mavlink_msg_hil_state_quaternion.h File Reference

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Data Structures
struct	__mavlink_hil_state_quaternion_t

Macros
#define	MAVLINK_MSG_ID_HIL_STATE_QUATERNION   115
#define	MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN   64
#define	MAVLINK_MSG_ID_115_LEN   64
#define	MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC   4
#define	MAVLINK_MSG_ID_115_CRC   4
#define	MAVLINK_MSG_HIL_STATE_QUATERNION_FIELD_ATTITUDE_QUATERNION_LEN   4
#define	MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION

Typedefs
typedef struct __mavlink_hil_state_quaternion_t	mavlink_hil_state_quaternion_t

Macro Definition 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) }, \
         } \
}

#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

Typedef Documentation

typedef struct __mavlink_hil_state_quaternion_t mavlink_hil_state_quaternion_t