![]() |
ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
|
#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 |
Definition at line 19 of file control_hooks.h.
| 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().
| float ctrl_rate_in_t::dt |
| uint32_t ctrl_rate_in_t::step |
Definition at line 22 of file control_hooks.h.
Referenced by on_step().