EV2_GCS_Mavlink/v2.0/common/mavlink_msg_gimbal_device_attitude_status.h

#pragma once
// MESSAGE GIMBAL_DEVICE_ATTITUDE_STATUS PACKING

#define MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS 285


typedef struct __mavlink_gimbal_device_attitude_status_t {
 uint32_t time_boot_ms; /*< [ms] Timestamp (time since system boot).*/
 float q[4]; /*<  Quaternion components, w, x, y, z (1 0 0 0 is the null-rotation). The frame is described in the message description.*/
 float angular_velocity_x; /*< [rad/s] X component of angular velocity (positive: rolling to the right). The frame is described in the message description. NaN if unknown.*/
 float angular_velocity_y; /*< [rad/s] Y component of angular velocity (positive: pitching up). The frame is described in the message description. NaN if unknown.*/
 float angular_velocity_z; /*< [rad/s] Z component of angular velocity (positive: yawing to the right). The frame is described in the message description. NaN if unknown.*/
 uint32_t failure_flags; /*<  Failure flags (0 for no failure)*/
 uint16_t flags; /*<  Current gimbal flags set.*/
 uint8_t target_system; /*<  System ID*/
 uint8_t target_component; /*<  Component ID*/
 float delta_yaw; /*< [rad] Yaw angle relating the quaternions in earth and body frames (see message description). NaN if unknown.*/
 float delta_yaw_velocity; /*< [rad/s] Yaw angular velocity relating the angular velocities in earth and body frames (see message description). NaN if unknown.*/
 uint8_t gimbal_device_id; /*<  This field is to be used if the gimbal manager and the gimbal device are the same component and hence have the same component ID. This field is then set a number between 1-6. If the component ID is separate, this field is not required and must be set to 0.*/
} mavlink_gimbal_device_attitude_status_t;

#define MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN 49
#define MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN 40
#define MAVLINK_MSG_ID_285_LEN 49
#define MAVLINK_MSG_ID_285_MIN_LEN 40

#define MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC 137
#define MAVLINK_MSG_ID_285_CRC 137

#define MAVLINK_MSG_GIMBAL_DEVICE_ATTITUDE_STATUS_FIELD_Q_LEN 4

#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_GIMBAL_DEVICE_ATTITUDE_STATUS { \
    285, \
    "GIMBAL_DEVICE_ATTITUDE_STATUS", \
    12, \
    {  { "target_system", NULL, MAVLINK_TYPE_UINT8_T, 0, 38, offsetof(mavlink_gimbal_device_attitude_status_t, target_system) }, \
         { "target_component", NULL, MAVLINK_TYPE_UINT8_T, 0, 39, offsetof(mavlink_gimbal_device_attitude_status_t, target_component) }, \
         { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_gimbal_device_attitude_status_t, time_boot_ms) }, \
         { "flags", NULL, MAVLINK_TYPE_UINT16_T, 0, 36, offsetof(mavlink_gimbal_device_attitude_status_t, flags) }, \
         { "q", NULL, MAVLINK_TYPE_FLOAT, 4, 4, offsetof(mavlink_gimbal_device_attitude_status_t, q) }, \
         { "angular_velocity_x", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_gimbal_device_attitude_status_t, angular_velocity_x) }, \
         { "angular_velocity_y", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_gimbal_device_attitude_status_t, angular_velocity_y) }, \
         { "angular_velocity_z", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_gimbal_device_attitude_status_t, angular_velocity_z) }, \
         { "failure_flags", NULL, MAVLINK_TYPE_UINT32_T, 0, 32, offsetof(mavlink_gimbal_device_attitude_status_t, failure_flags) }, \
         { "delta_yaw", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_gimbal_device_attitude_status_t, delta_yaw) }, \
         { "delta_yaw_velocity", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_gimbal_device_attitude_status_t, delta_yaw_velocity) }, \
         { "gimbal_device_id", NULL, MAVLINK_TYPE_UINT8_T, 0, 48, offsetof(mavlink_gimbal_device_attitude_status_t, gimbal_device_id) }, \
         } \
}
#else
#define MAVLINK_MESSAGE_INFO_GIMBAL_DEVICE_ATTITUDE_STATUS { \
    "GIMBAL_DEVICE_ATTITUDE_STATUS", \
    12, \
    {  { "target_system", NULL, MAVLINK_TYPE_UINT8_T, 0, 38, offsetof(mavlink_gimbal_device_attitude_status_t, target_system) }, \
         { "target_component", NULL, MAVLINK_TYPE_UINT8_T, 0, 39, offsetof(mavlink_gimbal_device_attitude_status_t, target_component) }, \
         { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_gimbal_device_attitude_status_t, time_boot_ms) }, \
         { "flags", NULL, MAVLINK_TYPE_UINT16_T, 0, 36, offsetof(mavlink_gimbal_device_attitude_status_t, flags) }, \
         { "q", NULL, MAVLINK_TYPE_FLOAT, 4, 4, offsetof(mavlink_gimbal_device_attitude_status_t, q) }, \
         { "angular_velocity_x", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_gimbal_device_attitude_status_t, angular_velocity_x) }, \
         { "angular_velocity_y", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_gimbal_device_attitude_status_t, angular_velocity_y) }, \
         { "angular_velocity_z", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_gimbal_device_attitude_status_t, angular_velocity_z) }, \
         { "failure_flags", NULL, MAVLINK_TYPE_UINT32_T, 0, 32, offsetof(mavlink_gimbal_device_attitude_status_t, failure_flags) }, \
         { "delta_yaw", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_gimbal_device_attitude_status_t, delta_yaw) }, \
         { "delta_yaw_velocity", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_gimbal_device_attitude_status_t, delta_yaw_velocity) }, \
         { "gimbal_device_id", NULL, MAVLINK_TYPE_UINT8_T, 0, 48, offsetof(mavlink_gimbal_device_attitude_status_t, gimbal_device_id) }, \
         } \
}
#endif

/**
 * @brief Pack a gimbal_device_attitude_status message
 * @param system_id ID of this system
 * @param component_id ID of this component (e.g. 200 for IMU)
 * @param msg The MAVLink message to compress the data into
 *
 * @param target_system  System ID
 * @param target_component  Component ID
 * @param time_boot_ms [ms] Timestamp (time since system boot).
 * @param flags  Current gimbal flags set.
 * @param q  Quaternion components, w, x, y, z (1 0 0 0 is the null-rotation). The frame is described in the message description.
 * @param angular_velocity_x [rad/s] X component of angular velocity (positive: rolling to the right). The frame is described in the message description. NaN if unknown.
 * @param angular_velocity_y [rad/s] Y component of angular velocity (positive: pitching up). The frame is described in the message description. NaN if unknown.
 * @param angular_velocity_z [rad/s] Z component of angular velocity (positive: yawing to the right). The frame is described in the message description. NaN if unknown.
 * @param failure_flags  Failure flags (0 for no failure)
 * @param delta_yaw [rad] Yaw angle relating the quaternions in earth and body frames (see message description). NaN if unknown.
 * @param delta_yaw_velocity [rad/s] Yaw angular velocity relating the angular velocities in earth and body frames (see message description). NaN if unknown.
 * @param gimbal_device_id  This field is to be used if the gimbal manager and the gimbal device are the same component and hence have the same component ID. This field is then set a number between 1-6. If the component ID is separate, this field is not required and must be set to 0.
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_gimbal_device_attitude_status_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
                               uint8_t target_system, uint8_t target_component, uint32_t time_boot_ms, uint16_t flags, const float *q, float angular_velocity_x, float angular_velocity_y, float angular_velocity_z, uint32_t failure_flags, float delta_yaw, float delta_yaw_velocity, uint8_t gimbal_device_id)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_float(buf, 20, angular_velocity_x);
    _mav_put_float(buf, 24, angular_velocity_y);
    _mav_put_float(buf, 28, angular_velocity_z);
    _mav_put_uint32_t(buf, 32, failure_flags);
    _mav_put_uint16_t(buf, 36, flags);
    _mav_put_uint8_t(buf, 38, target_system);
    _mav_put_uint8_t(buf, 39, target_component);
    _mav_put_float(buf, 40, delta_yaw);
    _mav_put_float(buf, 44, delta_yaw_velocity);
    _mav_put_uint8_t(buf, 48, gimbal_device_id);
    _mav_put_float_array(buf, 4, q, 4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN);
#else
    mavlink_gimbal_device_attitude_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.angular_velocity_x = angular_velocity_x;
    packet.angular_velocity_y = angular_velocity_y;
    packet.angular_velocity_z = angular_velocity_z;
    packet.failure_flags = failure_flags;
    packet.flags = flags;
    packet.target_system = target_system;
    packet.target_component = target_component;
    packet.delta_yaw = delta_yaw;
    packet.delta_yaw_velocity = delta_yaw_velocity;
    packet.gimbal_device_id = gimbal_device_id;
    mav_array_memcpy(packet.q, q, sizeof(float)*4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN);
#endif

    msg->msgid = MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS;
    return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC);
}

/**
 * @brief Pack a gimbal_device_attitude_status message
 * @param system_id ID of this system
 * @param component_id ID of this component (e.g. 200 for IMU)
 * @param status MAVLink status structure
 * @param msg The MAVLink message to compress the data into
 *
 * @param target_system  System ID
 * @param target_component  Component ID
 * @param time_boot_ms [ms] Timestamp (time since system boot).
 * @param flags  Current gimbal flags set.
 * @param q  Quaternion components, w, x, y, z (1 0 0 0 is the null-rotation). The frame is described in the message description.
 * @param angular_velocity_x [rad/s] X component of angular velocity (positive: rolling to the right). The frame is described in the message description. NaN if unknown.
 * @param angular_velocity_y [rad/s] Y component of angular velocity (positive: pitching up). The frame is described in the message description. NaN if unknown.
 * @param angular_velocity_z [rad/s] Z component of angular velocity (positive: yawing to the right). The frame is described in the message description. NaN if unknown.
 * @param failure_flags  Failure flags (0 for no failure)
 * @param delta_yaw [rad] Yaw angle relating the quaternions in earth and body frames (see message description). NaN if unknown.
 * @param delta_yaw_velocity [rad/s] Yaw angular velocity relating the angular velocities in earth and body frames (see message description). NaN if unknown.
 * @param gimbal_device_id  This field is to be used if the gimbal manager and the gimbal device are the same component and hence have the same component ID. This field is then set a number between 1-6. If the component ID is separate, this field is not required and must be set to 0.
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_gimbal_device_attitude_status_pack_status(uint8_t system_id, uint8_t component_id, mavlink_status_t *_status, mavlink_message_t* msg,
                               uint8_t target_system, uint8_t target_component, uint32_t time_boot_ms, uint16_t flags, const float *q, float angular_velocity_x, float angular_velocity_y, float angular_velocity_z, uint32_t failure_flags, float delta_yaw, float delta_yaw_velocity, uint8_t gimbal_device_id)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_float(buf, 20, angular_velocity_x);
    _mav_put_float(buf, 24, angular_velocity_y);
    _mav_put_float(buf, 28, angular_velocity_z);
    _mav_put_uint32_t(buf, 32, failure_flags);
    _mav_put_uint16_t(buf, 36, flags);
    _mav_put_uint8_t(buf, 38, target_system);
    _mav_put_uint8_t(buf, 39, target_component);
    _mav_put_float(buf, 40, delta_yaw);
    _mav_put_float(buf, 44, delta_yaw_velocity);
    _mav_put_uint8_t(buf, 48, gimbal_device_id);
    _mav_put_float_array(buf, 4, q, 4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN);
#else
    mavlink_gimbal_device_attitude_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.angular_velocity_x = angular_velocity_x;
    packet.angular_velocity_y = angular_velocity_y;
    packet.angular_velocity_z = angular_velocity_z;
    packet.failure_flags = failure_flags;
    packet.flags = flags;
    packet.target_system = target_system;
    packet.target_component = target_component;
    packet.delta_yaw = delta_yaw;
    packet.delta_yaw_velocity = delta_yaw_velocity;
    packet.gimbal_device_id = gimbal_device_id;
    mav_array_memcpy(packet.q, q, sizeof(float)*4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN);
#endif

    msg->msgid = MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS;
#if MAVLINK_CRC_EXTRA
    return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC);
#else
    return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN);
#endif
}

/**
 * @brief Pack a gimbal_device_attitude_status message on a channel
 * @param system_id ID of this system
 * @param component_id ID of this component (e.g. 200 for IMU)
 * @param chan The MAVLink channel this message will be sent over
 * @param msg The MAVLink message to compress the data into
 * @param target_system  System ID
 * @param target_component  Component ID
 * @param time_boot_ms [ms] Timestamp (time since system boot).
 * @param flags  Current gimbal flags set.
 * @param q  Quaternion components, w, x, y, z (1 0 0 0 is the null-rotation). The frame is described in the message description.
 * @param angular_velocity_x [rad/s] X component of angular velocity (positive: rolling to the right). The frame is described in the message description. NaN if unknown.
 * @param angular_velocity_y [rad/s] Y component of angular velocity (positive: pitching up). The frame is described in the message description. NaN if unknown.
 * @param angular_velocity_z [rad/s] Z component of angular velocity (positive: yawing to the right). The frame is described in the message description. NaN if unknown.
 * @param failure_flags  Failure flags (0 for no failure)
 * @param delta_yaw [rad] Yaw angle relating the quaternions in earth and body frames (see message description). NaN if unknown.
 * @param delta_yaw_velocity [rad/s] Yaw angular velocity relating the angular velocities in earth and body frames (see message description). NaN if unknown.
 * @param gimbal_device_id  This field is to be used if the gimbal manager and the gimbal device are the same component and hence have the same component ID. This field is then set a number between 1-6. If the component ID is separate, this field is not required and must be set to 0.
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_gimbal_device_attitude_status_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
                               mavlink_message_t* msg,
                                   uint8_t target_system,uint8_t target_component,uint32_t time_boot_ms,uint16_t flags,const float *q,float angular_velocity_x,float angular_velocity_y,float angular_velocity_z,uint32_t failure_flags,float delta_yaw,float delta_yaw_velocity,uint8_t gimbal_device_id)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_float(buf, 20, angular_velocity_x);
    _mav_put_float(buf, 24, angular_velocity_y);
    _mav_put_float(buf, 28, angular_velocity_z);
    _mav_put_uint32_t(buf, 32, failure_flags);
    _mav_put_uint16_t(buf, 36, flags);
    _mav_put_uint8_t(buf, 38, target_system);
    _mav_put_uint8_t(buf, 39, target_component);
    _mav_put_float(buf, 40, delta_yaw);
    _mav_put_float(buf, 44, delta_yaw_velocity);
    _mav_put_uint8_t(buf, 48, gimbal_device_id);
    _mav_put_float_array(buf, 4, q, 4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN);
#else
    mavlink_gimbal_device_attitude_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.angular_velocity_x = angular_velocity_x;
    packet.angular_velocity_y = angular_velocity_y;
    packet.angular_velocity_z = angular_velocity_z;
    packet.failure_flags = failure_flags;
    packet.flags = flags;
    packet.target_system = target_system;
    packet.target_component = target_component;
    packet.delta_yaw = delta_yaw;
    packet.delta_yaw_velocity = delta_yaw_velocity;
    packet.gimbal_device_id = gimbal_device_id;
    mav_array_memcpy(packet.q, q, sizeof(float)*4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN);
#endif

    msg->msgid = MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS;
    return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC);
}

/**
 * @brief Encode a gimbal_device_attitude_status struct
 *
 * @param system_id ID of this system
 * @param component_id ID of this component (e.g. 200 for IMU)
 * @param msg The MAVLink message to compress the data into
 * @param gimbal_device_attitude_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_gimbal_device_attitude_status_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_gimbal_device_attitude_status_t* gimbal_device_attitude_status)
{
    return mavlink_msg_gimbal_device_attitude_status_pack(system_id, component_id, msg, gimbal_device_attitude_status->target_system, gimbal_device_attitude_status->target_component, gimbal_device_attitude_status->time_boot_ms, gimbal_device_attitude_status->flags, gimbal_device_attitude_status->q, gimbal_device_attitude_status->angular_velocity_x, gimbal_device_attitude_status->angular_velocity_y, gimbal_device_attitude_status->angular_velocity_z, gimbal_device_attitude_status->failure_flags, gimbal_device_attitude_status->delta_yaw, gimbal_device_attitude_status->delta_yaw_velocity, gimbal_device_attitude_status->gimbal_device_id);
}

/**
 * @brief Encode a gimbal_device_attitude_status struct on a channel
 *
 * @param system_id ID of this system
 * @param component_id ID of this component (e.g. 200 for IMU)
 * @param chan The MAVLink channel this message will be sent over
 * @param msg The MAVLink message to compress the data into
 * @param gimbal_device_attitude_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_gimbal_device_attitude_status_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_gimbal_device_attitude_status_t* gimbal_device_attitude_status)
{
    return mavlink_msg_gimbal_device_attitude_status_pack_chan(system_id, component_id, chan, msg, gimbal_device_attitude_status->target_system, gimbal_device_attitude_status->target_component, gimbal_device_attitude_status->time_boot_ms, gimbal_device_attitude_status->flags, gimbal_device_attitude_status->q, gimbal_device_attitude_status->angular_velocity_x, gimbal_device_attitude_status->angular_velocity_y, gimbal_device_attitude_status->angular_velocity_z, gimbal_device_attitude_status->failure_flags, gimbal_device_attitude_status->delta_yaw, gimbal_device_attitude_status->delta_yaw_velocity, gimbal_device_attitude_status->gimbal_device_id);
}

/**
 * @brief Encode a gimbal_device_attitude_status struct with provided status structure
 *
 * @param system_id ID of this system
 * @param component_id ID of this component (e.g. 200 for IMU)
 * @param status MAVLink status structure
 * @param msg The MAVLink message to compress the data into
 * @param gimbal_device_attitude_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_gimbal_device_attitude_status_encode_status(uint8_t system_id, uint8_t component_id, mavlink_status_t* _status, mavlink_message_t* msg, const mavlink_gimbal_device_attitude_status_t* gimbal_device_attitude_status)
{
    return mavlink_msg_gimbal_device_attitude_status_pack_status(system_id, component_id, _status, msg,  gimbal_device_attitude_status->target_system, gimbal_device_attitude_status->target_component, gimbal_device_attitude_status->time_boot_ms, gimbal_device_attitude_status->flags, gimbal_device_attitude_status->q, gimbal_device_attitude_status->angular_velocity_x, gimbal_device_attitude_status->angular_velocity_y, gimbal_device_attitude_status->angular_velocity_z, gimbal_device_attitude_status->failure_flags, gimbal_device_attitude_status->delta_yaw, gimbal_device_attitude_status->delta_yaw_velocity, gimbal_device_attitude_status->gimbal_device_id);
}

/**
 * @brief Send a gimbal_device_attitude_status message
 * @param chan MAVLink channel to send the message
 *
 * @param target_system  System ID
 * @param target_component  Component ID
 * @param time_boot_ms [ms] Timestamp (time since system boot).
 * @param flags  Current gimbal flags set.
 * @param q  Quaternion components, w, x, y, z (1 0 0 0 is the null-rotation). The frame is described in the message description.
 * @param angular_velocity_x [rad/s] X component of angular velocity (positive: rolling to the right). The frame is described in the message description. NaN if unknown.
 * @param angular_velocity_y [rad/s] Y component of angular velocity (positive: pitching up). The frame is described in the message description. NaN if unknown.
 * @param angular_velocity_z [rad/s] Z component of angular velocity (positive: yawing to the right). The frame is described in the message description. NaN if unknown.
 * @param failure_flags  Failure flags (0 for no failure)
 * @param delta_yaw [rad] Yaw angle relating the quaternions in earth and body frames (see message description). NaN if unknown.
 * @param delta_yaw_velocity [rad/s] Yaw angular velocity relating the angular velocities in earth and body frames (see message description). NaN if unknown.
 * @param gimbal_device_id  This field is to be used if the gimbal manager and the gimbal device are the same component and hence have the same component ID. This field is then set a number between 1-6. If the component ID is separate, this field is not required and must be set to 0.
 */
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS

static inline void mavlink_msg_gimbal_device_attitude_status_send(mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint32_t time_boot_ms, uint16_t flags, const float *q, float angular_velocity_x, float angular_velocity_y, float angular_velocity_z, uint32_t failure_flags, float delta_yaw, float delta_yaw_velocity, uint8_t gimbal_device_id)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_float(buf, 20, angular_velocity_x);
    _mav_put_float(buf, 24, angular_velocity_y);
    _mav_put_float(buf, 28, angular_velocity_z);
    _mav_put_uint32_t(buf, 32, failure_flags);
    _mav_put_uint16_t(buf, 36, flags);
    _mav_put_uint8_t(buf, 38, target_system);
    _mav_put_uint8_t(buf, 39, target_component);
    _mav_put_float(buf, 40, delta_yaw);
    _mav_put_float(buf, 44, delta_yaw_velocity);
    _mav_put_uint8_t(buf, 48, gimbal_device_id);
    _mav_put_float_array(buf, 4, q, 4);
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS, buf, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC);
#else
    mavlink_gimbal_device_attitude_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.angular_velocity_x = angular_velocity_x;
    packet.angular_velocity_y = angular_velocity_y;
    packet.angular_velocity_z = angular_velocity_z;
    packet.failure_flags = failure_flags;
    packet.flags = flags;
    packet.target_system = target_system;
    packet.target_component = target_component;
    packet.delta_yaw = delta_yaw;
    packet.delta_yaw_velocity = delta_yaw_velocity;
    packet.gimbal_device_id = gimbal_device_id;
    mav_array_memcpy(packet.q, q, sizeof(float)*4);
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS, (const char *)&packet, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC);
#endif
}

/**
 * @brief Send a gimbal_device_attitude_status message
 * @param chan MAVLink channel to send the message
 * @param struct The MAVLink struct to serialize
 */
static inline void mavlink_msg_gimbal_device_attitude_status_send_struct(mavlink_channel_t chan, const mavlink_gimbal_device_attitude_status_t* gimbal_device_attitude_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    mavlink_msg_gimbal_device_attitude_status_send(chan, gimbal_device_attitude_status->target_system, gimbal_device_attitude_status->target_component, gimbal_device_attitude_status->time_boot_ms, gimbal_device_attitude_status->flags, gimbal_device_attitude_status->q, gimbal_device_attitude_status->angular_velocity_x, gimbal_device_attitude_status->angular_velocity_y, gimbal_device_attitude_status->angular_velocity_z, gimbal_device_attitude_status->failure_flags, gimbal_device_attitude_status->delta_yaw, gimbal_device_attitude_status->delta_yaw_velocity, gimbal_device_attitude_status->gimbal_device_id);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS, (const char *)gimbal_device_attitude_status, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC);
#endif
}

#if MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN
/*
  This variant of _send() can be used to save stack space by re-using
  memory from the receive buffer.  The caller provides a
  mavlink_message_t which is the size of a full mavlink message. This
  is usually the receive buffer for the channel, and allows a reply to an
  incoming message with minimum stack space usage.
 */
static inline void mavlink_msg_gimbal_device_attitude_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan,  uint8_t target_system, uint8_t target_component, uint32_t time_boot_ms, uint16_t flags, const float *q, float angular_velocity_x, float angular_velocity_y, float angular_velocity_z, uint32_t failure_flags, float delta_yaw, float delta_yaw_velocity, uint8_t gimbal_device_id)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char *buf = (char *)msgbuf;
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_float(buf, 20, angular_velocity_x);
    _mav_put_float(buf, 24, angular_velocity_y);
    _mav_put_float(buf, 28, angular_velocity_z);
    _mav_put_uint32_t(buf, 32, failure_flags);
    _mav_put_uint16_t(buf, 36, flags);
    _mav_put_uint8_t(buf, 38, target_system);
    _mav_put_uint8_t(buf, 39, target_component);
    _mav_put_float(buf, 40, delta_yaw);
    _mav_put_float(buf, 44, delta_yaw_velocity);
    _mav_put_uint8_t(buf, 48, gimbal_device_id);
    _mav_put_float_array(buf, 4, q, 4);
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS, buf, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC);
#else
    mavlink_gimbal_device_attitude_status_t *packet = (mavlink_gimbal_device_attitude_status_t *)msgbuf;
    packet->time_boot_ms = time_boot_ms;
    packet->angular_velocity_x = angular_velocity_x;
    packet->angular_velocity_y = angular_velocity_y;
    packet->angular_velocity_z = angular_velocity_z;
    packet->failure_flags = failure_flags;
    packet->flags = flags;
    packet->target_system = target_system;
    packet->target_component = target_component;
    packet->delta_yaw = delta_yaw;
    packet->delta_yaw_velocity = delta_yaw_velocity;
    packet->gimbal_device_id = gimbal_device_id;
    mav_array_memcpy(packet->q, q, sizeof(float)*4);
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS, (const char *)packet, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_MIN_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_CRC);
#endif
}
#endif

#endif

// MESSAGE GIMBAL_DEVICE_ATTITUDE_STATUS UNPACKING


/**
 * @brief Get field target_system from gimbal_device_attitude_status message
 *
 * @return  System ID
 */
static inline uint8_t mavlink_msg_gimbal_device_attitude_status_get_target_system(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  38);
}

/**
 * @brief Get field target_component from gimbal_device_attitude_status message
 *
 * @return  Component ID
 */
static inline uint8_t mavlink_msg_gimbal_device_attitude_status_get_target_component(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  39);
}

/**
 * @brief Get field time_boot_ms from gimbal_device_attitude_status message
 *
 * @return [ms] Timestamp (time since system boot).
 */
static inline uint32_t mavlink_msg_gimbal_device_attitude_status_get_time_boot_ms(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint32_t(msg,  0);
}

/**
 * @brief Get field flags from gimbal_device_attitude_status message
 *
 * @return  Current gimbal flags set.
 */
static inline uint16_t mavlink_msg_gimbal_device_attitude_status_get_flags(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint16_t(msg,  36);
}

/**
 * @brief Get field q from gimbal_device_attitude_status message
 *
 * @return  Quaternion components, w, x, y, z (1 0 0 0 is the null-rotation). The frame is described in the message description.
 */
static inline uint16_t mavlink_msg_gimbal_device_attitude_status_get_q(const mavlink_message_t* msg, float *q)
{
    return _MAV_RETURN_float_array(msg, q, 4,  4);
}

/**
 * @brief Get field angular_velocity_x from gimbal_device_attitude_status message
 *
 * @return [rad/s] X component of angular velocity (positive: rolling to the right). The frame is described in the message description. NaN if unknown.
 */
static inline float mavlink_msg_gimbal_device_attitude_status_get_angular_velocity_x(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  20);
}

/**
 * @brief Get field angular_velocity_y from gimbal_device_attitude_status message
 *
 * @return [rad/s] Y component of angular velocity (positive: pitching up). The frame is described in the message description. NaN if unknown.
 */
static inline float mavlink_msg_gimbal_device_attitude_status_get_angular_velocity_y(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  24);
}

/**
 * @brief Get field angular_velocity_z from gimbal_device_attitude_status message
 *
 * @return [rad/s] Z component of angular velocity (positive: yawing to the right). The frame is described in the message description. NaN if unknown.
 */
static inline float mavlink_msg_gimbal_device_attitude_status_get_angular_velocity_z(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  28);
}

/**
 * @brief Get field failure_flags from gimbal_device_attitude_status message
 *
 * @return  Failure flags (0 for no failure)
 */
static inline uint32_t mavlink_msg_gimbal_device_attitude_status_get_failure_flags(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint32_t(msg,  32);
}

/**
 * @brief Get field delta_yaw from gimbal_device_attitude_status message
 *
 * @return [rad] Yaw angle relating the quaternions in earth and body frames (see message description). NaN if unknown.
 */
static inline float mavlink_msg_gimbal_device_attitude_status_get_delta_yaw(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  40);
}

/**
 * @brief Get field delta_yaw_velocity from gimbal_device_attitude_status message
 *
 * @return [rad/s] Yaw angular velocity relating the angular velocities in earth and body frames (see message description). NaN if unknown.
 */
static inline float mavlink_msg_gimbal_device_attitude_status_get_delta_yaw_velocity(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  44);
}

/**
 * @brief Get field gimbal_device_id from gimbal_device_attitude_status message
 *
 * @return  This field is to be used if the gimbal manager and the gimbal device are the same component and hence have the same component ID. This field is then set a number between 1-6. If the component ID is separate, this field is not required and must be set to 0.
 */
static inline uint8_t mavlink_msg_gimbal_device_attitude_status_get_gimbal_device_id(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  48);
}

/**
 * @brief Decode a gimbal_device_attitude_status message into a struct
 *
 * @param msg The message to decode
 * @param gimbal_device_attitude_status C-struct to decode the message contents into
 */
static inline void mavlink_msg_gimbal_device_attitude_status_decode(const mavlink_message_t* msg, mavlink_gimbal_device_attitude_status_t* gimbal_device_attitude_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    gimbal_device_attitude_status->time_boot_ms = mavlink_msg_gimbal_device_attitude_status_get_time_boot_ms(msg);
    mavlink_msg_gimbal_device_attitude_status_get_q(msg, gimbal_device_attitude_status->q);
    gimbal_device_attitude_status->angular_velocity_x = mavlink_msg_gimbal_device_attitude_status_get_angular_velocity_x(msg);
    gimbal_device_attitude_status->angular_velocity_y = mavlink_msg_gimbal_device_attitude_status_get_angular_velocity_y(msg);
    gimbal_device_attitude_status->angular_velocity_z = mavlink_msg_gimbal_device_attitude_status_get_angular_velocity_z(msg);
    gimbal_device_attitude_status->failure_flags = mavlink_msg_gimbal_device_attitude_status_get_failure_flags(msg);
    gimbal_device_attitude_status->flags = mavlink_msg_gimbal_device_attitude_status_get_flags(msg);
    gimbal_device_attitude_status->target_system = mavlink_msg_gimbal_device_attitude_status_get_target_system(msg);
    gimbal_device_attitude_status->target_component = mavlink_msg_gimbal_device_attitude_status_get_target_component(msg);
    gimbal_device_attitude_status->delta_yaw = mavlink_msg_gimbal_device_attitude_status_get_delta_yaw(msg);
    gimbal_device_attitude_status->delta_yaw_velocity = mavlink_msg_gimbal_device_attitude_status_get_delta_yaw_velocity(msg);
    gimbal_device_attitude_status->gimbal_device_id = mavlink_msg_gimbal_device_attitude_status_get_gimbal_device_id(msg);
#else
        uint8_t len = msg->len < MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN? msg->len : MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN;
        memset(gimbal_device_attitude_status, 0, MAVLINK_MSG_ID_GIMBAL_DEVICE_ATTITUDE_STATUS_LEN);
    memcpy(gimbal_device_attitude_status, _MAV_PAYLOAD(msg), len);
#endif
}