VK_Mavlink/v2.0/VKFly/mavlink_msg_vk_fixedwing_control_value.h

#pragma once
// MESSAGE VK_FIXEDWING_CONTROL_VALUE PACKING

#define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE 53009


typedef struct __mavlink_vk_fixedwing_control_value_t {
 uint32_t timestamp; /*< [ms] Timestamp from system boot.*/
 float roll_value; /*<  Roll control value,
        negative value means roll left.*/
 float pitch_value; /*<  Pitch control value,
        negative value means pitch down.*/
 float throttle_value; /*<  Throttle control
        value, negative value means throttle off*/
 float yaw_value; /*<  Throttle control
        value, negative value means turn left*/
} mavlink_vk_fixedwing_control_value_t;

#define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN 20
#define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN 20
#define MAVLINK_MSG_ID_53009_LEN 20
#define MAVLINK_MSG_ID_53009_MIN_LEN 20

#define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC 226
#define MAVLINK_MSG_ID_53009_CRC 226



#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_VK_FIXEDWING_CONTROL_VALUE { \
    53009, \
    "VK_FIXEDWING_CONTROL_VALUE", \
    5, \
    {  { "timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vk_fixedwing_control_value_t, timestamp) }, \
         { "roll_value", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_vk_fixedwing_control_value_t, roll_value) }, \
         { "pitch_value", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_vk_fixedwing_control_value_t, pitch_value) }, \
         { "throttle_value", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_vk_fixedwing_control_value_t, throttle_value) }, \
         { "yaw_value", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_vk_fixedwing_control_value_t, yaw_value) }, \
         } \
}
#else
#define MAVLINK_MESSAGE_INFO_VK_FIXEDWING_CONTROL_VALUE { \
    "VK_FIXEDWING_CONTROL_VALUE", \
    5, \
    {  { "timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vk_fixedwing_control_value_t, timestamp) }, \
         { "roll_value", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_vk_fixedwing_control_value_t, roll_value) }, \
         { "pitch_value", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_vk_fixedwing_control_value_t, pitch_value) }, \
         { "throttle_value", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_vk_fixedwing_control_value_t, throttle_value) }, \
         { "yaw_value", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_vk_fixedwing_control_value_t, yaw_value) }, \
         } \
}
#endif

/**
 * @brief Pack a vk_fixedwing_control_value 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 timestamp [ms] Timestamp from system boot.
 * @param roll_value  Roll control value,
        negative value means roll left.
 * @param pitch_value  Pitch control value,
        negative value means pitch down.
 * @param throttle_value  Throttle control
        value, negative value means throttle off
 * @param yaw_value  Throttle control
        value, negative value means turn left
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vk_fixedwing_control_value_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
                               uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN];
    _mav_put_uint32_t(buf, 0, timestamp);
    _mav_put_float(buf, 4, roll_value);
    _mav_put_float(buf, 8, pitch_value);
    _mav_put_float(buf, 12, throttle_value);
    _mav_put_float(buf, 16, yaw_value);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
#else
    mavlink_vk_fixedwing_control_value_t packet;
    packet.timestamp = timestamp;
    packet.roll_value = roll_value;
    packet.pitch_value = pitch_value;
    packet.throttle_value = throttle_value;
    packet.yaw_value = yaw_value;

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
#endif

    msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE;
    return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
}

/**
 * @brief Pack a vk_fixedwing_control_value 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 timestamp [ms] Timestamp from system boot.
 * @param roll_value  Roll control value,
        negative value means roll left.
 * @param pitch_value  Pitch control value,
        negative value means pitch down.
 * @param throttle_value  Throttle control
        value, negative value means throttle off
 * @param yaw_value  Throttle control
        value, negative value means turn left
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vk_fixedwing_control_value_pack_status(uint8_t system_id, uint8_t component_id, mavlink_status_t *_status, mavlink_message_t* msg,
                               uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN];
    _mav_put_uint32_t(buf, 0, timestamp);
    _mav_put_float(buf, 4, roll_value);
    _mav_put_float(buf, 8, pitch_value);
    _mav_put_float(buf, 12, throttle_value);
    _mav_put_float(buf, 16, yaw_value);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
#else
    mavlink_vk_fixedwing_control_value_t packet;
    packet.timestamp = timestamp;
    packet.roll_value = roll_value;
    packet.pitch_value = pitch_value;
    packet.throttle_value = throttle_value;
    packet.yaw_value = yaw_value;

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
#endif

    msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE;
#if MAVLINK_CRC_EXTRA
    return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
#else
    return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
#endif
}

/**
 * @brief Pack a vk_fixedwing_control_value 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 timestamp [ms] Timestamp from system boot.
 * @param roll_value  Roll control value,
        negative value means roll left.
 * @param pitch_value  Pitch control value,
        negative value means pitch down.
 * @param throttle_value  Throttle control
        value, negative value means throttle off
 * @param yaw_value  Throttle control
        value, negative value means turn left
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vk_fixedwing_control_value_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
                               mavlink_message_t* msg,
                                   uint32_t timestamp,float roll_value,float pitch_value,float throttle_value,float yaw_value)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN];
    _mav_put_uint32_t(buf, 0, timestamp);
    _mav_put_float(buf, 4, roll_value);
    _mav_put_float(buf, 8, pitch_value);
    _mav_put_float(buf, 12, throttle_value);
    _mav_put_float(buf, 16, yaw_value);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
#else
    mavlink_vk_fixedwing_control_value_t packet;
    packet.timestamp = timestamp;
    packet.roll_value = roll_value;
    packet.pitch_value = pitch_value;
    packet.throttle_value = throttle_value;
    packet.yaw_value = yaw_value;

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
#endif

    msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE;
    return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
}

/**
 * @brief Encode a vk_fixedwing_control_value 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 vk_fixedwing_control_value C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
{
    return mavlink_msg_vk_fixedwing_control_value_pack(system_id, component_id, msg, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value);
}

/**
 * @brief Encode a vk_fixedwing_control_value 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 vk_fixedwing_control_value C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
{
    return mavlink_msg_vk_fixedwing_control_value_pack_chan(system_id, component_id, chan, msg, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value);
}

/**
 * @brief Encode a vk_fixedwing_control_value 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 vk_fixedwing_control_value C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode_status(uint8_t system_id, uint8_t component_id, mavlink_status_t* _status, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
{
    return mavlink_msg_vk_fixedwing_control_value_pack_status(system_id, component_id, _status, msg,  vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value);
}

/**
 * @brief Send a vk_fixedwing_control_value message
 * @param chan MAVLink channel to send the message
 *
 * @param timestamp [ms] Timestamp from system boot.
 * @param roll_value  Roll control value,
        negative value means roll left.
 * @param pitch_value  Pitch control value,
        negative value means pitch down.
 * @param throttle_value  Throttle control
        value, negative value means throttle off
 * @param yaw_value  Throttle control
        value, negative value means turn left
 */
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS

static inline void mavlink_msg_vk_fixedwing_control_value_send(mavlink_channel_t chan, uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN];
    _mav_put_uint32_t(buf, 0, timestamp);
    _mav_put_float(buf, 4, roll_value);
    _mav_put_float(buf, 8, pitch_value);
    _mav_put_float(buf, 12, throttle_value);
    _mav_put_float(buf, 16, yaw_value);

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
#else
    mavlink_vk_fixedwing_control_value_t packet;
    packet.timestamp = timestamp;
    packet.roll_value = roll_value;
    packet.pitch_value = pitch_value;
    packet.throttle_value = throttle_value;
    packet.yaw_value = yaw_value;

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)&packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
#endif
}

/**
 * @brief Send a vk_fixedwing_control_value message
 * @param chan MAVLink channel to send the message
 * @param struct The MAVLink struct to serialize
 */
static inline void mavlink_msg_vk_fixedwing_control_value_send_struct(mavlink_channel_t chan, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    mavlink_msg_vk_fixedwing_control_value_send(chan, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)vk_fixedwing_control_value, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
#endif
}

#if MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_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_vk_fixedwing_control_value_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan,  uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char *buf = (char *)msgbuf;
    _mav_put_uint32_t(buf, 0, timestamp);
    _mav_put_float(buf, 4, roll_value);
    _mav_put_float(buf, 8, pitch_value);
    _mav_put_float(buf, 12, throttle_value);
    _mav_put_float(buf, 16, yaw_value);

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
#else
    mavlink_vk_fixedwing_control_value_t *packet = (mavlink_vk_fixedwing_control_value_t *)msgbuf;
    packet->timestamp = timestamp;
    packet->roll_value = roll_value;
    packet->pitch_value = pitch_value;
    packet->throttle_value = throttle_value;
    packet->yaw_value = yaw_value;

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
#endif
}
#endif

#endif

// MESSAGE VK_FIXEDWING_CONTROL_VALUE UNPACKING


/**
 * @brief Get field timestamp from vk_fixedwing_control_value message
 *
 * @return [ms] Timestamp from system boot.
 */
static inline uint32_t mavlink_msg_vk_fixedwing_control_value_get_timestamp(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint32_t(msg,  0);
}

/**
 * @brief Get field roll_value from vk_fixedwing_control_value message
 *
 * @return  Roll control value,
        negative value means roll left.
 */
static inline float mavlink_msg_vk_fixedwing_control_value_get_roll_value(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  4);
}

/**
 * @brief Get field pitch_value from vk_fixedwing_control_value message
 *
 * @return  Pitch control value,
        negative value means pitch down.
 */
static inline float mavlink_msg_vk_fixedwing_control_value_get_pitch_value(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  8);
}

/**
 * @brief Get field throttle_value from vk_fixedwing_control_value message
 *
 * @return  Throttle control
        value, negative value means throttle off
 */
static inline float mavlink_msg_vk_fixedwing_control_value_get_throttle_value(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  12);
}

/**
 * @brief Get field yaw_value from vk_fixedwing_control_value message
 *
 * @return  Throttle control
        value, negative value means turn left
 */
static inline float mavlink_msg_vk_fixedwing_control_value_get_yaw_value(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  16);
}

/**
 * @brief Decode a vk_fixedwing_control_value message into a struct
 *
 * @param msg The message to decode
 * @param vk_fixedwing_control_value C-struct to decode the message contents into
 */
static inline void mavlink_msg_vk_fixedwing_control_value_decode(const mavlink_message_t* msg, mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    vk_fixedwing_control_value->timestamp = mavlink_msg_vk_fixedwing_control_value_get_timestamp(msg);
    vk_fixedwing_control_value->roll_value = mavlink_msg_vk_fixedwing_control_value_get_roll_value(msg);
    vk_fixedwing_control_value->pitch_value = mavlink_msg_vk_fixedwing_control_value_get_pitch_value(msg);
    vk_fixedwing_control_value->throttle_value = mavlink_msg_vk_fixedwing_control_value_get_throttle_value(msg);
    vk_fixedwing_control_value->yaw_value = mavlink_msg_vk_fixedwing_control_value_get_yaw_value(msg);
#else
        uint8_t len = msg->len < MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN? msg->len : MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN;
        memset(vk_fixedwing_control_value, 0, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
    memcpy(vk_fixedwing_control_value, _MAV_PAYLOAD(msg), len);
#endif
}