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ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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Initial conditions, typically from calib_finish() More...
#include <iekf.h>
Data Fields | |
| float | R0 [9] |
| float | b0 [3] |
| float | g_ref [3] |
| accelerometer direction at rest, world frame | |
| float | m_ref [3] |
| magnetic field direction, world frame | |
| float | nom_acc |
| nominal magnitudes for the adaptive gating | |
| float | nom_mag |
Initial conditions, typically from calib_finish()
| float iekf_seed_t::R0[9] |
Definition at line 88 of file iekf.h.
Referenced by tlm_build_init().
| float iekf_seed_t::b0[3] |
Definition at line 89 of file iekf.h.
Referenced by tlm_build_init().
| float iekf_seed_t::g_ref[3] |
accelerometer direction at rest, world frame
Definition at line 90 of file iekf.h.
Referenced by tlm_build_init().
| float iekf_seed_t::m_ref[3] |
magnetic field direction, world frame
Definition at line 91 of file iekf.h.
Referenced by tlm_build_init().
| float iekf_seed_t::nom_acc |
nominal magnitudes for the adaptive gating
Definition at line 92 of file iekf.h.
Referenced by tlm_build_init().
| float iekf_seed_t::nom_mag |
Definition at line 93 of file iekf.h.
Referenced by tlm_build_init().