#ifndef AP_DCM_FW_h #define AP_DCM_FW_h #include #include #include #include "WProgram.h" #include #include #include #include class AP_DCM_FW { public: // Constructors AP_DCM_FW(AP_ADC * adc, GPS *gps); // Constructor - no magnetometer AP_DCM_FW(AP_ADC * adc, GPS *gps, APM_Compass_Class *withCompass); // Constructor for case with magnetometer // Accessors Vector3f get_gyros(void); Vector3f get_accels(void); Matrix3f get_dcm_matrix(void); AP_IMU * get_imu(void); // Methods void quick_init(uint16_t *_offset_address); void gyro_init(uint16_t *_offset_address); void init(uint16_t *_offset_address); void update_DCM(float _G_Dt); long roll_sensor; // Degrees * 100 long pitch_sensor; // Degrees * 100 long yaw_sensor; // Degrees * 100 float roll; // Radians float pitch; // Radians float yaw; // Radians float imu_health; //Metric based on accel gain deweighting uint8_t gyro_sat_count; uint8_t adc_constraints; uint8_t renorm_sqrt_count; uint8_t renorm_blowup_count; private: // Methods void read_adc_raw(void); void accel_adjust(void); float read_adc(int select); void matrix_update(float _G_Dt); void normalize(void); Vector3f renorm(Vector3f const &a, int &problem); void drift_correction(void); void euler_angles(void); // members APM_Compass_Class *_compass; GPS *_gps; AP_IMU _imu; Matrix3f _dcm_matrix; Vector3f _accel_vector; // Store the acceleration in a vector Vector3f _gyro_vector; //Store the gyros turn rate in a vector Vector3f _omega_P; //Omega Proportional correction Vector3f _omega_I; //Omega Integrator correction Vector3f _omega_integ_corr; //Partially corrected Gyro_Vector data - used for centrepetal correction Vector3f _omega; //Corrected Gyro_Vector data Vector3f _error_roll_pitch; Vector3f _error_yaw; float _errorCourse; float _course_over_ground_x; //Course overground X axis float _course_over_ground_y; //Course overground Y axis }; #endif