Mirror
/
ardupilot
mirror of https://github.com/ArduPilot/ardupilot
5
0
Fork 0
Code Issues Packages Projects Releases Wiki Activity
ardupilot/libraries/AP_InertialNav/AP_InertialNav.h

324 lines
13 KiB
C++
Raw Blame History

/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#ifndef __AP_INERTIALNAV_H__
#define __AP_INERTIALNAV_H__
#include <AP_AHRS.h>
#include <AP_InertialSensor.h> // ArduPilot Mega IMU Library
#include <AP_Baro.h> // ArduPilot Mega Barometer Library
#include <AP_Buffer.h> // FIFO buffer library
#include <AP_GPS_Glitch.h> // GPS Glitch detection library
#define AP_INTERTIALNAV_TC_XY 2.5f // default time constant for complementary filter's X & Y axis
#define AP_INTERTIALNAV_TC_Z 5.0f // 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
#define AP_INTERTIALNAV_GPS_TIMEOUT_MS 300 // timeout after which position error from GPS will fall to zero
/*
* AP_InertialNav blends accelerometer data with gps and barometer data to improve altitude and position hold.
*
* Most of the functions have to be called at 100Hz. (see defines above)
*
* The accelerometer values are integrated over time to approximate velocity and position.
* The inaccurcy of these estimates grows over time due to noisy sensor data.
* To improve the accuracy, baro and gps readings are used:
* An error value is calculated as the difference between the sensor's measurement and the last position estimation.
* This value is weighted with a gain factor and incorporated into the new estimation
*/
class AP_InertialNav
{
public:
// Constructor
AP_InertialNav( const AP_AHRS &ahrs, AP_Baro &baro, GPS*& gps, GPS_Glitch& gps_glitch ) :
_ahrs(ahrs),
_baro(baro),
_gps(gps),
_xy_enabled(false),
_gps_last_update(0),
_gps_last_time(0),
_historic_xy_counter(0),
_baro_last_update(0),
_glitch_detector(gps_glitch),
_error_count(0)
{
AP_Param::setup_object_defaults(this, var_info);
}
/**
* initializes the object.
*
* AP_InertialNav::set_home_position(int32_t, int32_t) should be called later,
* to enable all "horizontal related" getter-methods.
*/
void init();
/**
* update - updates velocity and position estimates using latest info from accelerometers
* augmented with gps and baro readings
*
* @param dt : time since last update in seconds
*/
void update(float dt);
//
// XY Axis specific methods
//
/**
* set_time_constant_xy - sets time constant used by complementary filter for horizontal position estimate
*
* smaller values means higher influence of gps on position estimation
* bigger values favor the integrated accelerometer data for position estimation
*
* @param time_constant_in_seconds : constant in seconds; 0 < constant < 30 must hold
*/
void set_time_constant_xy( float time_constant_in_seconds );
/**
* position_ok - true if inertial based altitude and position can be trusted
* @return
*/
bool position_ok() const;
/**
* check_gps - checks if new gps readings have arrived and calls correct_with_gps to
* calculate the horizontal position error
* @see correct_with_gps(int32_t lon, int32_t lat, float dt);
*/
void check_gps();
/**
* correct_with_gps - calculates horizontal position error using gps
*
* @param now : current time since boot in milliseconds
* @param lon : longitude in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
* @param lat : latitude in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
*/
void correct_with_gps(uint32_t now, int32_t lon, int32_t lat);
/**
* get_position - returns the current position relative to the home location in cm.
*
* the home location was set with AP_InertialNav::set_home_position(int32_t, int32_t)
*
* @return
*/
const Vector3f& get_position() const { return _position; }
/**
* get_latitude - returns the latitude of the current position estimation in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
* @return
*/
int32_t get_latitude() const;
/**
* get_longitude - returns the longitude of the current position estimation in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
* @return
*/
int32_t get_longitude() const;
/**
* set_home_position - sets home position
*
* all internal calculations are recorded as the distances from this point.
*
* @param lon : longitude in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
* @param lat : latitude in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
*/
void set_home_position(int32_t lon, int32_t lat);
/**
* get_latitude_diff - returns the current latitude difference from the home location.
*
* @return difference in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
*/
float get_latitude_diff() const;
/**
* get_longitude_diff - returns the current longitude difference from the home location.
*
* @return difference in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
*/
float get_longitude_diff() const;
/**
* get_velocity - returns the current velocity in cm/s
*
* @return velocity vector:
* .x : latitude velocity in cm/s
* .y : longitude velocity in cm/s
* .z : vertical velocity in cm/s
*/
const Vector3f& get_velocity() const { return _velocity; }
/**
* get_velocity_xy - returns the current horizontal velocity in cm/s
*
* @returns the current horizontal velocity in cm/s
*/
float get_velocity_xy();
/**
* set_velocity_xy - overwrites the current horizontal velocity in cm/s
*
* @param x : latitude velocity in cm/s
* @param y : longitude velocity in cm/s
*/
void set_velocity_xy(float x, float y);
//
// Z Axis methods
//
/**
* set_time_constant_z - sets timeconstant used by complementary filter for vertical position estimation
*
* smaller values means higher influence of barometer in altitude estimation
* bigger values favor the integrated accelerometer data for altitude estimation
*
* @param time_constant_in_seconds : constant in s; 0 < constant < 30 must hold
*/
void set_time_constant_z( float time_constant_in_seconds );
/**
* altitude_ok - returns true if inertial based altitude and position can be trusted
* @return
*/
bool altitude_ok() const { return true; }
/**
* check_baro - checks if new baro readings have arrived and calls correct_with_baro to
* calculate the vertical position error
*
* @see correct_with_baro(float baro_alt, float dt);
*/
void check_baro();
/**
* correct_with_baro - calculates vertical position error using barometer.
*
* @param baro_alt : altitude in cm
* @param dt : time since last baro reading in s
*/
void correct_with_baro(float baro_alt, float dt);
/**
* get_altitude - get latest altitude estimate in cm
* @return
*/
float get_altitude() const { return _position.z; }
/**
* set_altitude - overwrites the current altitude value.
*
* @param new_altitude : altitude in cm
*/
void set_altitude( float new_altitude);
/**
* get_velocity_z - returns the current climbrate.
*
* @see get_velocity().z
*
* @return climbrate in cm/s
*/
float get_velocity_z() const { return _velocity.z; }
/**
* set_velocity_z - overwrites the current climbrate.
*
* @param new_velocity : climbrate in cm/s
*/
void set_velocity_z( float new_velocity );
/**
* error_count - returns number of missed updates from GPS
*/
uint8_t error_count() const { return _error_count; }
/**
* ignore_next_error - the next error (if it occurs immediately) will not be added to the error count
*/
void ignore_next_error() { _flags.ignore_error = 7; }
// class level parameters
static const struct AP_Param::GroupInfo var_info[];
// public variables
Vector3f accel_correction_ef; // earth frame accelerometer corrections. here for logging purposes only
protected:
/**
* update gains from time constant.
*
* The time constants (in s) can be set with the following methods:
*
* @see: AP_InertialNav::set_time_constant_xy(float)
* @see: AP_InertialNav::set_time_constant_z(float)
*/
void update_gains();
/**
* set_position_xy - overwrites the current position relative to the home location in cm
*
* the home location was set with AP_InertialNav::set_home_location(int32_t, int32_t)
*
* @param x : relative latitude position in cm
* @param y : relative longitude position in cm
*/
void set_position_xy(float x, float y);
// structure for holding flags
struct InertialNav_flags {
uint8_t gps_glitching : 1; // 1 if glitch detector was previously indicating a gps glitch
uint8_t ignore_error : 3; // the number of iterations for which we should ignore errors
} _flags;
const AP_AHRS &_ahrs; // reference to ahrs object
AP_Baro &_baro; // reference to barometer
GPS*& _gps; // pointer to gps
// XY Axis specific variables
bool _xy_enabled; // xy position estimates enabled
AP_Float _time_constant_xy; // time constant for horizontal corrections in s
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 in ms
uint32_t _gps_last_time; // time of last gps update according to the gps itself in ms
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 gpslag
AP_BufferFloat_Size5 _hist_position_estimate_y; // buffer of historic accel based position to account for gps lag
int32_t _base_lat; // base latitude (home location) in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
int32_t _base_lon; // base longitude (home location) in 100 nano degrees (i.e. degree value multiplied by 10,000,000)
float _lon_to_cm_scaling; // conversion of longitude to centimeters
// Z Axis specific variables
AP_Float _time_constant_z; // time constant for vertical corrections in s
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 in ms
AP_BufferFloat_Size15 _hist_position_estimate_z; // buffer of historic accel based altitudes to account for barometer lag
// general variables
Vector3f _position_base; // (uncorrected) position estimate in cm - relative to the home location (_base_lat, _base_lon, 0)
Vector3f _position_correction; // sum of corrections to _position_base from delayed 1st order samples in cm
Vector3f _velocity; // latest velocity estimate (integrated from accelerometer values) in cm/s
Vector3f _position_error; // current position error in cm - is set by the check_* methods and used by update method to calculate the correction terms
Vector3f _position; // sum(_position_base, _position_correction) - corrected position estimate in cm - relative to the home location (_base_lat, _base_lon, 0)
// error handling
GPS_Glitch& _glitch_detector; // GPS Glitch detector
uint8_t _error_count; // number of missed GPS updates
};
#endif // __AP_INERTIALNAV_H__
Reference in New Issue View Git Blame Copy Permalink