VK_Mavlink/v2.0/VKFly/mavlink_msg_vkfmu_status.h

#pragma once
// MESSAGE VKFMU_STATUS PACKING

#define MAVLINK_MSG_ID_VKFMU_STATUS 53001


typedef struct __mavlink_vkfmu_status_t {
 uint32_t time_boot_ms; /*< [ms] Timestamp in ms from system boot.*/
 uint32_t flight_time; /*< [s] flight time in seconds*/
 uint32_t dist_to_tar; /*< [cm] distance to target position in cm*/
 float flight_dist; /*< [m] flight distance since this power up*/
 uint16_t ups_volt; /*<  ups voltage in 0.1V*/
 uint16_t adc_volt; /*<  adc voltage in 0.1V*/
 uint16_t servo_state; /*<  bitmap for servo state*/
 uint8_t rtl_reason; /*<  return to launch reason.*/
 uint8_t loiter_reason; /*<  Loiter reason */
 uint8_t s_flag3; /*<  fmu sflag3*/
} mavlink_vkfmu_status_t;

#define MAVLINK_MSG_ID_VKFMU_STATUS_LEN 25
#define MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN 25
#define MAVLINK_MSG_ID_53001_LEN 25
#define MAVLINK_MSG_ID_53001_MIN_LEN 25

#define MAVLINK_MSG_ID_VKFMU_STATUS_CRC 136
#define MAVLINK_MSG_ID_53001_CRC 136



#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_VKFMU_STATUS { \
    53001, \
    "VKFMU_STATUS", \
    10, \
    {  { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vkfmu_status_t, time_boot_ms) }, \
         { "rtl_reason", NULL, MAVLINK_TYPE_UINT8_T, 0, 22, offsetof(mavlink_vkfmu_status_t, rtl_reason) }, \
         { "loiter_reason", NULL, MAVLINK_TYPE_UINT8_T, 0, 23, offsetof(mavlink_vkfmu_status_t, loiter_reason) }, \
         { "s_flag3", NULL, MAVLINK_TYPE_UINT8_T, 0, 24, offsetof(mavlink_vkfmu_status_t, s_flag3) }, \
         { "ups_volt", NULL, MAVLINK_TYPE_UINT16_T, 0, 16, offsetof(mavlink_vkfmu_status_t, ups_volt) }, \
         { "adc_volt", NULL, MAVLINK_TYPE_UINT16_T, 0, 18, offsetof(mavlink_vkfmu_status_t, adc_volt) }, \
         { "flight_time", NULL, MAVLINK_TYPE_UINT32_T, 0, 4, offsetof(mavlink_vkfmu_status_t, flight_time) }, \
         { "dist_to_tar", NULL, MAVLINK_TYPE_UINT32_T, 0, 8, offsetof(mavlink_vkfmu_status_t, dist_to_tar) }, \
         { "servo_state", NULL, MAVLINK_TYPE_UINT16_T, 0, 20, offsetof(mavlink_vkfmu_status_t, servo_state) }, \
         { "flight_dist", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_vkfmu_status_t, flight_dist) }, \
         } \
}
#else
#define MAVLINK_MESSAGE_INFO_VKFMU_STATUS { \
    "VKFMU_STATUS", \
    10, \
    {  { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vkfmu_status_t, time_boot_ms) }, \
         { "rtl_reason", NULL, MAVLINK_TYPE_UINT8_T, 0, 22, offsetof(mavlink_vkfmu_status_t, rtl_reason) }, \
         { "loiter_reason", NULL, MAVLINK_TYPE_UINT8_T, 0, 23, offsetof(mavlink_vkfmu_status_t, loiter_reason) }, \
         { "s_flag3", NULL, MAVLINK_TYPE_UINT8_T, 0, 24, offsetof(mavlink_vkfmu_status_t, s_flag3) }, \
         { "ups_volt", NULL, MAVLINK_TYPE_UINT16_T, 0, 16, offsetof(mavlink_vkfmu_status_t, ups_volt) }, \
         { "adc_volt", NULL, MAVLINK_TYPE_UINT16_T, 0, 18, offsetof(mavlink_vkfmu_status_t, adc_volt) }, \
         { "flight_time", NULL, MAVLINK_TYPE_UINT32_T, 0, 4, offsetof(mavlink_vkfmu_status_t, flight_time) }, \
         { "dist_to_tar", NULL, MAVLINK_TYPE_UINT32_T, 0, 8, offsetof(mavlink_vkfmu_status_t, dist_to_tar) }, \
         { "servo_state", NULL, MAVLINK_TYPE_UINT16_T, 0, 20, offsetof(mavlink_vkfmu_status_t, servo_state) }, \
         { "flight_dist", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_vkfmu_status_t, flight_dist) }, \
         } \
}
#endif

/**
 * @brief Pack a vkfmu_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 time_boot_ms [ms] Timestamp in ms from system boot.
 * @param rtl_reason  return to launch reason.
 * @param loiter_reason  Loiter reason 
 * @param s_flag3  fmu sflag3
 * @param ups_volt  ups voltage in 0.1V
 * @param adc_volt  adc voltage in 0.1V
 * @param flight_time [s] flight time in seconds
 * @param dist_to_tar [cm] distance to target position in cm
 * @param servo_state  bitmap for servo state
 * @param flight_dist [m] flight distance since this power up
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vkfmu_status_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
                               uint32_t time_boot_ms, uint8_t rtl_reason, uint8_t loiter_reason, uint8_t s_flag3, uint16_t ups_volt, uint16_t adc_volt, uint32_t flight_time, uint32_t dist_to_tar, uint16_t servo_state, float flight_dist)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKFMU_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_uint32_t(buf, 4, flight_time);
    _mav_put_uint32_t(buf, 8, dist_to_tar);
    _mav_put_float(buf, 12, flight_dist);
    _mav_put_uint16_t(buf, 16, ups_volt);
    _mav_put_uint16_t(buf, 18, adc_volt);
    _mav_put_uint16_t(buf, 20, servo_state);
    _mav_put_uint8_t(buf, 22, rtl_reason);
    _mav_put_uint8_t(buf, 23, loiter_reason);
    _mav_put_uint8_t(buf, 24, s_flag3);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VKFMU_STATUS_LEN);
#else
    mavlink_vkfmu_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.flight_time = flight_time;
    packet.dist_to_tar = dist_to_tar;
    packet.flight_dist = flight_dist;
    packet.ups_volt = ups_volt;
    packet.adc_volt = adc_volt;
    packet.servo_state = servo_state;
    packet.rtl_reason = rtl_reason;
    packet.loiter_reason = loiter_reason;
    packet.s_flag3 = s_flag3;

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

    msg->msgid = MAVLINK_MSG_ID_VKFMU_STATUS;
    return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_CRC);
}

/**
 * @brief Pack a vkfmu_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 time_boot_ms [ms] Timestamp in ms from system boot.
 * @param rtl_reason  return to launch reason.
 * @param loiter_reason  Loiter reason 
 * @param s_flag3  fmu sflag3
 * @param ups_volt  ups voltage in 0.1V
 * @param adc_volt  adc voltage in 0.1V
 * @param flight_time [s] flight time in seconds
 * @param dist_to_tar [cm] distance to target position in cm
 * @param servo_state  bitmap for servo state
 * @param flight_dist [m] flight distance since this power up
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vkfmu_status_pack_status(uint8_t system_id, uint8_t component_id, mavlink_status_t *_status, mavlink_message_t* msg,
                               uint32_t time_boot_ms, uint8_t rtl_reason, uint8_t loiter_reason, uint8_t s_flag3, uint16_t ups_volt, uint16_t adc_volt, uint32_t flight_time, uint32_t dist_to_tar, uint16_t servo_state, float flight_dist)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKFMU_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_uint32_t(buf, 4, flight_time);
    _mav_put_uint32_t(buf, 8, dist_to_tar);
    _mav_put_float(buf, 12, flight_dist);
    _mav_put_uint16_t(buf, 16, ups_volt);
    _mav_put_uint16_t(buf, 18, adc_volt);
    _mav_put_uint16_t(buf, 20, servo_state);
    _mav_put_uint8_t(buf, 22, rtl_reason);
    _mav_put_uint8_t(buf, 23, loiter_reason);
    _mav_put_uint8_t(buf, 24, s_flag3);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VKFMU_STATUS_LEN);
#else
    mavlink_vkfmu_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.flight_time = flight_time;
    packet.dist_to_tar = dist_to_tar;
    packet.flight_dist = flight_dist;
    packet.ups_volt = ups_volt;
    packet.adc_volt = adc_volt;
    packet.servo_state = servo_state;
    packet.rtl_reason = rtl_reason;
    packet.loiter_reason = loiter_reason;
    packet.s_flag3 = s_flag3;

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

    msg->msgid = MAVLINK_MSG_ID_VKFMU_STATUS;
#if MAVLINK_CRC_EXTRA
    return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_CRC);
#else
    return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN);
#endif
}

/**
 * @brief Pack a vkfmu_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 time_boot_ms [ms] Timestamp in ms from system boot.
 * @param rtl_reason  return to launch reason.
 * @param loiter_reason  Loiter reason 
 * @param s_flag3  fmu sflag3
 * @param ups_volt  ups voltage in 0.1V
 * @param adc_volt  adc voltage in 0.1V
 * @param flight_time [s] flight time in seconds
 * @param dist_to_tar [cm] distance to target position in cm
 * @param servo_state  bitmap for servo state
 * @param flight_dist [m] flight distance since this power up
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vkfmu_status_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
                               mavlink_message_t* msg,
                                   uint32_t time_boot_ms,uint8_t rtl_reason,uint8_t loiter_reason,uint8_t s_flag3,uint16_t ups_volt,uint16_t adc_volt,uint32_t flight_time,uint32_t dist_to_tar,uint16_t servo_state,float flight_dist)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKFMU_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_uint32_t(buf, 4, flight_time);
    _mav_put_uint32_t(buf, 8, dist_to_tar);
    _mav_put_float(buf, 12, flight_dist);
    _mav_put_uint16_t(buf, 16, ups_volt);
    _mav_put_uint16_t(buf, 18, adc_volt);
    _mav_put_uint16_t(buf, 20, servo_state);
    _mav_put_uint8_t(buf, 22, rtl_reason);
    _mav_put_uint8_t(buf, 23, loiter_reason);
    _mav_put_uint8_t(buf, 24, s_flag3);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VKFMU_STATUS_LEN);
#else
    mavlink_vkfmu_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.flight_time = flight_time;
    packet.dist_to_tar = dist_to_tar;
    packet.flight_dist = flight_dist;
    packet.ups_volt = ups_volt;
    packet.adc_volt = adc_volt;
    packet.servo_state = servo_state;
    packet.rtl_reason = rtl_reason;
    packet.loiter_reason = loiter_reason;
    packet.s_flag3 = s_flag3;

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

    msg->msgid = MAVLINK_MSG_ID_VKFMU_STATUS;
    return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_CRC);
}

/**
 * @brief Encode a vkfmu_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 vkfmu_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vkfmu_status_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_vkfmu_status_t* vkfmu_status)
{
    return mavlink_msg_vkfmu_status_pack(system_id, component_id, msg, vkfmu_status->time_boot_ms, vkfmu_status->rtl_reason, vkfmu_status->loiter_reason, vkfmu_status->s_flag3, vkfmu_status->ups_volt, vkfmu_status->adc_volt, vkfmu_status->flight_time, vkfmu_status->dist_to_tar, vkfmu_status->servo_state, vkfmu_status->flight_dist);
}

/**
 * @brief Encode a vkfmu_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 vkfmu_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vkfmu_status_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_vkfmu_status_t* vkfmu_status)
{
    return mavlink_msg_vkfmu_status_pack_chan(system_id, component_id, chan, msg, vkfmu_status->time_boot_ms, vkfmu_status->rtl_reason, vkfmu_status->loiter_reason, vkfmu_status->s_flag3, vkfmu_status->ups_volt, vkfmu_status->adc_volt, vkfmu_status->flight_time, vkfmu_status->dist_to_tar, vkfmu_status->servo_state, vkfmu_status->flight_dist);
}

/**
 * @brief Encode a vkfmu_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 vkfmu_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vkfmu_status_encode_status(uint8_t system_id, uint8_t component_id, mavlink_status_t* _status, mavlink_message_t* msg, const mavlink_vkfmu_status_t* vkfmu_status)
{
    return mavlink_msg_vkfmu_status_pack_status(system_id, component_id, _status, msg,  vkfmu_status->time_boot_ms, vkfmu_status->rtl_reason, vkfmu_status->loiter_reason, vkfmu_status->s_flag3, vkfmu_status->ups_volt, vkfmu_status->adc_volt, vkfmu_status->flight_time, vkfmu_status->dist_to_tar, vkfmu_status->servo_state, vkfmu_status->flight_dist);
}

/**
 * @brief Send a vkfmu_status message
 * @param chan MAVLink channel to send the message
 *
 * @param time_boot_ms [ms] Timestamp in ms from system boot.
 * @param rtl_reason  return to launch reason.
 * @param loiter_reason  Loiter reason 
 * @param s_flag3  fmu sflag3
 * @param ups_volt  ups voltage in 0.1V
 * @param adc_volt  adc voltage in 0.1V
 * @param flight_time [s] flight time in seconds
 * @param dist_to_tar [cm] distance to target position in cm
 * @param servo_state  bitmap for servo state
 * @param flight_dist [m] flight distance since this power up
 */
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS

static inline void mavlink_msg_vkfmu_status_send(mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t rtl_reason, uint8_t loiter_reason, uint8_t s_flag3, uint16_t ups_volt, uint16_t adc_volt, uint32_t flight_time, uint32_t dist_to_tar, uint16_t servo_state, float flight_dist)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKFMU_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_uint32_t(buf, 4, flight_time);
    _mav_put_uint32_t(buf, 8, dist_to_tar);
    _mav_put_float(buf, 12, flight_dist);
    _mav_put_uint16_t(buf, 16, ups_volt);
    _mav_put_uint16_t(buf, 18, adc_volt);
    _mav_put_uint16_t(buf, 20, servo_state);
    _mav_put_uint8_t(buf, 22, rtl_reason);
    _mav_put_uint8_t(buf, 23, loiter_reason);
    _mav_put_uint8_t(buf, 24, s_flag3);

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFMU_STATUS, buf, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_CRC);
#else
    mavlink_vkfmu_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.flight_time = flight_time;
    packet.dist_to_tar = dist_to_tar;
    packet.flight_dist = flight_dist;
    packet.ups_volt = ups_volt;
    packet.adc_volt = adc_volt;
    packet.servo_state = servo_state;
    packet.rtl_reason = rtl_reason;
    packet.loiter_reason = loiter_reason;
    packet.s_flag3 = s_flag3;

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFMU_STATUS, (const char *)&packet, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_CRC);
#endif
}

/**
 * @brief Send a vkfmu_status message
 * @param chan MAVLink channel to send the message
 * @param struct The MAVLink struct to serialize
 */
static inline void mavlink_msg_vkfmu_status_send_struct(mavlink_channel_t chan, const mavlink_vkfmu_status_t* vkfmu_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    mavlink_msg_vkfmu_status_send(chan, vkfmu_status->time_boot_ms, vkfmu_status->rtl_reason, vkfmu_status->loiter_reason, vkfmu_status->s_flag3, vkfmu_status->ups_volt, vkfmu_status->adc_volt, vkfmu_status->flight_time, vkfmu_status->dist_to_tar, vkfmu_status->servo_state, vkfmu_status->flight_dist);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFMU_STATUS, (const char *)vkfmu_status, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_CRC);
#endif
}

#if MAVLINK_MSG_ID_VKFMU_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_vkfmu_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan,  uint32_t time_boot_ms, uint8_t rtl_reason, uint8_t loiter_reason, uint8_t s_flag3, uint16_t ups_volt, uint16_t adc_volt, uint32_t flight_time, uint32_t dist_to_tar, uint16_t servo_state, float flight_dist)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char *buf = (char *)msgbuf;
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_uint32_t(buf, 4, flight_time);
    _mav_put_uint32_t(buf, 8, dist_to_tar);
    _mav_put_float(buf, 12, flight_dist);
    _mav_put_uint16_t(buf, 16, ups_volt);
    _mav_put_uint16_t(buf, 18, adc_volt);
    _mav_put_uint16_t(buf, 20, servo_state);
    _mav_put_uint8_t(buf, 22, rtl_reason);
    _mav_put_uint8_t(buf, 23, loiter_reason);
    _mav_put_uint8_t(buf, 24, s_flag3);

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFMU_STATUS, buf, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_CRC);
#else
    mavlink_vkfmu_status_t *packet = (mavlink_vkfmu_status_t *)msgbuf;
    packet->time_boot_ms = time_boot_ms;
    packet->flight_time = flight_time;
    packet->dist_to_tar = dist_to_tar;
    packet->flight_dist = flight_dist;
    packet->ups_volt = ups_volt;
    packet->adc_volt = adc_volt;
    packet->servo_state = servo_state;
    packet->rtl_reason = rtl_reason;
    packet->loiter_reason = loiter_reason;
    packet->s_flag3 = s_flag3;

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFMU_STATUS, (const char *)packet, MAVLINK_MSG_ID_VKFMU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_LEN, MAVLINK_MSG_ID_VKFMU_STATUS_CRC);
#endif
}
#endif

#endif

// MESSAGE VKFMU_STATUS UNPACKING


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

/**
 * @brief Get field rtl_reason from vkfmu_status message
 *
 * @return  return to launch reason.
 */
static inline uint8_t mavlink_msg_vkfmu_status_get_rtl_reason(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  22);
}

/**
 * @brief Get field loiter_reason from vkfmu_status message
 *
 * @return  Loiter reason 
 */
static inline uint8_t mavlink_msg_vkfmu_status_get_loiter_reason(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  23);
}

/**
 * @brief Get field s_flag3 from vkfmu_status message
 *
 * @return  fmu sflag3
 */
static inline uint8_t mavlink_msg_vkfmu_status_get_s_flag3(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  24);
}

/**
 * @brief Get field ups_volt from vkfmu_status message
 *
 * @return  ups voltage in 0.1V
 */
static inline uint16_t mavlink_msg_vkfmu_status_get_ups_volt(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint16_t(msg,  16);
}

/**
 * @brief Get field adc_volt from vkfmu_status message
 *
 * @return  adc voltage in 0.1V
 */
static inline uint16_t mavlink_msg_vkfmu_status_get_adc_volt(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint16_t(msg,  18);
}

/**
 * @brief Get field flight_time from vkfmu_status message
 *
 * @return [s] flight time in seconds
 */
static inline uint32_t mavlink_msg_vkfmu_status_get_flight_time(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint32_t(msg,  4);
}

/**
 * @brief Get field dist_to_tar from vkfmu_status message
 *
 * @return [cm] distance to target position in cm
 */
static inline uint32_t mavlink_msg_vkfmu_status_get_dist_to_tar(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint32_t(msg,  8);
}

/**
 * @brief Get field servo_state from vkfmu_status message
 *
 * @return  bitmap for servo state
 */
static inline uint16_t mavlink_msg_vkfmu_status_get_servo_state(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint16_t(msg,  20);
}

/**
 * @brief Get field flight_dist from vkfmu_status message
 *
 * @return [m] flight distance since this power up
 */
static inline float mavlink_msg_vkfmu_status_get_flight_dist(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  12);
}

/**
 * @brief Decode a vkfmu_status message into a struct
 *
 * @param msg The message to decode
 * @param vkfmu_status C-struct to decode the message contents into
 */
static inline void mavlink_msg_vkfmu_status_decode(const mavlink_message_t* msg, mavlink_vkfmu_status_t* vkfmu_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    vkfmu_status->time_boot_ms = mavlink_msg_vkfmu_status_get_time_boot_ms(msg);
    vkfmu_status->flight_time = mavlink_msg_vkfmu_status_get_flight_time(msg);
    vkfmu_status->dist_to_tar = mavlink_msg_vkfmu_status_get_dist_to_tar(msg);
    vkfmu_status->flight_dist = mavlink_msg_vkfmu_status_get_flight_dist(msg);
    vkfmu_status->ups_volt = mavlink_msg_vkfmu_status_get_ups_volt(msg);
    vkfmu_status->adc_volt = mavlink_msg_vkfmu_status_get_adc_volt(msg);
    vkfmu_status->servo_state = mavlink_msg_vkfmu_status_get_servo_state(msg);
    vkfmu_status->rtl_reason = mavlink_msg_vkfmu_status_get_rtl_reason(msg);
    vkfmu_status->loiter_reason = mavlink_msg_vkfmu_status_get_loiter_reason(msg);
    vkfmu_status->s_flag3 = mavlink_msg_vkfmu_status_get_s_flag3(msg);
#else
        uint8_t len = msg->len < MAVLINK_MSG_ID_VKFMU_STATUS_LEN? msg->len : MAVLINK_MSG_ID_VKFMU_STATUS_LEN;
        memset(vkfmu_status, 0, MAVLINK_MSG_ID_VKFMU_STATUS_LEN);
    memcpy(vkfmu_status, _MAV_PAYLOAD(msg), len);
#endif
}