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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/>.
*/
/*
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support for autotune of helicopters
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*/
# pragma once
# include "AC_AutoTune.h"
class AC_AutoTune_Heli : public AC_AutoTune
{
public :
// constructor
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AC_AutoTune_Heli ( ) ;
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// save gained, called on disarm
void save_tuning_gains ( ) override ;
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// var_info for holding Parameter information
static const struct AP_Param : : GroupInfo var_info [ ] ;
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protected :
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//
// methods to load and save gains
//
// backup original gains and prepare for start of tuning
void backup_gains_and_initialise ( ) override ;
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// switch to use original gains
void load_orig_gains ( ) override ;
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// switch to gains found by last successful autotune
void load_tuned_gains ( ) override ;
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// 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 ;
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// reset the test vaariables for heli
void reset_vehicle_test_variables ( ) override ;
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// reset the update gain variables for heli
void reset_update_gain_variables ( ) override ;
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// initializes test
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void test_init ( ) override ;
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// runs test
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void test_run ( AxisType test_axis , const float dir_sign ) override ;
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// update gains for the rate p up tune type
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void updating_rate_p_up_all ( AxisType test_axis ) override ;
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// update gains for the rate d up tune type
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void updating_rate_d_up_all ( AxisType test_axis ) override ;
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// update gains for the rate d down tune type
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void updating_rate_d_down_all ( AxisType test_axis ) override { } ;
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// update gains for the rate ff up tune type
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void updating_rate_ff_up_all ( AxisType test_axis ) override ;
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// update gains for the angle p up tune type
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void updating_angle_p_up_all ( AxisType test_axis ) override ;
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// update gains for the angle p down tune type
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void updating_angle_p_down_all ( AxisType test_axis ) override { } ;
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// update gains for the max gain tune type
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void updating_max_gains_all ( AxisType test_axis ) override ;
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// set gains post tune for the tune type
void set_gains_post_tune ( AxisType test_axis ) override ;
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// reverse direction for twitch test
bool twitch_reverse_direction ( ) override { return positive_direction ; }
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// methods to log autotune summary data
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void Log_AutoTune ( ) override ;
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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 ) ;
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// methods to log autotune time history results for command, angular rate, and attitude.
void Log_AutoTuneDetails ( ) override ;
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void Log_Write_AutoTuneDetails ( float motor_cmd , float tgt_rate_rads , float rate_rads , float tgt_ang_rad , float ang_rad ) ;
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// methods to log autotune frequency response results
void Log_AutoTuneSweep ( ) override ;
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void Log_Write_AutoTuneSweep ( float freq , float gain , float phase ) ;
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// send intermittant updates to user on status of tune
void do_gcs_announcements ( ) override ;
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// send post test updates to user
void do_post_test_gcs_announcements ( ) override ;
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// set the tuning test sequence
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void set_tune_sequence ( ) override ;
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// get_axis_bitmask accessor
uint8_t get_axis_bitmask ( ) const override { return axis_bitmask ; }
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// get_testing_step_timeout_ms accessor
uint32_t get_testing_step_timeout_ms ( ) const override ;
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private :
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// 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
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void dwell_test_init ( float start_frq , float filt_freq ) ;
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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
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void angle_dwell_test_init ( float start_frq , float filt_freq ) ;
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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 ) ;
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// 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 ) ;
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// 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
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void updating_rate_p_up ( float & tune_p , float * freq , float * gain , float * phase , uint8_t & frq_cnt , max_gain_data & max_gain_p ) ;
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// 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
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void updating_rate_d_up ( float & tune_d , float * freq , float * gain , float * phase , uint8_t & frq_cnt , max_gain_data & max_gain_d ) ;
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// updating_angle_p_up - determines maximum angle p gain for pitch and roll
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void updating_angle_p_up ( float & tune_p , float * freq , float * gain , float * phase , uint8_t & frq_cnt ) ;
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// 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 ) ;
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// reset the max_gains update gain variables
void reset_maxgains_update_gain_variables ( ) ;
// reset the sweep variables
void reset_sweep_variables ( ) ;
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// exceeded_freq_range - ensures tuning remains inside frequency range
bool exceeded_freq_range ( float frequency ) ;
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// updating rate FF variables
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// flag for completion of the initial direction for the feedforward test
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bool first_dir_complete ;
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// feedforward gain resulting from testing in the initial direction
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float first_dir_rff ;
// updating max gain variables
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// flag for finding maximum p gain
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bool found_max_p ;
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// flag for finding maximum d gain
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bool found_max_d ;
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// flag for interpolating to find max response gain
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bool find_middle ;
// updating angle P up variables
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// track the maximum phase
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float phase_max ;
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// previous gain
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float sp_prev_gain ;
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// flag for finding the peak of the gain response
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bool find_peak ;
// updating angle P up yaw
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// counter value of previous good frequency
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uint8_t sp_prev_good_frq_cnt ;
// updating rate P up
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// counter value of previous good frequency
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uint8_t rp_prev_good_frq_cnt ;
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// previous gain
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float rp_prev_gain ;
// updating rate D up
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// counter value of previous good frequency
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uint8_t rd_prev_good_frq_cnt ;
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// previous gain
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float rd_prev_gain ;
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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 ;
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LowPassFilterFloat rate_request_cds ;
LowPassFilterFloat angle_request_cd ;
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// variables from dwell test
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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
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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
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// 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 ;
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// 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
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// 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 ;
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} ;