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ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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#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 | |
Definition at line 47 of file calib_mgr.h.
| float cal_sample_t::acc[3] |
| float cal_sample_t::gyro[3] |
| 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().
| 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().
| uint8_t cal_sample_t::mag_new |
Definition at line 52 of file calib_mgr.h.
Referenced by on_state().
| uint8_t cal_sample_t::running |