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ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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#include <proto_v2.h>
Data Fields | |
| uint8_t | arm |
| < 0x06 FLIGHT | |
| uint8_t | mode |
| uint8_t | autom |
| uint8_t | failsafe |
| uint16_t | flags |
| uint8_t | input |
| uint16_t | flight_time_s |
| int32_t | alt_rel_cm |
| int16_t | vz_cms |
| uint16_t | ground_speed_cms |
| uint16_t | heading_cdeg |
| uint16_t | home_dist_m |
| 0xFFFF n/a | |
| uint16_t | home_bearing_cdeg |
| uint16_t | rth_eta_s |
| 0xFFFF n/a | |
Definition at line 179 of file proto_v2.h.
| uint8_t pv2_flight_t::arm |
| uint8_t pv2_flight_t::mode |
Definition at line 180 of file proto_v2.h.
Referenced by send_flight().
| uint8_t pv2_flight_t::autom |
Definition at line 180 of file proto_v2.h.
Referenced by send_flight().
| uint8_t pv2_flight_t::failsafe |
Definition at line 180 of file proto_v2.h.
Referenced by send_flight().
| uint16_t pv2_flight_t::flags |
Definition at line 181 of file proto_v2.h.
Referenced by send_flight().
| uint8_t pv2_flight_t::input |
Definition at line 182 of file proto_v2.h.
Referenced by send_flight().
| uint16_t pv2_flight_t::flight_time_s |
Definition at line 183 of file proto_v2.h.
Referenced by send_flight().
| int32_t pv2_flight_t::alt_rel_cm |
Definition at line 184 of file proto_v2.h.
Referenced by send_flight().
| int16_t pv2_flight_t::vz_cms |
Definition at line 185 of file proto_v2.h.
Referenced by send_flight().
| uint16_t pv2_flight_t::ground_speed_cms |
Definition at line 186 of file proto_v2.h.
Referenced by send_flight().
| uint16_t pv2_flight_t::heading_cdeg |
Definition at line 187 of file proto_v2.h.
Referenced by send_flight().
| uint16_t pv2_flight_t::home_dist_m |
| uint16_t pv2_flight_t::home_bearing_cdeg |
Definition at line 189 of file proto_v2.h.
Referenced by send_flight().
| uint16_t pv2_flight_t::rth_eta_s |