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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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# ifndef __AP_INERTIAL_SENSOR_H__
# define __AP_INERTIAL_SENSOR_H__
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// Gyro and Accelerometer calibration criteria
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# define AP_INERTIAL_SENSOR_ACCEL_TOT_MAX_OFFSET_CHANGE 4.0f
# define AP_INERTIAL_SENSOR_ACCEL_MAX_OFFSET 250.0f
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/**
maximum number of INS instances available on this platform . If more
than 1 then redundent sensors may be available
*/
# if CONFIG_HAL_BOARD == HAL_BOARD_PX4
# define INS_MAX_INSTANCES 2
# else
# define INS_MAX_INSTANCES 1
# endif
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# include <stdint.h>
# include <AP_HAL.h>
# include <AP_Math.h>
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# include "AP_InertialSensor_UserInteract.h"
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/* AP_InertialSensor is an abstraction for gyro and accel measurements
* which are correctly aligned to the body axes and scaled to SI units .
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*
* Gauss - Newton accel calibration routines borrowed from Rolfe Schmidt
* blog post describing the method : http : //chionophilous.wordpress.com/2011/10/24/accelerometer-calibration-iv-1-implementing-gauss-newton-on-an-atmega/
* original sketch available at http : //rolfeschmidt.com/mathtools/skimetrics/adxl_gn_calibration.pde
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*/
class AP_InertialSensor
{
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public :
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AP_InertialSensor ( ) ;
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enum Start_style {
COLD_START = 0 ,
WARM_START
} ;
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// the rate that updates will be available to the application
enum Sample_rate {
RATE_50HZ ,
RATE_100HZ ,
RATE_200HZ
} ;
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/// Perform startup initialisation.
///
/// Called to initialise the state of the IMU.
///
/// For COLD_START, implementations using real sensors can assume
/// that the airframe is stationary and nominally oriented.
///
/// For WARM_START, no assumptions should be made about the
/// orientation or motion of the airframe. Calibration should be
/// as for the previous COLD_START call.
///
/// @param style The initialisation startup style.
///
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virtual void init ( Start_style style ,
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Sample_rate sample_rate ) ;
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/// Perform cold startup initialisation for just the accelerometers.
///
/// @note This should not be called unless ::init has previously
/// been called, as ::init may perform other work.
///
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virtual void init_accel ( ) ;
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# if !defined( __AVR_ATmega1280__ )
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// perform accelerometer calibration including providing user instructions
// and feedback
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virtual bool calibrate_accel ( AP_InertialSensor_UserInteract * interact ,
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float & trim_roll ,
float & trim_pitch ) ;
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# endif
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/// calibrated - returns true if the accelerometers have been calibrated
///
/// @note this should not be called while flying because it reads from the eeprom which can be slow
///
bool calibrated ( ) ;
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/// Perform cold-start initialisation for just the gyros.
///
/// @note This should not be called unless ::init has previously
/// been called, as ::init may perform other work
///
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virtual void init_gyro ( void ) ;
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/// Fetch the current gyro values
///
/// @returns vector of rotational rates in radians/sec
///
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const Vector3f & get_gyro ( uint8_t i ) const { return _gyro [ i ] ; }
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const Vector3f & get_gyro ( void ) const { return get_gyro ( _get_primary_gyro ( ) ) ; }
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virtual void set_gyro ( const Vector3f & gyro ) { }
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// set gyro offsets in radians/sec
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const Vector3f & get_gyro_offsets ( uint8_t i ) const { return _gyro_offset [ i ] ; }
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const Vector3f & get_gyro_offsets ( void ) const { return get_gyro_offsets ( _get_primary_gyro ( ) ) ; }
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/// Fetch the current accelerometer values
///
/// @returns vector of current accelerations in m/s/s
///
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const Vector3f & get_accel ( uint8_t i ) const { return _accel [ i ] ; }
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const Vector3f & get_accel ( void ) const { return get_accel ( _get_primary_accel ( ) ) ; }
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virtual void set_accel ( const Vector3f & accel ) { }
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// multi-device interface
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virtual bool get_gyro_health ( uint8_t instance ) const { return true ; }
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bool get_gyro_health ( void ) const { return get_gyro_health ( _get_primary_gyro ( ) ) ; }
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virtual uint8_t get_gyro_count ( void ) const { return 1 ; } ;
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virtual bool get_accel_health ( uint8_t instance ) const { return true ; }
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bool get_accel_health ( void ) const { return get_accel_health ( _get_primary_accel ( ) ) ; }
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virtual uint8_t get_accel_count ( void ) const { return 1 ; } ;
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// get accel offsets in m/s/s
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const Vector3f & get_accel_offsets ( uint8_t i ) const { return _accel_offset [ i ] ; }
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const Vector3f & get_accel_offsets ( void ) const { return get_accel_offsets ( _get_primary_accel ( ) ) ; }
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// get accel scale
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const Vector3f & get_accel_scale ( uint8_t i ) const { return _accel_scale [ i ] ; }
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const Vector3f & get_accel_scale ( void ) const { return get_accel_scale ( _get_primary_accel ( ) ) ; }
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/* Update the sensor data, so that getters are nonblocking.
* Returns a bool of whether data was updated or not .
*/
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virtual bool update ( ) = 0 ;
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/* get_delta_time returns the time period in seconds
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* overwhich the sensor data was collected
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*/
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virtual float get_delta_time ( ) = 0 ;
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// return the maximum gyro drift rate in radians/s/s. This
// depends on what gyro chips are being used
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virtual float get_gyro_drift_rate ( void ) = 0 ;
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// wait for a sample to be available, with timeout in milliseconds
virtual bool wait_for_sample ( uint16_t timeout_ms ) = 0 ;
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// class level parameters
static const struct AP_Param : : GroupInfo var_info [ ] ;
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// set overall board orientation
void set_board_orientation ( enum Rotation orientation ) {
_board_orientation = orientation ;
}
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// override default filter frequency
void set_default_filter ( float filter_hz ) {
if ( ! _mpu6000_filter . load ( ) ) {
_mpu6000_filter . set ( filter_hz ) ;
}
}
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virtual uint16_t error_count ( void ) const { return 0 ; }
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virtual bool healthy ( void ) const { return get_gyro_health ( ) & & get_accel_health ( ) ; }
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protected :
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virtual uint8_t _get_primary_gyro ( void ) const { return 0 ; }
virtual uint8_t _get_primary_accel ( void ) const { return 0 ; }
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// sensor specific init to be overwritten by descendant classes
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virtual uint16_t _init_sensor ( Sample_rate sample_rate ) = 0 ;
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// no-save implementations of accel and gyro initialisation routines
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virtual void _init_accel ( ) ;
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virtual void _init_gyro ( ) ;
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# if !defined( __AVR_ATmega1280__ )
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// Calibration routines borrowed from Rolfe Schmidt
// blog post describing the method: http://chionophilous.wordpress.com/2011/10/24/accelerometer-calibration-iv-1-implementing-gauss-newton-on-an-atmega/
// original sketch available at http://rolfeschmidt.com/mathtools/skimetrics/adxl_gn_calibration.pde
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// _calibrate_accel - perform low level accel calibration
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virtual bool _calibrate_accel ( Vector3f accel_sample [ 6 ] , Vector3f & accel_offsets , Vector3f & accel_scale ) ;
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virtual void _calibrate_update_matrices ( float dS [ 6 ] , float JS [ 6 ] [ 6 ] , float beta [ 6 ] , float data [ 3 ] ) ;
virtual void _calibrate_reset_matrices ( float dS [ 6 ] , float JS [ 6 ] [ 6 ] ) ;
virtual void _calibrate_find_delta ( float dS [ 6 ] , float JS [ 6 ] [ 6 ] , float delta [ 6 ] ) ;
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virtual void _calculate_trim ( Vector3f accel_sample , float & trim_roll , float & trim_pitch ) ;
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# endif
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// save parameters to eeprom
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void _save_parameters ( ) ;
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// Most recent accelerometer reading obtained by ::update
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Vector3f _accel [ INS_MAX_INSTANCES ] ;
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// previous accelerometer reading obtained by ::update
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Vector3f _previous_accel [ INS_MAX_INSTANCES ] ;
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// Most recent gyro reading obtained by ::update
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Vector3f _gyro [ INS_MAX_INSTANCES ] ;
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// product id
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AP_Int16 _product_id ;
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// accelerometer scaling and offsets
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AP_Vector3f _accel_scale [ INS_MAX_INSTANCES ] ;
AP_Vector3f _accel_offset [ INS_MAX_INSTANCES ] ;
AP_Vector3f _gyro_offset [ INS_MAX_INSTANCES ] ;
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// filtering frequency (0 means default)
AP_Int8 _mpu6000_filter ;
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// board orientation from AHRS
enum Rotation _board_orientation ;
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} ;
# include "AP_InertialSensor_Oilpan.h"
# include "AP_InertialSensor_MPU6000.h"
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# include "AP_InertialSensor_HIL.h"
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# include "AP_InertialSensor_PX4.h"
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# include "AP_InertialSensor_UserInteract_Stream.h"
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# include "AP_InertialSensor_UserInteract_MAVLink.h"
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# include "AP_InertialSensor_Flymaple.h"
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# include "AP_InertialSensor_L3G4200D.h"
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# endif // __AP_INERTIAL_SENSOR_H__