Data Fields
uint64_t	time_usec
	Timestamp (microseconds since UNIX epoch or microseconds since system boot) More...

float	attitude_quaternion [4]
	Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation) More...

float	rollspeed
	Body frame roll / phi angular speed (rad/s) More...

float	pitchspeed
	Body frame pitch / theta angular speed (rad/s) More...

float	yawspeed
	Body frame yaw / psi angular speed (rad/s) More...

int32_t	lat
	Latitude, expressed as * 1E7. More...

int32_t	lon
	Longitude, expressed as * 1E7. More...

int32_t	alt
	Altitude in meters, expressed as * 1000 (millimeters) More...

int16_t	vx
	Ground X Speed (Latitude), expressed as m/s * 100. More...

int16_t	vy
	Ground Y Speed (Longitude), expressed as m/s * 100. More...

int16_t	vz
	Ground Z Speed (Altitude), expressed as m/s * 100. More...

uint16_t	ind_airspeed
	Indicated airspeed, expressed as m/s * 100. More...

uint16_t	true_airspeed
	True airspeed, expressed as m/s * 100. More...

int16_t	xacc
	X acceleration (mg) More...

int16_t	yacc
	Y acceleration (mg) More...

int16_t	zacc
	Z acceleration (mg) More...

Field Documentation

int32_t __mavlink_hil_state_quaternion_t::alt

Altitude in meters, expressed as * 1000 (millimeters)

float __mavlink_hil_state_quaternion_t::attitude_quaternion[4]

Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)

uint16_t __mavlink_hil_state_quaternion_t::ind_airspeed

Indicated airspeed, expressed as m/s * 100.

int32_t __mavlink_hil_state_quaternion_t::lat

Latitude, expressed as * 1E7.

int32_t __mavlink_hil_state_quaternion_t::lon

Longitude, expressed as * 1E7.

float __mavlink_hil_state_quaternion_t::pitchspeed

Body frame pitch / theta angular speed (rad/s)

float __mavlink_hil_state_quaternion_t::rollspeed

Body frame roll / phi angular speed (rad/s)

uint64_t __mavlink_hil_state_quaternion_t::time_usec

Timestamp (microseconds since UNIX epoch or microseconds since system boot)

uint16_t __mavlink_hil_state_quaternion_t::true_airspeed

True airspeed, expressed as m/s * 100.

int16_t __mavlink_hil_state_quaternion_t::vx

Ground X Speed (Latitude), expressed as m/s * 100.

int16_t __mavlink_hil_state_quaternion_t::vy

Ground Y Speed (Longitude), expressed as m/s * 100.

int16_t __mavlink_hil_state_quaternion_t::vz

Ground Z Speed (Altitude), expressed as m/s * 100.

int16_t __mavlink_hil_state_quaternion_t::xacc

X acceleration (mg)

int16_t __mavlink_hil_state_quaternion_t::yacc

Y acceleration (mg)

float __mavlink_hil_state_quaternion_t::yawspeed

Body frame yaw / psi angular speed (rad/s)

int16_t __mavlink_hil_state_quaternion_t::zacc

Z acceleration (mg)

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

Data Fields