ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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pv2_nav_t Struct Reference

#include <proto_v2.h>

Data Fields

uint8_t fix
 < 0x08 NAV
 
uint8_t sats
 
uint16_t hdop_x100
 
int32_t lat_e7
 
int32_t lon_e7
 
int32_t alt_msl_cm
 
int16_t vel_ned_cms [3]
 
uint16_t tof_mm
 0xFFFF n/a
 
uint8_t flow_q
 0xFF n/a
 
uint32_t baro_pa
 
uint16_t wind_cms
 0xFFFF n/a
 

Detailed Description

Definition at line 204 of file proto_v2.h.

Field Documentation

◆ fix

uint8_t pv2_nav_t::fix

< 0x08 NAV

0xFF = no GNSS hardware

Definition at line 205 of file proto_v2.h.

◆ sats

uint8_t pv2_nav_t::sats

Definition at line 206 of file proto_v2.h.

◆ hdop_x100

uint16_t pv2_nav_t::hdop_x100

Definition at line 207 of file proto_v2.h.

◆ lat_e7

int32_t pv2_nav_t::lat_e7

Definition at line 208 of file proto_v2.h.

◆ lon_e7

int32_t pv2_nav_t::lon_e7

Definition at line 208 of file proto_v2.h.

◆ alt_msl_cm

int32_t pv2_nav_t::alt_msl_cm

Definition at line 209 of file proto_v2.h.

◆ vel_ned_cms

int16_t pv2_nav_t::vel_ned_cms[3]

Definition at line 210 of file proto_v2.h.

◆ tof_mm

uint16_t pv2_nav_t::tof_mm

0xFFFF n/a

Definition at line 211 of file proto_v2.h.

◆ flow_q

uint8_t pv2_nav_t::flow_q

0xFF n/a

Definition at line 212 of file proto_v2.h.

◆ baro_pa

uint32_t pv2_nav_t::baro_pa

Definition at line 213 of file proto_v2.h.

◆ wind_cms

uint16_t pv2_nav_t::wind_cms

0xFFFF n/a

Definition at line 214 of file proto_v2.h.


The documentation for this struct was generated from the following file: