ardupilot/libraries/AC_AutoTune/AC_AutoTune_Heli.h

286 lines
12 KiB
C++

/*
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 helicopters
*/
#pragma once
#include "AC_AutoTune.h"
class AC_AutoTune_Heli : public AC_AutoTune
{
public:
// constructor
AC_AutoTune_Heli();
// save gained, called on disarm
void save_tuning_gains() override;
// var_info for holding Parameter information
static const struct AP_Param::GroupInfo var_info[];
protected:
//
// methods to load and save gains
//
// backup original gains and prepare for start of tuning
void backup_gains_and_initialise() override;
// switch to use original gains
void load_orig_gains() override;
// switch to gains found by last successful autotune
void load_tuned_gains() override;
// load gains used between tests. called during testing mode's update-gains step to set gains ahead of return-to-level step
void load_intra_test_gains() override;
// load test gains
void load_test_gains() override;
// reset the test vaariables for heli
void reset_vehicle_test_variables() override;
// reset the update gain variables for heli
void reset_update_gain_variables() override;
// initializes test
void test_init() override;
// runs test
void test_run(AxisType test_axis, const float dir_sign) override;
// update gains for the rate p up tune type
void updating_rate_p_up_all(AxisType test_axis) override;
// update gains for the rate d up tune type
void updating_rate_d_up_all(AxisType test_axis) override;
// update gains for the rate d down tune type
void updating_rate_d_down_all(AxisType test_axis) override {};
// update gains for the rate ff up tune type
void updating_rate_ff_up_all(AxisType test_axis) override;
// update gains for the angle p up tune type
void updating_angle_p_up_all(AxisType test_axis) override;
// update gains for the angle p down tune type
void updating_angle_p_down_all(AxisType test_axis) override {};
// update gains for the max gain tune type
void updating_max_gains_all(AxisType test_axis) override;
// set gains post tune for the tune type
void set_gains_post_tune(AxisType test_axis) override;
// reverse direction for twitch test
bool twitch_reverse_direction() override { return positive_direction; }
// methods to log autotune summary data
void Log_AutoTune() override;
void Log_Write_AutoTune(uint8_t _axis, uint8_t tune_step, float dwell_freq, float meas_gain, float meas_phase, float new_gain_rff, float new_gain_rp, float new_gain_rd, float new_gain_sp, float max_accel);
// methods to log autotune time history results for command, angular rate, and attitude.
void Log_AutoTuneDetails() override;
void Log_Write_AutoTuneDetails(float motor_cmd, float tgt_rate_rads, float rate_rads, float tgt_ang_rad, float ang_rad);
// methods to log autotune frequency response results
void Log_AutoTuneSweep() override;
void Log_Write_AutoTuneSweep(float freq, float gain, float phase);
// send intermittant updates to user on status of tune
void do_gcs_announcements() override;
// send post test updates to user
void do_post_test_gcs_announcements() override;
// report final gains for a given axis to GCS
void report_final_gains(AxisType test_axis) const override;
// set the tuning test sequence
void set_tune_sequence() override;
// get_axis_bitmask accessor
uint8_t get_axis_bitmask() const override { return axis_bitmask; }
// get_testing_step_timeout_ms accessor
uint32_t get_testing_step_timeout_ms() const override;
private:
// max_gain_data type stores information from the max gain test
struct max_gain_data {
float freq;
float phase;
float gain;
float max_allowed;
};
// max gain data for rate p tuning
max_gain_data max_rate_p;
// max gain data for rate d tuning
max_gain_data max_rate_d;
// Feedforward test used to determine Rate FF gain
void rate_ff_test_init();
void rate_ff_test_run(float max_angle_cds, float target_rate_cds, float dir_sign);
// dwell test used to perform frequency dwells for rate gains
void dwell_test_init(float start_frq, float filt_freq);
void dwell_test_run(uint8_t freq_resp_input, float start_frq, float stop_frq, float &dwell_gain, float &dwell_phase);
// dwell test used to perform frequency dwells for angle gains
void angle_dwell_test_init(float start_frq, float filt_freq);
void angle_dwell_test_run(float start_frq, float stop_frq, float &dwell_gain, float &dwell_phase);
// generates waveform for frequency sweep excitations
float waveform(float time, float time_record, float waveform_magnitude, float wMin, float wMax);
// updating_rate_ff_up - adjust FF to ensure the target is reached
// FF is adjusted until rate requested is acheived
void updating_rate_ff_up(float &tune_ff, float rate_target, float meas_rate, float meas_command);
// updating_rate_p_up - uses maximum allowable gain determined from max_gain test to determine rate p gain that does not exceed exceed max response gain
void updating_rate_p_up(float &tune_p, float *freq, float *gain, float *phase, uint8_t &frq_cnt, max_gain_data &max_gain_p);
// updating_rate_d_up - uses maximum allowable gain determined from max_gain test to determine rate d gain where the response gain is at a minimum
void updating_rate_d_up(float &tune_d, float *freq, float *gain, float *phase, uint8_t &frq_cnt, max_gain_data &max_gain_d);
// updating_angle_p_up - determines maximum angle p gain for pitch and roll
void updating_angle_p_up(float &tune_p, float *freq, float *gain, float *phase, uint8_t &frq_cnt);
// updating_max_gains: use dwells at increasing frequency to determine gain at which instability will occur
void updating_max_gains(float *freq, float *gain, float *phase, uint8_t &frq_cnt, max_gain_data &max_gain_p, max_gain_data &max_gain_d, float &tune_p, float &tune_d);
// reset the max_gains update gain variables
void reset_maxgains_update_gain_variables();
// reset the sweep variables
void reset_sweep_variables();
// exceeded_freq_range - ensures tuning remains inside frequency range
bool exceeded_freq_range(float frequency);
// report gain formating helper
void report_axis_gains(const char* axis_string, float rate_P, float rate_I, float rate_D, float rate_ff, float angle_P, float max_accel) const;
// updating rate FF variables
// flag for completion of the initial direction for the feedforward test
bool first_dir_complete;
// feedforward gain resulting from testing in the initial direction
float first_dir_rff;
// updating max gain variables
// flag for finding maximum p gain
bool found_max_p;
// flag for finding maximum d gain
bool found_max_d;
// flag for interpolating to find max response gain
bool find_middle;
// updating angle P up variables
// track the maximum phase
float phase_max;
// previous gain
float sp_prev_gain;
// flag for finding the peak of the gain response
bool find_peak;
// updating rate P up
// counter value of previous good frequency
uint8_t rp_prev_good_frq_cnt;
// updating rate D up
// counter value of previous good frequency
uint8_t rd_prev_good_frq_cnt;
// previous gain
float rd_prev_gain;
uint8_t ff_test_phase; // phase of feedforward test
float test_command_filt; // filtered commanded output for FF test analysis
float test_rate_filt; // filtered rate output for FF test analysis
float command_out; // test axis command output
float test_tgt_rate_filt; // filtered target rate for FF test analysis
float filt_target_rate; // filtered target rate
float test_gain[20]; // frequency response gain for each dwell test iteration
float test_freq[20]; // frequency of each dwell test iteration
float test_phase[20]; // frequency response phase for each dwell test iteration
float dwell_start_time_ms; // start time in ms of dwell test
uint8_t freq_cnt_max; // counter number for frequency that produced max gain response
float curr_test_freq; // current test frequency
float curr_test_gain; // current test frequency response gain
float curr_test_phase; // current test frequency response phase
Vector3f start_angles; // aircraft attitude at the start of test
uint32_t settle_time; // time in ms for allowing aircraft to stabilize before initiating test
uint32_t phase_out_time; // time in ms to phase out response
float waveform_freq_rads; //current frequency for chirp waveform
float trim_pff_out; // trim output of the PID rate controller for P, I and FF terms
float trim_meas_rate; // trim measured gyro rate
//variables from rate FF test
float trim_command_reading;
float trim_heading;
LowPassFilterFloat rate_request_cds;
LowPassFilterFloat angle_request_cd;
// variables from dwell test
LowPassFilterVector2f filt_pit_roll_cd; // filtered pitch and roll attitude for dwell rate method
LowPassFilterFloat filt_heading_error_cd; // filtered heading error for dwell rate method
LowPassFilterVector2f filt_att_fdbk_from_velxy_cd;
LowPassFilterFloat filt_command_reading; // filtered command reading to keep oscillation centered
LowPassFilterFloat filt_gyro_reading; // filtered gyro reading to keep oscillation centered
LowPassFilterFloat filt_tgt_rate_reading; // filtered target rate reading to keep oscillation centered
// trim variables for determining trim state prior to test starting
Vector3f trim_attitude_cd; // trim attitude before starting test
float trim_command; // trim target yaw reading before starting test
float trim_yaw_tgt_reading; // trim target yaw reading before starting test
float trim_yaw_heading_reading; // trim heading reading before starting test
LowPassFilterFloat command_filt; // filtered command - filtering intended to remove noise
LowPassFilterFloat target_rate_filt; // filtered target rate in radians/second - filtering intended to remove noise
// sweep_data tracks the overall characteristics in the response to the frequency sweep
struct sweep_data {
float maxgain_freq;
float maxgain_gain;
float maxgain_phase;
float ph180_freq;
float ph180_gain;
float ph180_phase;
float ph270_freq;
float ph270_gain;
float ph270_phase;
uint8_t progress; // set based on phase of frequency response. 0 - start; 1 - reached 180 deg; 2 - reached 270 deg;
};
sweep_data sweep;
// parameters
AP_Int8 axis_bitmask; // axes to be tuned
AP_Int8 seq_bitmask; // tuning sequence bitmask
AP_Float min_sweep_freq; // minimum sweep frequency
AP_Float max_sweep_freq; // maximum sweep frequency
AP_Float max_resp_gain; // maximum response gain
AP_Float vel_hold_gain; // gain for velocity hold
// freqresp object for the rate frequency response tests
AC_AutoTune_FreqResp freqresp_rate;
// freqresp object for the angle frequency response tests
AC_AutoTune_FreqResp freqresp_angle;
};