_rate_max*aggressiveness) {
// ignore the next result unless it is the same as this one
ignore_next = true;
// bounce back is bigger than our threshold so increment the success counter
counter++;
} else {
if (ignore_next == false) {
// bounce back is smaller than our threshold so decrement the success counter
if (counter > 0) {
counter--;
}
// increase D gain (which should increase bounce back)
tune_d += tune_d*tune_d_step_ratio*2.0f;
// stop tuning if we hit maximum D
if (tune_d >= tune_d_max) {
tune_d = tune_d_max;
counter = AUTOTUNE_SUCCESS_COUNT;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
} else {
ignore_next = false;
}
}
}
}
// updating_rate_d_down - decrease D and adjust P to optimize the D term for no bounce back
// optimize D term while keeping the maximum just below the target by adjusting P
void AC_AutoTune_Multi::updating_rate_d_down(float &tune_d, float tune_d_min, float tune_d_step_ratio, float &tune_p, float tune_p_min, float tune_p_max, float tune_p_step_ratio, float rate_target, float meas_rate_min, float meas_rate_max)
{
if (meas_rate_max > rate_target) {
// if maximum measurement was higher than target
// reduce P gain (which should reduce maximum)
tune_p -= tune_p*tune_p_step_ratio;
if (tune_p < tune_p_min) {
// P gain is at minimum so start reducing D gain
tune_p = tune_p_min;
tune_d -= tune_d*tune_d_step_ratio;
if (tune_d <= tune_d_min) {
// We have reached minimum D so stop tuning
tune_d = tune_d_min;
counter = AUTOTUNE_SUCCESS_COUNT;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
}
} else if ((meas_rate_max < rate_target*(1.0f-AUTOTUNE_D_UP_DOWN_MARGIN)) && (tune_p <= tune_p_max)) {
// we have not achieved a high enough maximum to get a good measurement of bounce back.
// increase P gain (which should increase maximum)
tune_p += tune_p*tune_p_step_ratio;
if (tune_p >= tune_p_max) {
tune_p = tune_p_max;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
} else {
// we have a good measurement of bounce back
if (meas_rate_max-meas_rate_min < meas_rate_max*aggressiveness) {
if (ignore_next == false) {
// bounce back is less than our threshold so increment the success counter
counter++;
} else {
ignore_next = false;
}
} else {
// ignore the next result unless it is the same as this one
ignore_next = true;
// bounce back is larger than our threshold so decrement the success counter
if (counter > 0) {
counter--;
}
// decrease D gain (which should decrease bounce back)
tune_d -= tune_d*tune_d_step_ratio;
// stop tuning if we hit minimum D
if (tune_d <= tune_d_min) {
tune_d = tune_d_min;
counter = AUTOTUNE_SUCCESS_COUNT;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
}
}
}
// updating_rate_p_up_d_down - increase P to ensure the target is reached while checking bounce back isn't increasing
// P is increased until we achieve our target within a reasonable time while reducing D if bounce back increases above the threshold
void AC_AutoTune_Multi::updating_rate_p_up_d_down(float &tune_d, float tune_d_min, float tune_d_step_ratio, float &tune_p, float tune_p_min, float tune_p_max, float tune_p_step_ratio, float rate_target, float meas_rate_min, float meas_rate_max)
{
if (meas_rate_max > rate_target*(1+0.5f*aggressiveness)) {
// ignore the next result unless it is the same as this one
ignore_next = true;
// if maximum measurement was greater than target so increment the success counter
counter++;
} else if ((meas_rate_max < rate_target) && (meas_rate_max > rate_target*(1.0f-AUTOTUNE_D_UP_DOWN_MARGIN)) && (meas_rate_max-meas_rate_min > meas_rate_max*aggressiveness) && (tune_d > tune_d_min)) {
// if bounce back was larger than the threshold so decrement the success counter
if (counter > 0) {
counter--;
}
// decrease D gain (which should decrease bounce back)
tune_d -= tune_d*tune_d_step_ratio;
// do not decrease the D term past the minimum
if (tune_d <= tune_d_min) {
tune_d = tune_d_min;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
// decrease P gain to match D gain reduction
tune_p -= tune_p*tune_p_step_ratio;
// do not decrease the P term past the minimum
if (tune_p <= tune_p_min) {
tune_p = tune_p_min;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
// cancel change in direction
positive_direction = !positive_direction;
} else {
if (ignore_next == false) {
// if maximum measurement was lower than target so decrement the success counter
if (counter > 0) {
counter--;
}
// increase P gain (which should increase the maximum)
tune_p += tune_p*tune_p_step_ratio;
// stop tuning if we hit maximum P
if (tune_p >= tune_p_max) {
tune_p = tune_p_max;
counter = AUTOTUNE_SUCCESS_COUNT;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
} else {
ignore_next = false;
}
}
}
// updating_angle_p_down - decrease P until we don't reach the target before time out
// P is decreased to ensure we are not overshooting the target
void AC_AutoTune_Multi::updating_angle_p_down(float &tune_p, float tune_p_min, float tune_p_step_ratio, float angle_target, float meas_angle_max, float meas_rate_min, float meas_rate_max)
{
if (meas_angle_max < angle_target*(1+0.5f*aggressiveness)) {
if (ignore_next == false) {
// if maximum measurement was lower than target so increment the success counter
counter++;
} else {
ignore_next = false;
}
} else {
// ignore the next result unless it is the same as this one
ignore_next = true;
// if maximum measurement was higher than target so decrement the success counter
if (counter > 0) {
counter--;
}
// decrease P gain (which should decrease the maximum)
tune_p -= tune_p*tune_p_step_ratio;
// stop tuning if we hit maximum P
if (tune_p <= tune_p_min) {
tune_p = tune_p_min;
counter = AUTOTUNE_SUCCESS_COUNT;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
}
}
// updating_angle_p_up - increase P to ensure the target is reached
// P is increased until we achieve our target within a reasonable time
void AC_AutoTune_Multi::updating_angle_p_up(float &tune_p, float tune_p_max, float tune_p_step_ratio, float angle_target, float meas_angle_max, float meas_rate_min, float meas_rate_max)
{
if ((meas_angle_max > angle_target*(1+0.5f*aggressiveness)) ||
((meas_angle_max > angle_target) && (meas_rate_min < -meas_rate_max*aggressiveness))) {
// ignore the next result unless it is the same as this one
ignore_next = true;
// if maximum measurement was greater than target so increment the success counter
counter++;
} else {
if (ignore_next == false) {
// if maximum measurement was lower than target so decrement the success counter
if (counter > 0) {
counter--;
}
// increase P gain (which should increase the maximum)
tune_p += tune_p*tune_p_step_ratio;
// stop tuning if we hit maximum P
if (tune_p >= tune_p_max) {
tune_p = tune_p_max;
counter = AUTOTUNE_SUCCESS_COUNT;
AP::logger().Write_Event(LogEvent::AUTOTUNE_REACHED_LIMIT);
}
} else {
ignore_next = false;
}
}
}
void AC_AutoTune_Multi::Log_AutoTune()
{
if ((tune_type == SP_DOWN) || (tune_type == SP_UP)) {
switch (axis) {
case ROLL:
Log_Write_AutoTune(axis, tune_type, target_angle, test_angle_min, test_angle_max, tune_roll_rp, tune_roll_rd, tune_roll_sp, test_accel_max);
break;
case PITCH:
Log_Write_AutoTune(axis, tune_type, target_angle, test_angle_min, test_angle_max, tune_pitch_rp, tune_pitch_rd, tune_pitch_sp, test_accel_max);
break;
case YAW:
Log_Write_AutoTune(axis, tune_type, target_angle, test_angle_min, test_angle_max, tune_yaw_rp, tune_yaw_rLPF, tune_yaw_sp, test_accel_max);
break;
}
} else {
switch (axis) {
case ROLL:
Log_Write_AutoTune(axis, tune_type, target_rate, test_rate_min, test_rate_max, tune_roll_rp, tune_roll_rd, tune_roll_sp, test_accel_max);
break;
case PITCH:
Log_Write_AutoTune(axis, tune_type, target_rate, test_rate_min, test_rate_max, tune_pitch_rp, tune_pitch_rd, tune_pitch_sp, test_accel_max);
break;
case YAW:
Log_Write_AutoTune(axis, tune_type, target_rate, test_rate_min, test_rate_max, tune_yaw_rp, tune_yaw_rLPF, tune_yaw_sp, test_accel_max);
break;
}
}
}
void AC_AutoTune_Multi::Log_AutoTuneDetails()
{
Log_Write_AutoTuneDetails(lean_angle, rotation_rate);
}
// @LoggerMessage: ATUN
// @Description: Copter/QuadPlane AutoTune
// @Vehicles: Copter, Plane
// @Field: TimeUS: Time since system startup
// @Field: Axis: which axis is currently being tuned
// @Field: TuneStep: step in autotune process
// @Field: Targ: target angle or rate, depending on tuning step
// @Field: Min: measured minimum target angle or rate
// @Field: Max: measured maximum target angle or rate
// @Field: RP: new rate gain P term
// @Field: RD: new rate gain D term
// @Field: SP: new angle P term
// @Field: ddt: maximum measured twitching acceleration
// Write an Autotune data packet
void AC_AutoTune_Multi::Log_Write_AutoTune(uint8_t _axis, uint8_t tune_step, float meas_target, float meas_min, float meas_max, float new_gain_rp, float new_gain_rd, float new_gain_sp, float new_ddt)
{
AP::logger().Write(
"ATUN",
"TimeUS,Axis,TuneStep,Targ,Min,Max,RP,RD,SP,ddt",
"s--ddd---o",
"F--000---0",
"QBBfffffff",
AP_HAL::micros64(),
axis,
tune_step,
meas_target*0.01f,
meas_min*0.01f,
meas_max*0.01f,
new_gain_rp,
new_gain_rd,
new_gain_sp,
new_ddt);
}
// Write an Autotune data packet
void AC_AutoTune_Multi::Log_Write_AutoTuneDetails(float angle_cd, float rate_cds)
{
// @LoggerMessage: ATDE
// @Description: AutoTune data packet
// @Field: TimeUS: Time since system startup
// @Field: Angle: current angle
// @Field: Rate: current angular rate
AP::logger().WriteStreaming(
"ATDE",
"TimeUS,Angle,Rate",
"sdk",
"F00",
"Qff",
AP_HAL::micros64(),
angle_cd*0.01f,
rate_cds*0.01f);
}
// get intra test rate I gain for the specified axis
float AC_AutoTune_Multi::get_intra_test_ri(AxisType test_axis)
{
float ret = 0.0f;
switch (test_axis) {
case ROLL:
ret = orig_roll_rp * AUTOTUNE_PI_RATIO_FOR_TESTING;
break;
case PITCH:
ret = orig_pitch_rp * AUTOTUNE_PI_RATIO_FOR_TESTING;
break;
case YAW:
ret = orig_yaw_rp * AUTOTUNE_PI_RATIO_FOR_TESTING;
break;
}
return ret;
}
// get tuned rate I gain for the specified axis
float AC_AutoTune_Multi::get_tuned_ri(AxisType test_axis)
{
float ret = 0.0f;
switch (test_axis) {
case ROLL:
ret = tune_roll_rp*AUTOTUNE_PI_RATIO_FINAL;
break;
case PITCH:
ret = tune_pitch_rp*AUTOTUNE_PI_RATIO_FINAL;
break;
case YAW:
ret = tune_yaw_rp*AUTOTUNE_PI_RATIO_FINAL;
break;
}
return ret;
}
// get minimum rate P (for any axis)
float AC_AutoTune_Multi::get_rp_min() const
{
return AUTOTUNE_RP_MIN;
}
// get minimum angle P (for any axis)
float AC_AutoTune_Multi::get_sp_min() const
{
return AUTOTUNE_SP_MIN;
}
// get minimum rate Yaw filter value
float AC_AutoTune_Multi::get_yaw_rate_filt_min() const
{
return AUTOTUNE_RLPF_MIN;
}