ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
Loading...
Searching...
No Matches
ctrl_rate_in_t Struct Reference

#include <control_hooks.h>

Data Fields

float gyro [3]
 rad/s: mean of the step samples, estimated bias removed
 
float dt
 s
 
uint32_t step
 

Detailed Description

Definition at line 19 of file control_hooks.h.

Field Documentation

◆ gyro

float ctrl_rate_in_t::gyro[3]

rad/s: mean of the step samples, estimated bias removed

Definition at line 20 of file control_hooks.h.

Referenced by on_step().

◆ dt

float ctrl_rate_in_t::dt

s

Definition at line 21 of file control_hooks.h.

Referenced by on_step().

◆ step

uint32_t ctrl_rate_in_t::step

Definition at line 22 of file control_hooks.h.

Referenced by on_step().


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