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ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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#include <calib.h>
Data Fields | |
| uint32_t | n |
| float | acc [CALIB_MAX_SAMPLES][3] |
| float | mag [CALIB_MAX_SAMPLES][3] |
| float | gyro_sum [3] |
| float | gyro_norm_max |
| uint32_t calib_t::n |
Definition at line 23 of file calib.h.
Referenced by calib_add(), calib_count(), and calib_finish().
| float calib_t::acc[CALIB_MAX_SAMPLES][3] |
Definition at line 24 of file calib.h.
Referenced by calib_add(), and calib_finish().
| float calib_t::mag[CALIB_MAX_SAMPLES][3] |
Definition at line 25 of file calib.h.
Referenced by calib_add(), and calib_finish().
| float calib_t::gyro_sum[3] |
Definition at line 26 of file calib.h.
Referenced by calib_add(), and calib_finish().
| float calib_t::gyro_norm_max |
Definition at line 27 of file calib.h.
Referenced by calib_add().