ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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pv2_cal_gyro_t Struct Reference

#include <proto_v2.h>

Data Fields

uint16_t remaining_ms
 
int16_t bias_mdps [3]
 
uint16_t noise_mdps
 
int16_t temp_cc
 

Detailed Description

Definition at line 273 of file proto_v2.h.

Field Documentation

◆ remaining_ms

uint16_t pv2_cal_gyro_t::remaining_ms

Definition at line 273 of file proto_v2.h.

◆ bias_mdps

int16_t pv2_cal_gyro_t::bias_mdps[3]

Definition at line 273 of file proto_v2.h.

◆ noise_mdps

uint16_t pv2_cal_gyro_t::noise_mdps

Definition at line 273 of file proto_v2.h.

◆ temp_cc

int16_t pv2_cal_gyro_t::temp_cc

Definition at line 273 of file proto_v2.h.


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