ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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cal_sample_t Struct Reference

#include <calib_mgr.h>

Data Fields

float acc [3]
 g, body
 
float gyro [3]
 rad/s, body
 
float mag [3]
 uT, body (axis map applied, no hard/soft iron)
 
float q [4]
 attitude, body -> world NWU [w x y z]
 
uint8_t mag_new
 
uint8_t running
 estimator running
 

Detailed Description

Definition at line 47 of file calib_mgr.h.

Field Documentation

◆ acc

float cal_sample_t::acc[3]

g, body

Definition at line 48 of file calib_mgr.h.

Referenced by on_state().

◆ gyro

float cal_sample_t::gyro[3]

rad/s, body

Definition at line 49 of file calib_mgr.h.

Referenced by on_state().

◆ mag

float cal_sample_t::mag[3]

uT, body (axis map applied, no hard/soft iron)

Definition at line 50 of file calib_mgr.h.

Referenced by on_state().

◆ q

float cal_sample_t::q[4]

attitude, body -> world NWU [w x y z]

Definition at line 51 of file calib_mgr.h.

Referenced by on_state().

◆ mag_new

uint8_t cal_sample_t::mag_new

Definition at line 52 of file calib_mgr.h.

Referenced by on_state().

◆ running

uint8_t cal_sample_t::running

estimator running

Definition at line 53 of file calib_mgr.h.

Referenced by on_state().


The documentation for this struct was generated from the following file: