/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #ifndef __AP_INERTIALNAV_H__ #define __AP_INERTIALNAV_H__ #include #include // ArduPilot Mega IMU Library #include // ArduPilot Mega Barometer Library #include // FIFO buffer library #define AP_INTERTIALNAV_GRAVITY 9.80665 #define AP_INTERTIALNAV_TC_XY 3.0 // default time constant for complementary filter's X & Y axis #define AP_INTERTIALNAV_TC_Z 3.0 // default time constant for complementary filter's Z axis // #defines to control how often historical accel based positions are saved // so they can later be compared to laggy gps readings #define AP_INTERTIALNAV_SAVE_POS_AFTER_ITERATIONS 10 #define AP_INTERTIALNAV_GPS_LAG_IN_10HZ_INCREMENTS 4 // must not be larger than size of _hist_position_estimate_x and _hist_position_estimate_y /* * AP_InertialNav is an attempt to use accelerometers to augment other sensors to improve altitud e position hold */ class AP_InertialNav { public: // Constructor AP_InertialNav( AP_AHRS* ahrs, AP_InertialSensor* ins, AP_Baro* baro, GPS** gps_ptr ) : _ahrs(ahrs), _ins(ins), _baro(baro), _gps_ptr(gps_ptr), _xy_enabled(false), _gps_last_update(0), _baro_last_update(0) {} // Initialisation virtual void init(); // save_params - save all parameters to eeprom virtual void save_params(); // update - updates velocities and positions using latest info from accelerometers; virtual void update(float dt); // // XY Axis specific methods // // set time constant - set timeconstant used by complementary filter virtual void set_time_constant_xy( float time_constant_in_seconds ); // altitude_ok, position_ok - true if inertial based altitude and position can be trusted virtual bool position_ok(); // check_gps - check if new gps readings have arrived and use them to correct position estimates virtual void check_gps(); // correct_with_gps - modifies accelerometer offsets using gps. dt is time since last gps update virtual void correct_with_gps(int32_t lon, int32_t lat, float dt); // get latitude & longitude positions virtual int32_t get_latitude(); virtual int32_t get_longitude(); // set_current_position - all internal calculations are recorded as the distances from this point virtual void set_current_position(int32_t lon, int32_t lat); // get latitude & longitude positions from base location (in cm) virtual float get_latitude_diff(); virtual float get_longitude_diff(); // get velocity in latitude & longitude directions (in cm/s) virtual float get_latitude_velocity(); virtual float get_longitude_velocity(); // set velocity in latitude & longitude directions (in cm/s) virtual void set_velocity_xy(float x, float y); // // Z Axis methods // // set time constant - set timeconstant used by complementary filter virtual void set_time_constant_z( float time_constant_in_seconds ); // altitude_ok, position_ok - true if inertial based altitude and position can be trusted virtual bool altitude_ok() { return true; } // check_baro - check if new baro readings have arrived and use them to correct vertical accelerometer offsets virtual void check_baro(); // correct_with_baro - modifies accelerometer offsets using barometer. dt is time since last baro reading virtual void correct_with_baro(float baro_alt, float dt); // get_altitude - get latest altitude estimate in cm virtual float get_altitude() { return _position_base.z + _position_correction.z; } virtual void set_altitude( float new_altitude); // get_velocity_z - get latest climb rate (in cm/s) virtual float get_velocity_z() { return _velocity.z; } virtual void set_velocity_z( float new_velocity ); // class level parameters static const struct AP_Param::GroupInfo var_info[]; // public variables AP_Vector3f accel_correction; // acceleration corrections Vector3f accel_correction_ef; // earth frame accelerometer corrections. here for logging purposes only protected: virtual void update_gains(); // update_gains - update gains from time constant (given in seconds) AP_AHRS* _ahrs; // pointer to ahrs object AP_InertialSensor* _ins; // pointer to inertial sensor AP_Baro* _baro; // pointer to barometer GPS** _gps_ptr; // pointer to pointer to gps // XY Axis specific variables bool _xy_enabled; // xy position estimates enabled AP_Float _time_constant_xy; // time constant for horizontal corrections float _k1_xy; // gain for horizontal position correction float _k2_xy; // gain for horizontal velocity correction float _k3_xy; // gain for horizontal accelerometer offset correction uint32_t _gps_last_update; // system time of last gps update uint32_t _gps_last_time; // time of last gps update according to the gps itself uint8_t _historic_xy_counter; // counter used to slow saving of position estimates for later comparison to gps AP_BufferFloat_Size5 _hist_position_estimate_x; // buffer of historic accel based position to account for lag AP_BufferFloat_Size5 _hist_position_estimate_y; // buffer of historic accel based position to account for lag int32_t _base_lat; // base latitude int32_t _base_lon; // base longitude float _lon_to_m_scaling; // conversion of longitude to meters // Z Axis specific variables AP_Float _time_constant_z; // time constant for vertical corrections float _k1_z; // gain for vertical position correction float _k2_z; // gain for vertical velocity correction float _k3_z; // gain for vertical accelerometer offset correction uint32_t _baro_last_update; // time of last barometer update AP_BufferFloat_Size15 _hist_position_estimate_z; // buffer of historic accel based altitudes to account for lag // general variables Vector3f _position_base; // position estimate Vector3f _position_correction; // sum of correction to _comp_h from delayed 1st order samples Vector3f _velocity; // latest velocity estimate (integrated from accelerometer values) }; #endif // __AP_INERTIALNAV_H__