mirror of https://github.com/ArduPilot/ardupilot
164 lines
4.2 KiB
C++
164 lines
4.2 KiB
C++
#ifndef AP_DCM_h
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#define AP_DCM_h
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// temporarily include all other classes here
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// since this naming is a bit off from the
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// convention and the AP_DCM should be the top
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// header file
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#include "AP_DCM_HIL.h"
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#include "../FastSerial/FastSerial.h"
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#include "../AP_Math/AP_Math.h"
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#include <inttypes.h>
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#include "../AP_Compass/AP_Compass.h"
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#include "../AP_ADC/AP_ADC.h"
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#include "../AP_GPS/AP_GPS.h"
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#include "../AP_IMU/AP_IMU.h"
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#if defined(ARDUINO) && ARDUINO >= 100
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#include "Arduino.h"
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#else
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#include "WProgram.h"
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#endif
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class AP_DCM
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{
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public:
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// Constructors
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AP_DCM(IMU *imu, GPS *&gps) :
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_kp_roll_pitch(12.0),
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_ki_roll_pitch(0.0006),
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_kp_yaw(3.0),
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_ki_yaw(0.003),
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_gps(gps),
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_imu(imu),
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_dcm_matrix(1, 0, 0,
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0, 1, 0,
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0, 0, 1),
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_health(1.),
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_toggle(0)
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{}
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// Accessors
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// return the smoothed gyro vector corrected for drift
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Vector3f get_gyro(void) {return _omega_smoothed; }
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Matrix3f get_dcm_matrix(void) {return _dcm_matrix; }
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Matrix3f get_dcm_transposed(void) {Matrix3f temp = _dcm_matrix; return temp.transpose();}
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// return the current drift correction integrator value
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Vector3f get_integrator(void) {return _omega_I; }
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float get_health(void) {return _health;}
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void set_centripetal(bool b) {_centripetal = b;}
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bool get_centripetal(void) {return _centripetal;}
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void set_compass(Compass *compass);
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// Methods
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void update_DCM(uint8_t drift_correction_frequency=1);
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void update_DCM_fast(void);
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void matrix_reset(bool recover_eulers = false);
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long roll_sensor; // Degrees * 100
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long pitch_sensor; // Degrees * 100
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long yaw_sensor; // Degrees * 100
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float roll; // Radians
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float pitch; // Radians
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float yaw; // Radians
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uint8_t gyro_sat_count;
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uint8_t renorm_range_count;
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uint8_t renorm_blowup_count;
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float kp_roll_pitch() { return _kp_roll_pitch; }
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void kp_roll_pitch(float v) { _kp_roll_pitch = v; }
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float ki_roll_pitch() { return _ki_roll_pitch; }
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void ki_roll_pitch(float v) { _ki_roll_pitch = v; }
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float kp_yaw() { return _kp_yaw; }
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void kp_yaw(float v) { _kp_yaw = v; }
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float ki_yaw() { return _ki_yaw; }
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void ki_yaw(float v) { _ki_yaw = v; }
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// status reporting
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float get_accel_weight(void);
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float get_renorm_val(void);
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float get_error_rp(void);
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float get_error_yaw(void);
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private:
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float _kp_roll_pitch;
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float _ki_roll_pitch;
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float _kp_yaw;
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float _ki_yaw;
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bool _have_initial_yaw;
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// Methods
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void read_adc_raw(void);
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void accel_adjust(Vector3f &accel);
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float read_adc(int select);
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void matrix_update(float _G_Dt);
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void normalize(void);
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void check_matrix(void);
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bool renorm(Vector3f const &a, Vector3f &result);
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void drift_correction(float deltat);
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void euler_angles(void);
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// max rate of gyro drift in degrees/s/s
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static const float _gyro_drift_rate = 0.04;
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// members
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Compass * _compass;
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// note: we use ref-to-pointer here so that our caller can change the GPS without our noticing
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// IMU under us without our noticing.
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GPS *&_gps; // note: this is a reference to a pointer owned by the caller
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IMU *_imu;
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Matrix3f _dcm_matrix;
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// sum of accel vectors between drift_correction() calls
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// this allows the drift correction to run at a different rate
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// to the main DCM update code
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Vector3f _accel_vector;
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Vector3f _accel_sum;
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Vector3f _gyro_vector; // Store the gyros turn rate in a vector
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Vector3f _omega_P; // Omega Proportional correction
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Vector3f _omega_I; // Omega Integrator correction
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Vector3f _omega_integ_corr; // Partially corrected Gyro_Vector data - used for centrepetal correction
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Vector3f _omega; // Corrected Gyro_Vector data
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Vector3f _omega_sum;
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Vector3f _omega_smoothed;
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float _health;
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bool _centripetal;
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uint8_t _toggle;
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// state to support status reporting
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float _renorm_val_sum;
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uint16_t _renorm_val_count;
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float _error_rp_sum;
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uint16_t _error_rp_count;
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float _error_yaw_sum;
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uint16_t _error_yaw_count;
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// time in micros when we last got a compass fix
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uint32_t _compass_last_update;
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// time in millis when we last got a GPS heading
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uint32_t _gps_last_update;
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// counter of calls to update_DCM() without drift correction
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uint8_t _drift_correction_count;
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float _drift_correction_time;
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};
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#endif
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