mirror of https://github.com/ArduPilot/ardupilot
585 lines
29 KiB
Plaintext
585 lines
29 KiB
Plaintext
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#if AUTOTUNE == ENABLED
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/*
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Auto tuning works in this way:
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i) set up 3-position ch7 or ch8 switch to "AutoTune"
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2) take-off in stabilize mode, put the copter into a level hover and switch ch7/ch8 to high position to start tuning
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3) auto tuner brings roll and pitch level
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4) the following procedure is run for roll and then pitch
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a) invokes 90 deg/sec rate request
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b) records maximum "forward" roll rate and bounce back rate
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c) when copter reaches 20 degrees or 1 second has passed, it commands level
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d) tries to keep max rotation rate between 80% ~ 100% of requested rate (90deg/sec) by adjusting rate P
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e) increases rate D until the bounce back becomes greater than 10% of requested rate (90deg/sec)
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f) decreases rate D until the bounce back becomes less than 10% of requested rate (90deg/sec)
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g) increases rate P until the max rotate rate becomes greater than the requeste rate (90deg/sec)
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h) invokes a 20deg angle request on roll or pitch
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i) increases stab P until the maximum angle becomes greater than 110% of the requested angle (20deg)
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j) decreases stab P by 25%
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If pilot inputs any stick inputs these becomes the desired roll, pitch angles sent to the stabilize controller and the tuner is disabled until the sticks are put back into the middle for 1 second
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*/
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#define AUTO_TUNE_PILOT_OVERRIDE_TIMEOUT_MS 500 // restart tuning if pilot has left sticks in middle for 2 seconds
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#define AUTO_TUNE_TARGET_RATE_TIMEOUT_MS 500 // timeout for rate test step
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#define AUTO_TUNE_TARGET_RATE_CDS 9000 // target roll/pitch rate during AUTO_TUNE_STEP_TESTING step
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#define AUTO_TUNE_LEVEL_ANGLE_CD 300 // angle which qualifies as level
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#define AUTO_TUNE_TARGET_ANGLE_CD 2000 // target angle during TESTING_RATE step that will cause us to move to next step
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#define AUTO_TUNE_REQUIRED_LEVEL_TIME_MS 250 // time we require the copter to be level
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#define AUTO_TUNE_AGGRESSIVENESS 0.1f // tuning for 10% overshoot
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#define AUTO_TUNE_RD_STEP 0.0005f // minimum increment when increasing/decreasing Rate D term
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#define AUTO_TUNE_RP_STEP 0.005f // minimum increment when increasing/decreasing Rate P term
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#define AUTO_TUNE_SP_STEP 0.5f // minimum increment when increasing/decreasing Stab P term
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#define AUTO_TUNE_SP_BACKOFF 0.75f // back off on the Stab P tune
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#define AUTO_TUNE_PI_RATIO_FOR_TESTING 0.1f // I is set 10x smaller than P during testing
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#define AUTO_TUNE_RP_RATIO_FINAL 1.0f // I is set 1x P after testing
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#define AUTO_TUNE_RD_MIN 0.0f // minimum Rate D value
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#define AUTO_TUNE_RD_MAX 0.1f // maximum Rate D value
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#define AUTO_TUNE_RP_MIN 0.02f // minimum Rate P value
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#define AUTO_TUNE_RP_MAX 1.0f // maximum Rate P value
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#define AUTO_TUNE_SP_MIN 1.0f // minimum Stab P value
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#define AUTO_TUNE_SP_MAX 15.0f // maximum Stab P value
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#define AUTO_TUNE_SUCCESS_COUNT 4 // how many successful iterations we need to freeze at current gains
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// things that can be tuned
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enum AutoTuneAxisType {
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AUTO_TUNE_AXIS_ROLL = 0,
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AUTO_TUNE_AXIS_PITCH = 1
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};
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// steps performed during tuning
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enum AutoTuneStepType {
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AUTO_TUNE_STEP_WAITING_FOR_LEVEL = 0,
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AUTO_TUNE_STEP_TESTING = 1,
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AUTO_TUNE_STEP_UPDATE_GAINS = 2
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};
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// steps performed during tuning
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enum AutoTuneTuneType {
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AUTO_TUNE_TYPE_RD_UP = 0,
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AUTO_TUNE_TYPE_RD_DOWN = 1,
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AUTO_TUNE_TYPE_RP_UP = 2,
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AUTO_TUNE_TYPE_SP_UP = 3
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};
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// state
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struct auto_tune_state_struct {
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uint8_t enabled : 1; // 0 = disabled, 1 = enabled
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uint8_t active : 1; // 0 = inactive (temporarily suspended), 1 = actively tuning
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uint8_t pilot_override : 1; // 1 = pilot is overriding controls so we suspend tuning temporarily
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AutoTuneAxisType axis : 1; // see AutoTuneAxisType for which things can be tuned
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uint8_t positive_direction : 1; // 0 = tuning in negative direction (i.e. left for roll), 1 = positive direction (i.e. right for roll)
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AutoTuneStepType step : 2; // see AutoTuneStepType for what steps are performed
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AutoTuneTuneType tune_type : 2; // see AutoTuneTuneType
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} auto_tune_state;
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// variables
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uint32_t auto_tune_override_time; // the last time the pilot overrode the controls
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float auto_tune_test_min; // the minimum angular rate achieved during TESTING_RATE step
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float auto_tune_test_max; // the maximum angular rate achieved during TESTING_RATE step
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uint32_t auto_tune_timer; // generic timer variable
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int8_t auto_tune_counter; // counter for tuning gains
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float orig_roll_rp, orig_roll_ri, orig_roll_rd, orig_roll_sp; // backup of currently being tuned parameter values
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float orig_pitch_rp, orig_pitch_ri, orig_pitch_rd, orig_pitch_sp; // backup of currently being tuned parameter values
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float tune_roll_rp, tune_roll_rd, tune_roll_sp; // currently being tuned parameter values
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float tune_pitch_rp, tune_pitch_rd, tune_pitch_sp; // currently being tuned parameter values
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// store current pids as originals
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void auto_tune_save_orig_pids()
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{
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orig_roll_rp = g.pid_rate_roll.kP();
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orig_roll_ri = g.pid_rate_roll.kI();
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orig_roll_rd = g.pid_rate_roll.kD();
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orig_roll_sp = g.pi_stabilize_roll.kP();
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orig_pitch_rp = g.pid_rate_pitch.kP();
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orig_pitch_ri = g.pid_rate_pitch.kI();
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orig_pitch_rd = g.pid_rate_pitch.kD();
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orig_pitch_sp = g.pi_stabilize_pitch.kP();
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}
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// auto_tune_restore_orig_pids - restore pids to their original values
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void auto_tune_restore_orig_pids()
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{
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g.pid_rate_roll.kP(orig_roll_rp);
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g.pid_rate_roll.kI(orig_roll_ri);
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g.pid_rate_roll.kD(orig_roll_rd);
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g.pi_stabilize_roll.kP(orig_roll_sp);
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g.pid_rate_pitch.kP(orig_pitch_rp);
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g.pid_rate_pitch.kI(orig_pitch_ri);
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g.pid_rate_pitch.kD(orig_pitch_rd);
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g.pi_stabilize_pitch.kP(orig_pitch_sp);
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ap.disable_stab_rate_limit = false;
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}
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// auto_tune_load_tuned_pids - restore pids to their original values
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void auto_tune_load_tuned_pids()
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{
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if (tune_roll_rp != 0 && tune_pitch_rp != 0) {
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g.pid_rate_roll.kP(tune_roll_rp);
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g.pid_rate_roll.kI(tune_roll_rp*AUTO_TUNE_RP_RATIO_FINAL);
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g.pid_rate_roll.kD(tune_roll_rd);
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g.pi_stabilize_roll.kP(tune_roll_sp);
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g.pid_rate_pitch.kP(tune_pitch_rp);
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g.pid_rate_pitch.kI(tune_pitch_rp*AUTO_TUNE_RP_RATIO_FINAL);
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g.pid_rate_pitch.kD(tune_pitch_rd);
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g.pi_stabilize_pitch.kP(tune_pitch_sp);
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ap.disable_stab_rate_limit = false;
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}
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}
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// start an auto tuning session
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void auto_tune_start()
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{
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// check we are in stabilize mode
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if (control_mode == STABILIZE || control_mode == ALT_HOLD) {
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// reset axis if this is our first time (i.e. we were not just suspended)
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if (!auto_tune_state.active) {
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auto_tune_state.active = true;
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auto_tune_state.axis = AUTO_TUNE_AXIS_ROLL;
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auto_tune_state.positive_direction = false;
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auto_tune_state.step = AUTO_TUNE_STEP_WAITING_FOR_LEVEL;
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auto_tune_timer = millis();
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auto_tune_state.tune_type = AUTO_TUNE_TYPE_RD_UP;
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auto_tune_save_orig_pids();
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// initialise tuned pid values
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tune_roll_rp = g.pid_rate_roll.kP();
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tune_roll_rd = g.pid_rate_roll.kD();
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tune_roll_sp = g.pi_stabilize_roll.kP();
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tune_pitch_rp = g.pid_rate_pitch.kP();
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tune_pitch_rd = g.pid_rate_pitch.kD();
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tune_pitch_sp = g.pi_stabilize_pitch.kP();
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}else{
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// restarting from suspended state
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auto_tune_restore_orig_pids();
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}
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// set roll-pitch mode to our special auto tuning stabilize roll-pitch mode
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if (set_roll_pitch_mode(ROLL_PITCH_AUTOTUNE)) {
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auto_tune_state.enabled = true;
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Log_Write_Event(DATA_AUTOTUNE_ON);
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}
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}
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}
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// turn off tuning and return to standard pids
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void auto_tune_stop()
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{
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if (auto_tune_state.enabled) {
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auto_tune_state.enabled = false;
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auto_tune_state.active = false;
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ap.disable_stab_rate_limit = false;
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if (roll_pitch_mode == ROLL_PITCH_AUTOTUNE) {
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set_roll_pitch_mode(ROLL_PITCH_STABLE); // restore roll-pitch mode
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rate_targets_frame = EARTH_FRAME; // regular stabilize mode frame
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}
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// restore pids to their original values
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auto_tune_restore_orig_pids();
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Log_Write_Event(DATA_AUTOTUNE_OFF);
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}
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}
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// stop tuning but remain with tuned pids
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void auto_tune_suspend()
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{
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auto_tune_load_tuned_pids();
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if (auto_tune_state.active) {
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auto_tune_state.active = false;
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Log_Write_Event(DATA_AUTOTUNE_SUSPENDED);
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}
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}
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// save discovered gains to eeprom if auto tuner is enabled (i.e. switch is in middle or high position)
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void auto_tune_save_tuning_gains()
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{
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if (auto_tune_state.enabled) {
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auto_tune_load_tuned_pids();
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g.pid_rate_roll.save_gains();
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g.pid_rate_pitch.save_gains();
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g.pi_stabilize_roll.save_gains();
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g.pi_stabilize_pitch.save_gains();
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Log_Write_Event(DATA_AUTOTUNE_SAVEDGAINS);
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}
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}
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// Auto tuning roll-pitch controller
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static void
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get_autotune_roll_pitch_controller(int32_t pilot_roll_angle, int32_t pilot_pitch_angle)
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{
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int32_t target_roll_rate, target_pitch_rate;
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float rotation_rate; // rotation rate in radians/second
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int32_t lean_angle;
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// exit immediately if not enabled or not actively tuning
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if (!auto_tune_state.enabled || !auto_tune_state.active) {
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return;
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}
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// check for pilot override
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if (pilot_roll_angle != 0 || pilot_pitch_angle != 0 ) {
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if (!auto_tune_state.pilot_override) {
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// restore pids to their original values
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auto_tune_restore_orig_pids();
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}
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auto_tune_state.pilot_override = true;
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auto_tune_override_time = millis();
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}else if (auto_tune_state.pilot_override) {
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// check if we should resume tuning after pilot's override
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if (millis() - auto_tune_override_time > AUTO_TUNE_PILOT_OVERRIDE_TIMEOUT_MS) {
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auto_tune_state.pilot_override = false; // turn off pilot override
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auto_tune_state.step = AUTO_TUNE_STEP_WAITING_FOR_LEVEL; // set tuning step back from beginning
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auto_tune_timer = millis();
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}
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}
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// check tuning step
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if (!auto_tune_state.pilot_override) {
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switch (auto_tune_state.step) {
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case AUTO_TUNE_STEP_WAITING_FOR_LEVEL:
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// reset counter if we are no longer level
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if ((labs(ahrs.roll_sensor) > AUTO_TUNE_LEVEL_ANGLE_CD) || (labs(ahrs.pitch_sensor) > AUTO_TUNE_LEVEL_ANGLE_CD)) {
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auto_tune_timer = millis();
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}
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// if we have been level for a sufficient amount of time (0.5 seconds) move onto next step
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if (millis() - auto_tune_timer >= AUTO_TUNE_REQUIRED_LEVEL_TIME_MS) {
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auto_tune_state.step = AUTO_TUNE_STEP_TESTING;
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// init variables for next step
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auto_tune_test_max = 0;
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auto_tune_test_min = 0;
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rotation_rate = 0;
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auto_tune_timer = millis();
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// initialise rate controller targets
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acro_roll_rate = roll_rate_target_bf;
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acro_pitch_rate = pitch_rate_target_bf;
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acro_yaw_rate = yaw_rate_target_bf;
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// restore pids to their tuning values
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if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
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g.pid_rate_roll.kP(tune_roll_rp);
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g.pid_rate_roll.kI(tune_roll_rp*0.01f);
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g.pid_rate_roll.kD(tune_roll_rd);
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g.pi_stabilize_roll.kP(tune_roll_sp);
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}else{
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g.pid_rate_pitch.kP(tune_pitch_rp);
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g.pid_rate_pitch.kI(tune_pitch_rp*0.01f);
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g.pid_rate_pitch.kD(tune_pitch_rd);
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g.pi_stabilize_pitch.kP(tune_pitch_sp);
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}
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ap.disable_stab_rate_limit = true; // disable rate limits
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}
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break;
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case AUTO_TUNE_STEP_TESTING:
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// Run the test
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// update rotation targets in body-earth frame
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if(auto_tune_state.tune_type == AUTO_TUNE_TYPE_SP_UP){
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if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
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// override roll angle
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if (auto_tune_state.positive_direction) {
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control_roll = AUTO_TUNE_TARGET_ANGLE_CD;
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}else{
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control_roll = -AUTO_TUNE_TARGET_ANGLE_CD;
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}
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get_stabilize_roll(control_roll);
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}else{
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// override pitch angle
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if (auto_tune_state.positive_direction) {
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control_pitch = AUTO_TUNE_TARGET_ANGLE_CD;
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}else{
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control_pitch = -AUTO_TUNE_TARGET_ANGLE_CD;
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}
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get_stabilize_pitch(control_pitch);
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}
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} else {
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if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
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// override roll rate
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if (auto_tune_state.positive_direction) {
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target_roll_rate = AUTO_TUNE_TARGET_RATE_CDS;
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}else{
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target_roll_rate = -AUTO_TUNE_TARGET_RATE_CDS;
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}
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// set body frame targets for rate controller
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set_roll_rate_target(target_roll_rate, BODY_FRAME);
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set_pitch_rate_target(acro_pitch_rate, BODY_FRAME);
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set_yaw_rate_target(acro_yaw_rate, BODY_FRAME);
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}else{
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// override pitch rate
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if (auto_tune_state.positive_direction) {
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target_pitch_rate = AUTO_TUNE_TARGET_RATE_CDS;
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}else{
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target_pitch_rate = -AUTO_TUNE_TARGET_RATE_CDS;
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}
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// set body frame targets for rate controller
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set_pitch_rate_target(target_pitch_rate, BODY_FRAME);
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set_roll_rate_target(acro_roll_rate, BODY_FRAME);
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set_yaw_rate_target(acro_yaw_rate, BODY_FRAME);
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}
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rate_targets_frame = BODY_EARTH_FRAME;
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}
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// Get Rate and Angle
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if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
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// 20 Hz filter on rate
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rotation_rate = ToDeg(fabs(ahrs.get_gyro().x)) * 100.0f;
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lean_angle = labs(ahrs.roll_sensor);
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}else{
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// 20 Hz filter on rate
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// rotation_rate = rotation_rate + 0.55686f*(ToDeg(fabs(ahrs.get_gyro().y))*100.0f-rotation_rate);
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rotation_rate = ToDeg(fabs(ahrs.get_gyro().y)) * 100.0f;
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lean_angle = labs(ahrs.pitch_sensor);
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}
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// Make measurements
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if(auto_tune_state.tune_type == AUTO_TUNE_TYPE_SP_UP){
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// capture max angle
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if (lean_angle > auto_tune_test_max) {
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auto_tune_test_max = lean_angle;
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auto_tune_test_min = lean_angle;
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}
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// capture min rotation rate
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if (lean_angle < auto_tune_test_min && auto_tune_test_max > AUTO_TUNE_TARGET_ANGLE_CD*(1-AUTO_TUNE_AGGRESSIVENESS)) {
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auto_tune_test_min = lean_angle;
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}
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}else{
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// capture max rotation rate
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if (rotation_rate > auto_tune_test_max) {
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auto_tune_test_max = rotation_rate;
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auto_tune_test_min = rotation_rate;
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}
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// capture min rotation rate
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if (rotation_rate < auto_tune_test_min && auto_tune_test_max > AUTO_TUNE_TARGET_RATE_CDS*(1-2*AUTO_TUNE_AGGRESSIVENESS)) {
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auto_tune_test_min = rotation_rate;
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}
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}
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// check for end of test conditions
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if(millis() - auto_tune_timer >= AUTO_TUNE_TARGET_RATE_TIMEOUT_MS) {
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auto_tune_state.step = AUTO_TUNE_STEP_UPDATE_GAINS;
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}
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if(auto_tune_state.tune_type == AUTO_TUNE_TYPE_SP_UP){
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if ((lean_angle >= AUTO_TUNE_TARGET_ANGLE_CD*(1+AUTO_TUNE_AGGRESSIVENESS)) ||
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(auto_tune_test_max-auto_tune_test_min > AUTO_TUNE_TARGET_ANGLE_CD*AUTO_TUNE_AGGRESSIVENESS)) {
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auto_tune_state.step = AUTO_TUNE_STEP_UPDATE_GAINS;
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}
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}else{
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if (lean_angle >= AUTO_TUNE_TARGET_ANGLE_CD) {
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auto_tune_state.step = AUTO_TUNE_STEP_UPDATE_GAINS;
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}
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if (auto_tune_state.tune_type == AUTO_TUNE_TYPE_RD_UP || auto_tune_state.tune_type == AUTO_TUNE_TYPE_RD_DOWN) {
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if(auto_tune_test_max-auto_tune_test_min > AUTO_TUNE_TARGET_RATE_CDS*AUTO_TUNE_AGGRESSIVENESS) {
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auto_tune_state.step = AUTO_TUNE_STEP_UPDATE_GAINS;
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}
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}
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}
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// logging
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Log_Write_AutoTuneDetails((int16_t)lean_angle, rotation_rate);
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break;
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case AUTO_TUNE_STEP_UPDATE_GAINS:
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// restore pids to their original values
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g.pid_rate_roll.kP(orig_roll_rp);
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g.pid_rate_roll.kI(orig_roll_rp*AUTO_TUNE_PI_RATIO_FOR_TESTING);
|
|
g.pid_rate_roll.kD(orig_roll_rd);
|
|
g.pi_stabilize_roll.kP(orig_roll_sp);
|
|
g.pid_rate_pitch.kP(orig_pitch_rp);
|
|
g.pid_rate_pitch.kI(orig_pitch_rp*AUTO_TUNE_PI_RATIO_FOR_TESTING);
|
|
g.pid_rate_pitch.kD(orig_pitch_rd);
|
|
g.pi_stabilize_pitch.kP(orig_pitch_sp);
|
|
|
|
// re-enable the rate limits
|
|
ap.disable_stab_rate_limit = false;
|
|
|
|
// logging
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
Log_Write_AutoTune(auto_tune_state.axis, auto_tune_state.tune_type, auto_tune_test_min, auto_tune_test_max, tune_roll_rp, tune_roll_rd, tune_roll_sp);
|
|
}else{
|
|
Log_Write_AutoTune(auto_tune_state.axis, auto_tune_state.tune_type, auto_tune_test_min, auto_tune_test_max, tune_pitch_rp, tune_pitch_rd, tune_pitch_sp);
|
|
}
|
|
|
|
// do gain updates
|
|
if (auto_tune_state.tune_type == AUTO_TUNE_TYPE_RD_UP) {
|
|
if (auto_tune_test_max > AUTO_TUNE_TARGET_RATE_CDS) {
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_rp -= AUTO_TUNE_RP_STEP;
|
|
}else{
|
|
tune_pitch_rp -= AUTO_TUNE_RP_STEP;
|
|
}
|
|
// stop the auto tune if we have hit the minimum roll or pitch rate P
|
|
if(((auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL && tune_roll_rp < AUTO_TUNE_RP_MIN) ||
|
|
(auto_tune_state.axis == AUTO_TUNE_AXIS_PITCH && tune_pitch_rp < AUTO_TUNE_RP_MIN)) ) {
|
|
Log_Write_Event(DATA_AUTOTUNE_ABANDONED);
|
|
auto_tune_stop();
|
|
return;
|
|
}
|
|
}else if(auto_tune_test_max < AUTO_TUNE_TARGET_RATE_CDS*(1.0f-AUTO_TUNE_AGGRESSIVENESS*2.0f) &&
|
|
((auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL && tune_roll_rp <= AUTO_TUNE_RP_MAX) ||
|
|
(auto_tune_state.axis == AUTO_TUNE_AXIS_PITCH && tune_pitch_rp <= AUTO_TUNE_RP_MAX)) ) {
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_rp += AUTO_TUNE_RP_STEP*2.0f;
|
|
}else{
|
|
tune_pitch_rp += AUTO_TUNE_RP_STEP*2.0f;
|
|
}
|
|
}else{
|
|
if (auto_tune_test_max-auto_tune_test_min > AUTO_TUNE_TARGET_RATE_CDS*AUTO_TUNE_AGGRESSIVENESS) {
|
|
auto_tune_counter++;
|
|
}else{
|
|
if (auto_tune_counter > 0 ) {
|
|
auto_tune_counter--;
|
|
}
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_rd += AUTO_TUNE_RD_STEP*2.0f;
|
|
// stop tuning if we hit max D
|
|
if (tune_roll_rd >= AUTO_TUNE_RD_MAX) {
|
|
tune_roll_rd = AUTO_TUNE_RD_MAX;
|
|
auto_tune_counter = AUTO_TUNE_SUCCESS_COUNT;
|
|
}
|
|
}else{
|
|
tune_pitch_rd += AUTO_TUNE_RD_STEP*2.0f;
|
|
// stop tuning if we hit max D
|
|
if (tune_pitch_rd >= AUTO_TUNE_RD_MAX) {
|
|
tune_pitch_rd = AUTO_TUNE_RD_MAX;
|
|
auto_tune_counter = AUTO_TUNE_SUCCESS_COUNT;
|
|
}
|
|
}
|
|
}
|
|
}
|
|
} else if (auto_tune_state.tune_type == AUTO_TUNE_TYPE_RD_DOWN) {
|
|
if (auto_tune_test_max > AUTO_TUNE_TARGET_RATE_CDS) {
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_rp -= AUTO_TUNE_RP_STEP;
|
|
}else{
|
|
tune_pitch_rp -= AUTO_TUNE_RP_STEP;
|
|
}
|
|
// stop the auto tune if we have hit the minimum roll or pitch rate P
|
|
if(((auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL && tune_roll_rp < AUTO_TUNE_RP_MIN) ||
|
|
(auto_tune_state.axis == AUTO_TUNE_AXIS_PITCH && tune_pitch_rp < AUTO_TUNE_RP_MIN)) ) {
|
|
Log_Write_Event(DATA_AUTOTUNE_ABANDONED);
|
|
auto_tune_stop();
|
|
return;
|
|
}
|
|
}else if(auto_tune_test_max < AUTO_TUNE_TARGET_RATE_CDS*(1-AUTO_TUNE_AGGRESSIVENESS*2.0f) &&
|
|
((auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL && tune_roll_rp <= AUTO_TUNE_RP_MAX) ||
|
|
(auto_tune_state.axis == AUTO_TUNE_AXIS_PITCH && tune_pitch_rp <= AUTO_TUNE_RP_MAX)) ) {
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_rp += AUTO_TUNE_RP_STEP;
|
|
}else{
|
|
tune_pitch_rp += AUTO_TUNE_RP_STEP;
|
|
}
|
|
}else{
|
|
if (auto_tune_test_max-auto_tune_test_min < AUTO_TUNE_TARGET_RATE_CDS*AUTO_TUNE_AGGRESSIVENESS) {
|
|
auto_tune_counter++;
|
|
}else{
|
|
if (auto_tune_counter > 0 ) {
|
|
auto_tune_counter--;
|
|
}
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_rd -= AUTO_TUNE_RD_STEP;
|
|
// stop tuning if we hit max D
|
|
if (tune_roll_rd <= AUTO_TUNE_RD_MIN) {
|
|
tune_roll_rd = AUTO_TUNE_RD_MIN;
|
|
auto_tune_counter = AUTO_TUNE_SUCCESS_COUNT;
|
|
}
|
|
}else{
|
|
tune_pitch_rd -= AUTO_TUNE_RD_STEP;
|
|
// stop tuning if we hit max D
|
|
if (tune_pitch_rd <= AUTO_TUNE_RD_MIN) {
|
|
tune_pitch_rd = AUTO_TUNE_RD_MIN;
|
|
auto_tune_counter = AUTO_TUNE_SUCCESS_COUNT;
|
|
}
|
|
}
|
|
}
|
|
}
|
|
} else if (auto_tune_state.tune_type == AUTO_TUNE_TYPE_RP_UP) {
|
|
if (auto_tune_test_max > AUTO_TUNE_TARGET_RATE_CDS) {
|
|
auto_tune_counter++;
|
|
}else{
|
|
if (auto_tune_counter > 0 ) {
|
|
auto_tune_counter--;
|
|
}
|
|
// increase P & I or D term
|
|
// update PI term
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_rp += AUTO_TUNE_RP_STEP;
|
|
// stop tuning if we hit max P
|
|
if (tune_roll_rp >= AUTO_TUNE_RP_MAX) {
|
|
tune_roll_rp = AUTO_TUNE_RP_MAX;
|
|
auto_tune_counter = AUTO_TUNE_SUCCESS_COUNT;
|
|
}
|
|
}else{
|
|
tune_pitch_rp += AUTO_TUNE_RP_STEP;
|
|
// stop tuning if we hit max P
|
|
if (tune_pitch_rp >= AUTO_TUNE_RP_MAX) {
|
|
tune_pitch_rp = AUTO_TUNE_RP_MAX;
|
|
auto_tune_counter = AUTO_TUNE_SUCCESS_COUNT;
|
|
}
|
|
}
|
|
}
|
|
} else if (auto_tune_state.tune_type == AUTO_TUNE_TYPE_SP_UP) {
|
|
if (auto_tune_test_max > AUTO_TUNE_TARGET_ANGLE_CD*(1+AUTO_TUNE_AGGRESSIVENESS) ||
|
|
(auto_tune_test_max-auto_tune_test_min > AUTO_TUNE_TARGET_ANGLE_CD*AUTO_TUNE_AGGRESSIVENESS)) {
|
|
auto_tune_counter++;
|
|
}else{
|
|
if (auto_tune_counter > 0 ) {
|
|
auto_tune_counter--;
|
|
}
|
|
// increase P & I or D term
|
|
// update PI term
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_sp += AUTO_TUNE_SP_STEP;
|
|
// stop tuning if we hit max P
|
|
if (tune_roll_sp >= AUTO_TUNE_SP_MAX) {
|
|
tune_roll_sp = AUTO_TUNE_SP_MAX;
|
|
auto_tune_counter = AUTO_TUNE_SUCCESS_COUNT;
|
|
}
|
|
}else{
|
|
tune_pitch_sp += AUTO_TUNE_SP_STEP;
|
|
// stop tuning if we hit max P
|
|
if (tune_pitch_sp >= AUTO_TUNE_SP_MAX) {
|
|
tune_pitch_sp = AUTO_TUNE_SP_MAX;
|
|
auto_tune_counter = AUTO_TUNE_SUCCESS_COUNT;
|
|
}
|
|
}
|
|
}
|
|
}
|
|
|
|
// reverse direction
|
|
auto_tune_state.positive_direction = !auto_tune_state.positive_direction;
|
|
|
|
// we've complete this step, finalise pids and move to next step
|
|
if (auto_tune_counter >= AUTO_TUNE_SUCCESS_COUNT) {
|
|
|
|
// reset counter
|
|
auto_tune_counter = 0;
|
|
|
|
// move to the next tuning type
|
|
if (auto_tune_state.tune_type < AUTO_TUNE_TYPE_SP_UP) {
|
|
auto_tune_state.tune_type++;
|
|
}else{
|
|
// we've reached the end of a D-up-down PI-up-down tune type cycle
|
|
auto_tune_state.tune_type = AUTO_TUNE_TYPE_RD_UP;
|
|
|
|
// if we've just completed roll move onto pitch
|
|
if (auto_tune_state.axis == AUTO_TUNE_AXIS_ROLL) {
|
|
tune_roll_sp = tune_roll_sp * AUTO_TUNE_SP_BACKOFF;
|
|
auto_tune_state.axis = AUTO_TUNE_AXIS_PITCH;
|
|
}else{
|
|
tune_pitch_sp = tune_pitch_sp * AUTO_TUNE_SP_BACKOFF;
|
|
tune_roll_sp = min(tune_roll_sp, tune_pitch_sp);
|
|
tune_pitch_sp = min(tune_roll_sp, tune_pitch_sp);
|
|
// if we've just completed pitch we are done so suspend tuning
|
|
auto_tune_suspend();
|
|
}
|
|
}
|
|
}
|
|
|
|
// reset testing step
|
|
auto_tune_state.step = AUTO_TUNE_STEP_WAITING_FOR_LEVEL;
|
|
auto_tune_timer = millis();
|
|
break;
|
|
}
|
|
}
|
|
}
|
|
#endif // AUTOTUNE == ENABLED |