#ifndef AP_AHRS_MPU6000_H #define AP_AHRS_MPU6000_H /* DCM based AHRS (Attitude Heading Reference System) interface for ArduPilot This library is free software; you can redistribute it and/or modify it under the terms of the GNU Lesser General Public License as published by the Free Software Foundation; either version 2.1 of the License, or (at your option) any later version. */ #define GYRO_BIAS_FROM_GRAVITY_RATE 4 // Rate of the gyro bias from gravity correction (200Hz/4) => 50Hz #define HEADING_UNKNOWN -9999 // Initial value to detect that compass correction is not initialized // max rate of gyro drift in gyro_LSB_units/s (16.4LSB = 1deg/s) static const float _MPU6000_gyro_drift_rate = 0.5; // This correspond to 0.03 degrees/s/s; class AP_AHRS_MPU6000 : public AP_AHRS { public: // Constructors AP_AHRS_MPU6000(AP_IMU_INS *imu, GPS *&gps, AP_InertialSensor_MPU6000 *mpu6000) : AP_AHRS(imu, gps), _mpu6000(mpu6000) { _dcm_matrix.identity(); // these are experimentally derived from the simulator // with large drift levels _ki = 0.0087; _ki_yaw = 0.01; // dmp related variable initialisation _gyro_bias_from_gravity_gain = 0.008; _compass_bias_time = 0; } // initialisation routine to start MPU6000's dmp void init(); // return the smoothed gyro vector corrected for drift Vector3f get_gyro(void) {return _imu->get_gyro(); } Matrix3f get_dcm_matrix(void) {return _dcm_matrix; } // return the current drift correction integrator value Vector3f get_gyro_drift(void) {return _omega_I; } // Methods void update(void); void reset(bool recover_eulers = false); // push offsets down from IMU to INS (required so MPU6000 can perform it's own attitude estimation) void push_offsets_to_ins(); void push_gains_to_dmp(); // status reporting float get_error_rp(void); float get_error_yaw(void); private: float _ki; float _ki_yaw; AP_InertialSensor_MPU6000 *_mpu6000; // Methods void drift_correction(float deltat); // Compass correction variables. TO-DO: move or replace? float wrap_PI(float angle_in_radians); // TO-DO: move this to standard AP_AHRS methods long _compass_bias_time; void drift_correction_yaw(void); float yaw_error_compass(); void euler_angles(void); Vector3f _accel_filtered; int16_t _accel_filtered_samples; float _gyro_bias[3]; // bias_tracking float _gyro_bias_from_gravity_gain; // bias correction algorithm gain uint8_t _gyro_bias_from_gravity_counter; // primary representation of attitude Matrix3f _dcm_matrix; Vector3f _accel_vector; // current accel vector Vector3f _omega_I; // Omega Integrator correction Vector3f _omega_I_sum; float _omega_I_sum_time; // state to support status reporting float _error_yaw_sum; uint16_t _error_yaw_count; float _error_yaw_last; }; #endif // AP_AHRS_MPU6000_H