mirror of https://github.com/ArduPilot/ardupilot
158 lines
7.4 KiB
C++
158 lines
7.4 KiB
C++
/// -*- 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
|
|
|
|
#define AP_INTERTIALNAV_GRAVITY 9.80665f
|
|
#define AP_INTERTIALNAV_TC_XY 3.0f // default time constant for complementary filter's X & Y axis
|
|
#define AP_INTERTIALNAV_TC_Z 7.0f // default time constant for complementary filter's Z axis
|
|
|
|
#define AP_INTERTIALNAV_ACCEL_CORR_MAX 100.0 // max allowed accelerometer offset correction
|
|
|
|
// #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
|
|
|
|
#define AP_INERTIALNAV_LATLON_TO_CM 1.1113175f
|
|
|
|
/*
|
|
* 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)
|
|
{
|
|
AP_Param::setup_object_defaults(this, var_info);
|
|
}
|
|
|
|
// 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
|
|
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)
|
|
Vector3f _position_error;
|
|
};
|
|
|
|
#endif // __AP_INERTIALNAV_H__
|