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Copter: Autotune adjustments

This commit is contained in:
Leonard Hall 2015-04-15 22:09:12 +09:30 committed by Randy Mackay
parent 3659cd7359
commit 2b5fb850dd
1 changed files with 14 additions and 5 deletions
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19
ArduCopter/control_autotune.pde
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@ -69,8 +69,9 @@
#define AUTOTUNE_SP_MIN 0.5f // maximum Stab P value
#define AUTOTUNE_ACCEL_RP_BACKOFF 1.0f // back off from maximum acceleration
#define AUTOTUNE_ACCEL_Y_BACKOFF 0.75f // back off from maximum acceleration
#define AUTOTUNE_RP_ACCEL_MIN 75000.0f // Minimum acceleration for Roll and Pitch
#define AUTOTUNE_Y_ACCEL_MIN 18000.0f // Minimum acceleration for Roll and Pitch
#define AUTOTUNE_RP_ACCEL_MIN 54000.0f // Minimum acceleration for Roll and Pitch
#define AUTOTUNE_Y_ACCEL_MIN 18000.0f // Minimum acceleration for Yaw
#define AUTOTUNE_Y_FILT_FREQ 10.0f // Minimum acceleration for Roll and Pitch
#define AUTOTUNE_SUCCESS_COUNT 4 // how many successful iterations we need to freeze at current gains
#define AUTOTUNE_D_UP_DOWN_MARGIN 0.2f // The margin below the target that we tune D in
@ -381,7 +382,7 @@ static void autotune_attitude_control()
autotune_target_angle = constrain_float(attitude_control.max_angle_step_bf_roll(), AUTOTUNE_TARGET_MIN_ANGLE_RLLPIT_CD, AUTOTUNE_TARGET_ANGLE_RLLPIT_CD);
autotune_start_rate = ToDeg(ahrs.get_gyro().x) * 100.0f;
autotune_start_angle = ahrs.roll_sensor;
rotation_rate_filt.set_cutoff_frequency(MAIN_LOOP_SECONDS,g.pid_rate_roll.filt_hz()*4.0f);
rotation_rate_filt.set_cutoff_frequency(MAIN_LOOP_SECONDS,g.pid_rate_roll.filt_hz()*2.0f);
if ((autotune_state.tune_type == AUTOTUNE_TYPE_SP_DOWN) || (autotune_state.tune_type == AUTOTUNE_TYPE_SP_UP)) {
rotation_rate_filt.reset(autotune_start_rate);
} else {
@ -393,7 +394,7 @@ static void autotune_attitude_control()
autotune_target_angle = constrain_float(attitude_control.max_angle_step_bf_pitch(), AUTOTUNE_TARGET_MIN_ANGLE_RLLPIT_CD, AUTOTUNE_TARGET_ANGLE_RLLPIT_CD);
autotune_start_rate = ToDeg(ahrs.get_gyro().y) * 100.0f;
autotune_start_angle = ahrs.pitch_sensor;
rotation_rate_filt.set_cutoff_frequency(MAIN_LOOP_SECONDS,g.pid_rate_pitch.filt_hz()*4.0f);
rotation_rate_filt.set_cutoff_frequency(MAIN_LOOP_SECONDS,g.pid_rate_pitch.filt_hz()*2.0f);
if ((autotune_state.tune_type == AUTOTUNE_TYPE_SP_DOWN) || (autotune_state.tune_type == AUTOTUNE_TYPE_SP_UP)) {
rotation_rate_filt.reset(autotune_start_rate);
} else {
@ -405,7 +406,7 @@ static void autotune_attitude_control()
autotune_target_angle = constrain_float(attitude_control.max_angle_step_bf_yaw(), AUTOTUNE_TARGET_MIN_ANGLE_YAW_CD, AUTOTUNE_TARGET_ANGLE_YAW_CD);
autotune_start_rate = ToDeg(ahrs.get_gyro().z) * 100.0f;
autotune_start_angle = ahrs.yaw_sensor;
rotation_rate_filt.set_cutoff_frequency(MAIN_LOOP_SECONDS,orig_yaw_rLPF*4.0f);
rotation_rate_filt.set_cutoff_frequency(MAIN_LOOP_SECONDS,AUTOTUNE_Y_FILT_FREQ);
if ((autotune_state.tune_type == AUTOTUNE_TYPE_SP_DOWN) || (autotune_state.tune_type == AUTOTUNE_TYPE_SP_UP)) {
rotation_rate_filt.reset(autotune_start_rate);
} else {
@ -1120,6 +1121,10 @@ void autotune_updating_d_up(float &tune_d, float tune_d_min, float tune_d_max, f
// 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;
Log_Write_Event(DATA_AUTOTUNE_REACHED_LIMIT);
}
}else{
// we have a good measurement of bounce back
if (measurement_max-measurement_min > measurement_max*g.autotune_aggressiveness) {
@ -1171,6 +1176,10 @@ void autotune_updating_d_down(float &tune_d, float tune_d_min, float tune_d_step
// 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;
Log_Write_Event(DATA_AUTOTUNE_REACHED_LIMIT);
}
}else{
// we have a good measurement of bounce back
if (measurement_max-measurement_min < measurement_max*g.autotune_aggressiveness) {