Paparazzi UAS  v4.2.2_stable-4-gcc32f65
Paparazzi is a free software Unmanned Aircraft System.
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ins_arduimu_basic.c File Reference
#include <stdbool.h>
#include "modules/ins/ins_arduimu_basic.h"
#include "mcu_periph/i2c.h"
#include "estimator.h"
#include "subsystems/gps.h"
#include "generated/airframe.h"
#include "inter_mcu.h"
#include "math/pprz_algebra_int.h"
+ Include dependency graph for ins_arduimu_basic.c:

Go to the source code of this file.

Macros

#define NB_DATA   9
 
#define ARDUIMU_I2C_DEV   i2c0
 
#define ArduIMU_SLAVE_ADDR   0x22
 
#define HIGH_ACCEL_LOW_SPEED   15.0
 
#define HIGH_ACCEL_LOW_SPEED_RESUME   4.0
 
#define HIGH_ACCEL_HIGH_THRUST   (0.8*MAX_PPRZ)
 
#define HIGH_ACCEL_HIGH_THRUST_RESUME   (0.1*MAX_PPRZ)
 
#define FillBufWith32bit(_buf, _index, _value)
 

Functions

void ArduIMU_init (void)
 
void ArduIMU_periodicGPS (void)
 
void ArduIMU_periodic (void)
 
void ArduIMU_event (void)
 

Variables

struct i2c_transaction ardu_gps_trans
 
struct i2c_transaction ardu_ins_trans
 
static int16_t recievedData [NB_DATA]
 
struct FloatEulers arduimu_eulers
 ArduIMU simulation. More...
 
struct FloatRates arduimu_rates
 
struct FloatVect3 arduimu_accel
 
float ins_roll_neutral
 
float ins_pitch_neutral
 
bool_t arduimu_calibrate_neutrals
 
bool_t high_accel_done
 
bool_t high_accel_flag
 

Macro Definition Documentation

#define ARDUIMU_I2C_DEV   i2c0

Definition at line 43 of file ins_arduimu_basic.c.

Referenced by ArduIMU_periodic(), and ArduIMU_periodicGPS().

#define ArduIMU_SLAVE_ADDR   0x22

Definition at line 49 of file ins_arduimu_basic.c.

Referenced by ArduIMU_periodic(), and ArduIMU_periodicGPS().

#define FillBufWith32bit (   _buf,
  _index,
  _value 
)
Value:
{ \
_buf[_index] = (uint8_t) (_value); \
_buf[_index+1] = (uint8_t) ((_value) >> 8); \
_buf[_index+2] = (uint8_t) ((_value) >> 16); \
_buf[_index+3] = (uint8_t) ((_value) >> 24); \
}
unsigned char uint8_t
Definition: types.h:14

Definition at line 100 of file ins_arduimu_basic.c.

Referenced by ArduIMU_periodicGPS().

#define HIGH_ACCEL_HIGH_THRUST   (0.8*MAX_PPRZ)

Definition at line 79 of file ins_arduimu_basic.c.

Referenced by ArduIMU_periodicGPS(), and Drift_correction().

#define HIGH_ACCEL_HIGH_THRUST_RESUME   (0.1*MAX_PPRZ)

Definition at line 80 of file ins_arduimu_basic.c.

Referenced by ArduIMU_periodicGPS(), and Drift_correction().

#define HIGH_ACCEL_LOW_SPEED   15.0

Definition at line 77 of file ins_arduimu_basic.c.

Referenced by ArduIMU_periodicGPS(), and Drift_correction().

#define HIGH_ACCEL_LOW_SPEED_RESUME   4.0

Definition at line 78 of file ins_arduimu_basic.c.

#define NB_DATA   9

Definition at line 40 of file ins_arduimu_basic.c.

Referenced by ArduIMU_periodic().

Function Documentation

Variable Documentation

struct i2c_transaction ardu_gps_trans

Definition at line 60 of file ins_arduimu_basic.c.

Referenced by ArduIMU_event(), ArduIMU_init(), and ArduIMU_periodicGPS().

struct i2c_transaction ardu_ins_trans

Definition at line 61 of file ins_arduimu_basic.c.

Referenced by ArduIMU_event(), ArduIMU_init(), and ArduIMU_periodic().

struct FloatVect3 arduimu_accel

Definition at line 67 of file ins_arduimu_basic.c.

bool_t arduimu_calibrate_neutrals

Definition at line 74 of file ins_arduimu_basic.c.

struct FloatEulers arduimu_eulers

ArduIMU simulation.

Sim provides attitude and rates.

Definition at line 65 of file ins_arduimu_basic.c.

struct FloatRates arduimu_rates

Definition at line 66 of file ins_arduimu_basic.c.

bool_t high_accel_done

Definition at line 81 of file ins_arduimu_basic.c.

Referenced by ahrs_init(), ArduIMU_init(), ArduIMU_periodicGPS(), and Drift_correction().

bool_t high_accel_flag

Definition at line 82 of file ins_arduimu_basic.c.

Referenced by ahrs_init(), ArduIMU_init(), ArduIMU_periodicGPS(), and Drift_correction().

float ins_pitch_neutral

Definition at line 70 of file ins_arduimu_basic.c.

float ins_roll_neutral

Definition at line 69 of file ins_arduimu_basic.c.

int16_t recievedData[NB_DATA]
static

Definition at line 63 of file ins_arduimu_basic.c.

Referenced by ArduIMU_event().