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Classes
struct	__mavlink_hil_state_quaternion_t
Defines
#define	MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION
#define	MAVLINK_MSG_HIL_STATE_QUATERNION_FIELD_ATTITUDE_QUATERNION_LEN 4
#define	MAVLINK_MSG_ID_115_CRC 4
#define	MAVLINK_MSG_ID_115_LEN 64
#define	MAVLINK_MSG_ID_HIL_STATE_QUATERNION 115
#define	MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC 4
#define	MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN 64
Typedefs
typedef struct __mavlink_hil_state_quaternion_t	mavlink_hil_state_quaternion_t
Functions
static void	mavlink_msg_hil_state_quaternion_decode (const mavlink_message_t msg, mavlink_hil_state_quaternion_t hil_state_quaternion)
	Decode a hil_state_quaternion message into a struct.
static uint16_t	mavlink_msg_hil_state_quaternion_encode (uint8_t system_id, uint8_t component_id, mavlink_message_t msg, const mavlink_hil_state_quaternion_t hil_state_quaternion)
	Encode a hil_state_quaternion struct.
static uint16_t	mavlink_msg_hil_state_quaternion_encode_chan (uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t msg, const mavlink_hil_state_quaternion_t hil_state_quaternion)
	Encode a hil_state_quaternion struct on a channel.
static int32_t	mavlink_msg_hil_state_quaternion_get_alt (const mavlink_message_t *msg)
	Get field alt from hil_state_quaternion message.
static uint16_t	mavlink_msg_hil_state_quaternion_get_attitude_quaternion (const mavlink_message_t msg, float attitude_quaternion)
	Get field attitude_quaternion from hil_state_quaternion message.
static uint16_t	mavlink_msg_hil_state_quaternion_get_ind_airspeed (const mavlink_message_t *msg)
	Get field ind_airspeed from hil_state_quaternion message.
static int32_t	mavlink_msg_hil_state_quaternion_get_lat (const mavlink_message_t *msg)
	Get field lat from hil_state_quaternion message.
static int32_t	mavlink_msg_hil_state_quaternion_get_lon (const mavlink_message_t *msg)
	Get field lon from hil_state_quaternion message.
static float	mavlink_msg_hil_state_quaternion_get_pitchspeed (const mavlink_message_t *msg)
	Get field pitchspeed from hil_state_quaternion message.
static float	mavlink_msg_hil_state_quaternion_get_rollspeed (const mavlink_message_t *msg)
	Get field rollspeed from hil_state_quaternion message.
static uint64_t	mavlink_msg_hil_state_quaternion_get_time_usec (const mavlink_message_t *msg)
	Send a hil_state_quaternion message.
static uint16_t	mavlink_msg_hil_state_quaternion_get_true_airspeed (const mavlink_message_t *msg)
	Get field true_airspeed from hil_state_quaternion message.
static int16_t	mavlink_msg_hil_state_quaternion_get_vx (const mavlink_message_t *msg)
	Get field vx from hil_state_quaternion message.
static int16_t	mavlink_msg_hil_state_quaternion_get_vy (const mavlink_message_t *msg)
	Get field vy from hil_state_quaternion message.
static int16_t	mavlink_msg_hil_state_quaternion_get_vz (const mavlink_message_t *msg)
	Get field vz from hil_state_quaternion message.
static int16_t	mavlink_msg_hil_state_quaternion_get_xacc (const mavlink_message_t *msg)
	Get field xacc from hil_state_quaternion message.
static int16_t	mavlink_msg_hil_state_quaternion_get_yacc (const mavlink_message_t *msg)
	Get field yacc from hil_state_quaternion message.
static float	mavlink_msg_hil_state_quaternion_get_yawspeed (const mavlink_message_t *msg)
	Get field yawspeed from hil_state_quaternion message.
static int16_t	mavlink_msg_hil_state_quaternion_get_zacc (const mavlink_message_t *msg)
	Get field zacc from hil_state_quaternion message.
static uint16_t	mavlink_msg_hil_state_quaternion_pack (uint8_t system_id, uint8_t component_id, mavlink_message_t msg, uint64_t time_usec, const float attitude_quaternion, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, uint16_t ind_airspeed, uint16_t true_airspeed, int16_t xacc, int16_t yacc, int16_t zacc)
	Pack a hil_state_quaternion message.
static uint16_t	mavlink_msg_hil_state_quaternion_pack_chan (uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t msg, uint64_t time_usec, const float attitude_quaternion, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, uint16_t ind_airspeed, uint16_t true_airspeed, int16_t xacc, int16_t yacc, int16_t zacc)
	Pack a hil_state_quaternion message on a channel.

Define Documentation

#define MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION

Value:

{ \
        "HIL_STATE_QUATERNION", \
        16, \
        {  { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \
         { "attitude_quaternion", NULL, MAVLINK_TYPE_FLOAT, 4, 8, offsetof(mavlink_hil_state_quaternion_t, attitude_quaternion) }, \
         { "rollspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_state_quaternion_t, rollspeed) }, \
         { "pitchspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_state_quaternion_t, pitchspeed) }, \
         { "yawspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_hil_state_quaternion_t, yawspeed) }, \
         { "lat", NULL, MAVLINK_TYPE_INT32_T, 0, 36, offsetof(mavlink_hil_state_quaternion_t, lat) }, \
         { "lon", NULL, MAVLINK_TYPE_INT32_T, 0, 40, offsetof(mavlink_hil_state_quaternion_t, lon) }, \
         { "alt", NULL, MAVLINK_TYPE_INT32_T, 0, 44, offsetof(mavlink_hil_state_quaternion_t, alt) }, \
         { "vx", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_hil_state_quaternion_t, vx) }, \
         { "vy", NULL, MAVLINK_TYPE_INT16_T, 0, 50, offsetof(mavlink_hil_state_quaternion_t, vy) }, \
         { "vz", NULL, MAVLINK_TYPE_INT16_T, 0, 52, offsetof(mavlink_hil_state_quaternion_t, vz) }, \
         { "ind_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 54, offsetof(mavlink_hil_state_quaternion_t, ind_airspeed) }, \
         { "true_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 56, offsetof(mavlink_hil_state_quaternion_t, true_airspeed) }, \
         { "xacc", NULL, MAVLINK_TYPE_INT16_T, 0, 58, offsetof(mavlink_hil_state_quaternion_t, xacc) }, \
         { "yacc", NULL, MAVLINK_TYPE_INT16_T, 0, 60, offsetof(mavlink_hil_state_quaternion_t, yacc) }, \
         { "zacc", NULL, MAVLINK_TYPE_INT16_T, 0, 62, offsetof(mavlink_hil_state_quaternion_t, zacc) }, \
         } \
}

Definition at line 33 of file mavlink_msg_hil_state_quaternion.h.

#define MAVLINK_MSG_HIL_STATE_QUATERNION_FIELD_ATTITUDE_QUATERNION_LEN 4

Definition at line 31 of file mavlink_msg_hil_state_quaternion.h.

#define MAVLINK_MSG_ID_115_CRC 4

Definition at line 29 of file mavlink_msg_hil_state_quaternion.h.

#define MAVLINK_MSG_ID_115_LEN 64

Definition at line 26 of file mavlink_msg_hil_state_quaternion.h.

#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION 115

Definition at line 3 of file mavlink_msg_hil_state_quaternion.h.

#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC 4

Definition at line 28 of file mavlink_msg_hil_state_quaternion.h.

#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN 64

Definition at line 25 of file mavlink_msg_hil_state_quaternion.h.

Typedef Documentation

typedef struct __mavlink_hil_state_quaternion_t mavlink_hil_state_quaternion_t

Function Documentation

static void mavlink_msg_hil_state_quaternion_decode	(	const mavlink_message_t *	msg,
		mavlink_hil_state_quaternion_t *	hil_state_quaternion
	)		`[inline, static]`

Decode a hil_state_quaternion message into a struct.

Parameters:

msg	The message to decode
hil_state_quaternion	C-struct to decode the message contents into

Definition at line 539 of file mavlink_msg_hil_state_quaternion.h.

static uint16_t mavlink_msg_hil_state_quaternion_encode	(	uint8_t	system_id,
		uint8_t	component_id,
		mavlink_message_t *	msg,
		const mavlink_hil_state_quaternion_t *	hil_state_quaternion
	)		`[inline, static]`

Encode a hil_state_quaternion struct.

Parameters:

system_id	ID of this system
component_id	ID of this component (e.g. 200 for IMU)
msg	The MAVLink message to compress the data into
hil_state_quaternion	C-struct to read the message contents from

Definition at line 215 of file mavlink_msg_hil_state_quaternion.h.

static uint16_t mavlink_msg_hil_state_quaternion_encode_chan	(	uint8_t	system_id,
		uint8_t	component_id,
		uint8_t	chan,
		mavlink_message_t *	msg,
		const mavlink_hil_state_quaternion_t *	hil_state_quaternion
	)		`[inline, static]`

Encode a hil_state_quaternion struct on a channel.

Parameters:

system_id	ID of this system
component_id	ID of this component (e.g. 200 for IMU)
chan	The MAVLink channel this message will be sent over
msg	The MAVLink message to compress the data into
hil_state_quaternion	C-struct to read the message contents from

Definition at line 229 of file mavlink_msg_hil_state_quaternion.h.

static int32_t mavlink_msg_hil_state_quaternion_get_alt ( const mavlink_message_t * msg ) [inline, static]

Get field alt from hil_state_quaternion message.

Returns:: Altitude in meters, expressed as * 1000 (millimeters)

Definition at line 448 of file mavlink_msg_hil_state_quaternion.h.

static uint16_t mavlink_msg_hil_state_quaternion_get_attitude_quaternion	(	const mavlink_message_t *	msg,
		float *	attitude_quaternion
	)		`[inline, static]`

Get field attitude_quaternion from hil_state_quaternion message.

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

Definition at line 388 of file mavlink_msg_hil_state_quaternion.h.

static uint16_t mavlink_msg_hil_state_quaternion_get_ind_airspeed ( const mavlink_message_t * msg ) [inline, static]

Get field ind_airspeed from hil_state_quaternion message.

Returns:: Indicated airspeed, expressed as m/s * 100

Definition at line 488 of file mavlink_msg_hil_state_quaternion.h.

static int32_t mavlink_msg_hil_state_quaternion_get_lat ( const mavlink_message_t * msg ) [inline, static]

Get field lat from hil_state_quaternion message.

Returns:: Latitude, expressed as * 1E7

Definition at line 428 of file mavlink_msg_hil_state_quaternion.h.

static int32_t mavlink_msg_hil_state_quaternion_get_lon ( const mavlink_message_t * msg ) [inline, static]

Get field lon from hil_state_quaternion message.

Returns:: Longitude, expressed as * 1E7

Definition at line 438 of file mavlink_msg_hil_state_quaternion.h.

static float mavlink_msg_hil_state_quaternion_get_pitchspeed ( const mavlink_message_t * msg ) [inline, static]

Get field pitchspeed from hil_state_quaternion message.

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

Definition at line 408 of file mavlink_msg_hil_state_quaternion.h.

static float mavlink_msg_hil_state_quaternion_get_rollspeed ( const mavlink_message_t * msg ) [inline, static]

Get field rollspeed from hil_state_quaternion message.

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

Definition at line 398 of file mavlink_msg_hil_state_quaternion.h.

static uint64_t mavlink_msg_hil_state_quaternion_get_time_usec ( const mavlink_message_t * msg ) [inline, static]

Send a hil_state_quaternion message.

Parameters:

chan	MAVLink channel to send the message
time_usec	Timestamp (microseconds since UNIX epoch or microseconds since system boot)
attitude_quaternion	Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)
rollspeed	Body frame roll / phi angular speed (rad/s)
pitchspeed	Body frame pitch / theta angular speed (rad/s)
yawspeed	Body frame yaw / psi angular speed (rad/s)
lat	Latitude, expressed as * 1E7
lon	Longitude, expressed as * 1E7
alt	Altitude in meters, expressed as * 1000 (millimeters)
vx	Ground X Speed (Latitude), expressed as m/s * 100
vy	Ground Y Speed (Longitude), expressed as m/s * 100
vz	Ground Z Speed (Altitude), expressed as m/s * 100
ind_airspeed	Indicated airspeed, expressed as m/s * 100
true_airspeed	True airspeed, expressed as m/s * 100
xacc	X acceleration (mg)
yacc	Y acceleration (mg)
zacc	Z acceleration (mg) Get field time_usec from hil_state_quaternion message

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

Definition at line 378 of file mavlink_msg_hil_state_quaternion.h.

static uint16_t mavlink_msg_hil_state_quaternion_get_true_airspeed ( const mavlink_message_t * msg ) [inline, static]

Get field true_airspeed from hil_state_quaternion message.

Returns:: True airspeed, expressed as m/s * 100

Definition at line 498 of file mavlink_msg_hil_state_quaternion.h.

static int16_t mavlink_msg_hil_state_quaternion_get_vx ( const mavlink_message_t * msg ) [inline, static]

Get field vx from hil_state_quaternion message.

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

Definition at line 458 of file mavlink_msg_hil_state_quaternion.h.

static int16_t mavlink_msg_hil_state_quaternion_get_vy ( const mavlink_message_t * msg ) [inline, static]

Get field vy from hil_state_quaternion message.

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

Definition at line 468 of file mavlink_msg_hil_state_quaternion.h.

static int16_t mavlink_msg_hil_state_quaternion_get_vz ( const mavlink_message_t * msg ) [inline, static]

Get field vz from hil_state_quaternion message.

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

Definition at line 478 of file mavlink_msg_hil_state_quaternion.h.

static int16_t mavlink_msg_hil_state_quaternion_get_xacc ( const mavlink_message_t * msg ) [inline, static]

Get field xacc from hil_state_quaternion message.

Returns:: X acceleration (mg)

Definition at line 508 of file mavlink_msg_hil_state_quaternion.h.

static int16_t mavlink_msg_hil_state_quaternion_get_yacc ( const mavlink_message_t * msg ) [inline, static]

Get field yacc from hil_state_quaternion message.

Returns:: Y acceleration (mg)

Definition at line 518 of file mavlink_msg_hil_state_quaternion.h.

static float mavlink_msg_hil_state_quaternion_get_yawspeed ( const mavlink_message_t * msg ) [inline, static]

Get field yawspeed from hil_state_quaternion message.

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

Definition at line 418 of file mavlink_msg_hil_state_quaternion.h.

static int16_t mavlink_msg_hil_state_quaternion_get_zacc ( const mavlink_message_t * msg ) [inline, static]

Get field zacc from hil_state_quaternion message.

Returns:: Z acceleration (mg)

Definition at line 528 of file mavlink_msg_hil_state_quaternion.h.

static uint16_t mavlink_msg_hil_state_quaternion_pack	(	uint8_t	system_id,
		uint8_t	component_id,
		mavlink_message_t *	msg,
		uint64_t	time_usec,
		const float *	attitude_quaternion,
		float	rollspeed,
		float	pitchspeed,
		float	yawspeed,
		int32_t	lat,
		int32_t	lon,
		int32_t	alt,
		int16_t	vx,
		int16_t	vy,
		int16_t	vz,
		uint16_t	ind_airspeed,
		uint16_t	true_airspeed,
		int16_t	xacc,
		int16_t	yacc,
		int16_t	zacc
	)		`[inline, static]`

Pack a hil_state_quaternion message.

Parameters:

system_id	ID of this system
component_id	ID of this component (e.g. 200 for IMU)
msg	The MAVLink message to compress the data into
time_usec	Timestamp (microseconds since UNIX epoch or microseconds since system boot)
attitude_quaternion	Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)
rollspeed	Body frame roll / phi angular speed (rad/s)
pitchspeed	Body frame pitch / theta angular speed (rad/s)
yawspeed	Body frame yaw / psi angular speed (rad/s)
lat	Latitude, expressed as * 1E7
lon	Longitude, expressed as * 1E7
alt	Altitude in meters, expressed as * 1000 (millimeters)
vx	Ground X Speed (Latitude), expressed as m/s * 100
vy	Ground Y Speed (Longitude), expressed as m/s * 100
vz	Ground Z Speed (Altitude), expressed as m/s * 100
ind_airspeed	Indicated airspeed, expressed as m/s * 100
true_airspeed	True airspeed, expressed as m/s * 100
xacc	X acceleration (mg)
yacc	Y acceleration (mg)
zacc	Z acceleration (mg)

Returns:: length of the message in bytes (excluding serial stream start sign)

Definition at line 80 of file mavlink_msg_hil_state_quaternion.h.

static uint16_t mavlink_msg_hil_state_quaternion_pack_chan	(	uint8_t	system_id,
		uint8_t	component_id,
		uint8_t	chan,
		mavlink_message_t *	msg,
		uint64_t	time_usec,
		const float *	attitude_quaternion,
		float	rollspeed,
		float	pitchspeed,
		float	yawspeed,
		int32_t	lat,
		int32_t	lon,
		int32_t	alt,
		int16_t	vx,
		int16_t	vy,
		int16_t	vz,
		uint16_t	ind_airspeed,
		uint16_t	true_airspeed,
		int16_t	xacc,
		int16_t	yacc,
		int16_t	zacc
	)		`[inline, static]`

Pack a hil_state_quaternion message on a channel.

Parameters:

system_id	ID of this system
component_id	ID of this component (e.g. 200 for IMU)
chan	The MAVLink channel this message will be sent over
msg	The MAVLink message to compress the data into
time_usec	Timestamp (microseconds since UNIX epoch or microseconds since system boot)
attitude_quaternion	Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)
rollspeed	Body frame roll / phi angular speed (rad/s)
pitchspeed	Body frame pitch / theta angular speed (rad/s)
yawspeed	Body frame yaw / psi angular speed (rad/s)
lat	Latitude, expressed as * 1E7
lon	Longitude, expressed as * 1E7
alt	Altitude in meters, expressed as * 1000 (millimeters)
vx	Ground X Speed (Latitude), expressed as m/s * 100
vy	Ground Y Speed (Longitude), expressed as m/s * 100
vz	Ground Z Speed (Altitude), expressed as m/s * 100
ind_airspeed	Indicated airspeed, expressed as m/s * 100
true_airspeed	True airspeed, expressed as m/s * 100
xacc	X acceleration (mg)
yacc	Y acceleration (mg)
zacc	Z acceleration (mg)

Returns:: length of the message in bytes (excluding serial stream start sign)

Definition at line 155 of file mavlink_msg_hil_state_quaternion.h.

Classes

Defines

Typedefs

Functions

Define Documentation

Typedef Documentation

Function Documentation