VK_Mavlink/v2.0/VKFly/mavlink_msg_vkfly_edu_status.h

#pragma once
// MESSAGE VKFLY_EDU_STATUS PACKING

#define MAVLINK_MSG_ID_VKFLY_EDU_STATUS 53025


typedef struct __mavlink_vkfly_edu_status_t {
 uint64_t unix_timestamp; /*< [ms] Unix timestamp in ms, from 1 Jan 1970.*/
 uint32_t boot_timestamp; /*< [ms] Timestamp in ms from system boot.*/
 uint32_t seq; /*<  Sequence number for this package.*/
 uint32_t dev_sn; /*<  Device SN number.*/
 int32_t longitude; /*< [degE7] wgs84 longitude*/
 int32_t latitude; /*< [degE7] wgs84 latitude*/
 float amsl; /*< [m] altitude amsl*/
 float alt_relative; /*< [m] altitude above takeoff*/
 int16_t ve; /*< [cm/s] */
 int16_t vn; /*< [cm/s] */
 int16_t vu; /*< [cm/s] */
 int16_t yaw; /*< [cdeg] */
 int16_t pitch; /*< [cdeg] */
 int16_t roll; /*< [cdeg] */
 int16_t yaw_rate; /*< [cdeg/s] */
 uint8_t dev_type; /*<  0 for flight controller. 1 for elec-stake*/
 uint8_t retry_cnt; /*<  Retry send this message count.*/
 uint8_t fix_type; /*<  0 no fix, 1 single, 2 RTK*/
 uint8_t reserve; /*<  */
 uint8_t flight_mode; /*<  */
} mavlink_vkfly_edu_status_t;

#define MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN 55
#define MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN 55
#define MAVLINK_MSG_ID_53025_LEN 55
#define MAVLINK_MSG_ID_53025_MIN_LEN 55

#define MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC 24
#define MAVLINK_MSG_ID_53025_CRC 24



#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_VKFLY_EDU_STATUS { \
    53025, \
    "VKFLY_EDU_STATUS", \
    20, \
    {  { "unix_timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_vkfly_edu_status_t, unix_timestamp) }, \
         { "boot_timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 8, offsetof(mavlink_vkfly_edu_status_t, boot_timestamp) }, \
         { "seq", NULL, MAVLINK_TYPE_UINT32_T, 0, 12, offsetof(mavlink_vkfly_edu_status_t, seq) }, \
         { "dev_sn", NULL, MAVLINK_TYPE_UINT32_T, 0, 16, offsetof(mavlink_vkfly_edu_status_t, dev_sn) }, \
         { "dev_type", NULL, MAVLINK_TYPE_UINT8_T, 0, 50, offsetof(mavlink_vkfly_edu_status_t, dev_type) }, \
         { "retry_cnt", NULL, MAVLINK_TYPE_UINT8_T, 0, 51, offsetof(mavlink_vkfly_edu_status_t, retry_cnt) }, \
         { "fix_type", NULL, MAVLINK_TYPE_UINT8_T, 0, 52, offsetof(mavlink_vkfly_edu_status_t, fix_type) }, \
         { "reserve", NULL, MAVLINK_TYPE_UINT8_T, 0, 53, offsetof(mavlink_vkfly_edu_status_t, reserve) }, \
         { "longitude", NULL, MAVLINK_TYPE_INT32_T, 0, 20, offsetof(mavlink_vkfly_edu_status_t, longitude) }, \
         { "latitude", NULL, MAVLINK_TYPE_INT32_T, 0, 24, offsetof(mavlink_vkfly_edu_status_t, latitude) }, \
         { "amsl", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_vkfly_edu_status_t, amsl) }, \
         { "alt_relative", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_vkfly_edu_status_t, alt_relative) }, \
         { "ve", NULL, MAVLINK_TYPE_INT16_T, 0, 36, offsetof(mavlink_vkfly_edu_status_t, ve) }, \
         { "vn", NULL, MAVLINK_TYPE_INT16_T, 0, 38, offsetof(mavlink_vkfly_edu_status_t, vn) }, \
         { "vu", NULL, MAVLINK_TYPE_INT16_T, 0, 40, offsetof(mavlink_vkfly_edu_status_t, vu) }, \
         { "yaw", NULL, MAVLINK_TYPE_INT16_T, 0, 42, offsetof(mavlink_vkfly_edu_status_t, yaw) }, \
         { "pitch", NULL, MAVLINK_TYPE_INT16_T, 0, 44, offsetof(mavlink_vkfly_edu_status_t, pitch) }, \
         { "roll", NULL, MAVLINK_TYPE_INT16_T, 0, 46, offsetof(mavlink_vkfly_edu_status_t, roll) }, \
         { "yaw_rate", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_vkfly_edu_status_t, yaw_rate) }, \
         { "flight_mode", NULL, MAVLINK_TYPE_UINT8_T, 0, 54, offsetof(mavlink_vkfly_edu_status_t, flight_mode) }, \
         } \
}
#else
#define MAVLINK_MESSAGE_INFO_VKFLY_EDU_STATUS { \
    "VKFLY_EDU_STATUS", \
    20, \
    {  { "unix_timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_vkfly_edu_status_t, unix_timestamp) }, \
         { "boot_timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 8, offsetof(mavlink_vkfly_edu_status_t, boot_timestamp) }, \
         { "seq", NULL, MAVLINK_TYPE_UINT32_T, 0, 12, offsetof(mavlink_vkfly_edu_status_t, seq) }, \
         { "dev_sn", NULL, MAVLINK_TYPE_UINT32_T, 0, 16, offsetof(mavlink_vkfly_edu_status_t, dev_sn) }, \
         { "dev_type", NULL, MAVLINK_TYPE_UINT8_T, 0, 50, offsetof(mavlink_vkfly_edu_status_t, dev_type) }, \
         { "retry_cnt", NULL, MAVLINK_TYPE_UINT8_T, 0, 51, offsetof(mavlink_vkfly_edu_status_t, retry_cnt) }, \
         { "fix_type", NULL, MAVLINK_TYPE_UINT8_T, 0, 52, offsetof(mavlink_vkfly_edu_status_t, fix_type) }, \
         { "reserve", NULL, MAVLINK_TYPE_UINT8_T, 0, 53, offsetof(mavlink_vkfly_edu_status_t, reserve) }, \
         { "longitude", NULL, MAVLINK_TYPE_INT32_T, 0, 20, offsetof(mavlink_vkfly_edu_status_t, longitude) }, \
         { "latitude", NULL, MAVLINK_TYPE_INT32_T, 0, 24, offsetof(mavlink_vkfly_edu_status_t, latitude) }, \
         { "amsl", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_vkfly_edu_status_t, amsl) }, \
         { "alt_relative", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_vkfly_edu_status_t, alt_relative) }, \
         { "ve", NULL, MAVLINK_TYPE_INT16_T, 0, 36, offsetof(mavlink_vkfly_edu_status_t, ve) }, \
         { "vn", NULL, MAVLINK_TYPE_INT16_T, 0, 38, offsetof(mavlink_vkfly_edu_status_t, vn) }, \
         { "vu", NULL, MAVLINK_TYPE_INT16_T, 0, 40, offsetof(mavlink_vkfly_edu_status_t, vu) }, \
         { "yaw", NULL, MAVLINK_TYPE_INT16_T, 0, 42, offsetof(mavlink_vkfly_edu_status_t, yaw) }, \
         { "pitch", NULL, MAVLINK_TYPE_INT16_T, 0, 44, offsetof(mavlink_vkfly_edu_status_t, pitch) }, \
         { "roll", NULL, MAVLINK_TYPE_INT16_T, 0, 46, offsetof(mavlink_vkfly_edu_status_t, roll) }, \
         { "yaw_rate", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_vkfly_edu_status_t, yaw_rate) }, \
         { "flight_mode", NULL, MAVLINK_TYPE_UINT8_T, 0, 54, offsetof(mavlink_vkfly_edu_status_t, flight_mode) }, \
         } \
}
#endif

/**
 * @brief Pack a vkfly_edu_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 unix_timestamp [ms] Unix timestamp in ms, from 1 Jan 1970.
 * @param boot_timestamp [ms] Timestamp in ms from system boot.
 * @param seq  Sequence number for this package.
 * @param dev_sn  Device SN number.
 * @param dev_type  0 for flight controller. 1 for elec-stake
 * @param retry_cnt  Retry send this message count.
 * @param fix_type  0 no fix, 1 single, 2 RTK
 * @param reserve  
 * @param longitude [degE7] wgs84 longitude
 * @param latitude [degE7] wgs84 latitude
 * @param amsl [m] altitude amsl
 * @param alt_relative [m] altitude above takeoff
 * @param ve [cm/s] 
 * @param vn [cm/s] 
 * @param vu [cm/s] 
 * @param yaw [cdeg] 
 * @param pitch [cdeg] 
 * @param roll [cdeg] 
 * @param yaw_rate [cdeg/s] 
 * @param flight_mode  
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vkfly_edu_status_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
                               uint64_t unix_timestamp, uint32_t boot_timestamp, uint32_t seq, uint32_t dev_sn, uint8_t dev_type, uint8_t retry_cnt, uint8_t fix_type, uint8_t reserve, int32_t longitude, int32_t latitude, float amsl, float alt_relative, int16_t ve, int16_t vn, int16_t vu, int16_t yaw, int16_t pitch, int16_t roll, int16_t yaw_rate, uint8_t flight_mode)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN];
    _mav_put_uint64_t(buf, 0, unix_timestamp);
    _mav_put_uint32_t(buf, 8, boot_timestamp);
    _mav_put_uint32_t(buf, 12, seq);
    _mav_put_uint32_t(buf, 16, dev_sn);
    _mav_put_int32_t(buf, 20, longitude);
    _mav_put_int32_t(buf, 24, latitude);
    _mav_put_float(buf, 28, amsl);
    _mav_put_float(buf, 32, alt_relative);
    _mav_put_int16_t(buf, 36, ve);
    _mav_put_int16_t(buf, 38, vn);
    _mav_put_int16_t(buf, 40, vu);
    _mav_put_int16_t(buf, 42, yaw);
    _mav_put_int16_t(buf, 44, pitch);
    _mav_put_int16_t(buf, 46, roll);
    _mav_put_int16_t(buf, 48, yaw_rate);
    _mav_put_uint8_t(buf, 50, dev_type);
    _mav_put_uint8_t(buf, 51, retry_cnt);
    _mav_put_uint8_t(buf, 52, fix_type);
    _mav_put_uint8_t(buf, 53, reserve);
    _mav_put_uint8_t(buf, 54, flight_mode);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN);
#else
    mavlink_vkfly_edu_status_t packet;
    packet.unix_timestamp = unix_timestamp;
    packet.boot_timestamp = boot_timestamp;
    packet.seq = seq;
    packet.dev_sn = dev_sn;
    packet.longitude = longitude;
    packet.latitude = latitude;
    packet.amsl = amsl;
    packet.alt_relative = alt_relative;
    packet.ve = ve;
    packet.vn = vn;
    packet.vu = vu;
    packet.yaw = yaw;
    packet.pitch = pitch;
    packet.roll = roll;
    packet.yaw_rate = yaw_rate;
    packet.dev_type = dev_type;
    packet.retry_cnt = retry_cnt;
    packet.fix_type = fix_type;
    packet.reserve = reserve;
    packet.flight_mode = flight_mode;

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

    msg->msgid = MAVLINK_MSG_ID_VKFLY_EDU_STATUS;
    return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC);
}

/**
 * @brief Pack a vkfly_edu_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 unix_timestamp [ms] Unix timestamp in ms, from 1 Jan 1970.
 * @param boot_timestamp [ms] Timestamp in ms from system boot.
 * @param seq  Sequence number for this package.
 * @param dev_sn  Device SN number.
 * @param dev_type  0 for flight controller. 1 for elec-stake
 * @param retry_cnt  Retry send this message count.
 * @param fix_type  0 no fix, 1 single, 2 RTK
 * @param reserve  
 * @param longitude [degE7] wgs84 longitude
 * @param latitude [degE7] wgs84 latitude
 * @param amsl [m] altitude amsl
 * @param alt_relative [m] altitude above takeoff
 * @param ve [cm/s] 
 * @param vn [cm/s] 
 * @param vu [cm/s] 
 * @param yaw [cdeg] 
 * @param pitch [cdeg] 
 * @param roll [cdeg] 
 * @param yaw_rate [cdeg/s] 
 * @param flight_mode  
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vkfly_edu_status_pack_status(uint8_t system_id, uint8_t component_id, mavlink_status_t *_status, mavlink_message_t* msg,
                               uint64_t unix_timestamp, uint32_t boot_timestamp, uint32_t seq, uint32_t dev_sn, uint8_t dev_type, uint8_t retry_cnt, uint8_t fix_type, uint8_t reserve, int32_t longitude, int32_t latitude, float amsl, float alt_relative, int16_t ve, int16_t vn, int16_t vu, int16_t yaw, int16_t pitch, int16_t roll, int16_t yaw_rate, uint8_t flight_mode)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN];
    _mav_put_uint64_t(buf, 0, unix_timestamp);
    _mav_put_uint32_t(buf, 8, boot_timestamp);
    _mav_put_uint32_t(buf, 12, seq);
    _mav_put_uint32_t(buf, 16, dev_sn);
    _mav_put_int32_t(buf, 20, longitude);
    _mav_put_int32_t(buf, 24, latitude);
    _mav_put_float(buf, 28, amsl);
    _mav_put_float(buf, 32, alt_relative);
    _mav_put_int16_t(buf, 36, ve);
    _mav_put_int16_t(buf, 38, vn);
    _mav_put_int16_t(buf, 40, vu);
    _mav_put_int16_t(buf, 42, yaw);
    _mav_put_int16_t(buf, 44, pitch);
    _mav_put_int16_t(buf, 46, roll);
    _mav_put_int16_t(buf, 48, yaw_rate);
    _mav_put_uint8_t(buf, 50, dev_type);
    _mav_put_uint8_t(buf, 51, retry_cnt);
    _mav_put_uint8_t(buf, 52, fix_type);
    _mav_put_uint8_t(buf, 53, reserve);
    _mav_put_uint8_t(buf, 54, flight_mode);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN);
#else
    mavlink_vkfly_edu_status_t packet;
    packet.unix_timestamp = unix_timestamp;
    packet.boot_timestamp = boot_timestamp;
    packet.seq = seq;
    packet.dev_sn = dev_sn;
    packet.longitude = longitude;
    packet.latitude = latitude;
    packet.amsl = amsl;
    packet.alt_relative = alt_relative;
    packet.ve = ve;
    packet.vn = vn;
    packet.vu = vu;
    packet.yaw = yaw;
    packet.pitch = pitch;
    packet.roll = roll;
    packet.yaw_rate = yaw_rate;
    packet.dev_type = dev_type;
    packet.retry_cnt = retry_cnt;
    packet.fix_type = fix_type;
    packet.reserve = reserve;
    packet.flight_mode = flight_mode;

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

    msg->msgid = MAVLINK_MSG_ID_VKFLY_EDU_STATUS;
#if MAVLINK_CRC_EXTRA
    return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC);
#else
    return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN);
#endif
}

/**
 * @brief Pack a vkfly_edu_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 unix_timestamp [ms] Unix timestamp in ms, from 1 Jan 1970.
 * @param boot_timestamp [ms] Timestamp in ms from system boot.
 * @param seq  Sequence number for this package.
 * @param dev_sn  Device SN number.
 * @param dev_type  0 for flight controller. 1 for elec-stake
 * @param retry_cnt  Retry send this message count.
 * @param fix_type  0 no fix, 1 single, 2 RTK
 * @param reserve  
 * @param longitude [degE7] wgs84 longitude
 * @param latitude [degE7] wgs84 latitude
 * @param amsl [m] altitude amsl
 * @param alt_relative [m] altitude above takeoff
 * @param ve [cm/s] 
 * @param vn [cm/s] 
 * @param vu [cm/s] 
 * @param yaw [cdeg] 
 * @param pitch [cdeg] 
 * @param roll [cdeg] 
 * @param yaw_rate [cdeg/s] 
 * @param flight_mode  
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vkfly_edu_status_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
                               mavlink_message_t* msg,
                                   uint64_t unix_timestamp,uint32_t boot_timestamp,uint32_t seq,uint32_t dev_sn,uint8_t dev_type,uint8_t retry_cnt,uint8_t fix_type,uint8_t reserve,int32_t longitude,int32_t latitude,float amsl,float alt_relative,int16_t ve,int16_t vn,int16_t vu,int16_t yaw,int16_t pitch,int16_t roll,int16_t yaw_rate,uint8_t flight_mode)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN];
    _mav_put_uint64_t(buf, 0, unix_timestamp);
    _mav_put_uint32_t(buf, 8, boot_timestamp);
    _mav_put_uint32_t(buf, 12, seq);
    _mav_put_uint32_t(buf, 16, dev_sn);
    _mav_put_int32_t(buf, 20, longitude);
    _mav_put_int32_t(buf, 24, latitude);
    _mav_put_float(buf, 28, amsl);
    _mav_put_float(buf, 32, alt_relative);
    _mav_put_int16_t(buf, 36, ve);
    _mav_put_int16_t(buf, 38, vn);
    _mav_put_int16_t(buf, 40, vu);
    _mav_put_int16_t(buf, 42, yaw);
    _mav_put_int16_t(buf, 44, pitch);
    _mav_put_int16_t(buf, 46, roll);
    _mav_put_int16_t(buf, 48, yaw_rate);
    _mav_put_uint8_t(buf, 50, dev_type);
    _mav_put_uint8_t(buf, 51, retry_cnt);
    _mav_put_uint8_t(buf, 52, fix_type);
    _mav_put_uint8_t(buf, 53, reserve);
    _mav_put_uint8_t(buf, 54, flight_mode);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN);
#else
    mavlink_vkfly_edu_status_t packet;
    packet.unix_timestamp = unix_timestamp;
    packet.boot_timestamp = boot_timestamp;
    packet.seq = seq;
    packet.dev_sn = dev_sn;
    packet.longitude = longitude;
    packet.latitude = latitude;
    packet.amsl = amsl;
    packet.alt_relative = alt_relative;
    packet.ve = ve;
    packet.vn = vn;
    packet.vu = vu;
    packet.yaw = yaw;
    packet.pitch = pitch;
    packet.roll = roll;
    packet.yaw_rate = yaw_rate;
    packet.dev_type = dev_type;
    packet.retry_cnt = retry_cnt;
    packet.fix_type = fix_type;
    packet.reserve = reserve;
    packet.flight_mode = flight_mode;

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

    msg->msgid = MAVLINK_MSG_ID_VKFLY_EDU_STATUS;
    return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC);
}

/**
 * @brief Encode a vkfly_edu_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 vkfly_edu_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vkfly_edu_status_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_vkfly_edu_status_t* vkfly_edu_status)
{
    return mavlink_msg_vkfly_edu_status_pack(system_id, component_id, msg, vkfly_edu_status->unix_timestamp, vkfly_edu_status->boot_timestamp, vkfly_edu_status->seq, vkfly_edu_status->dev_sn, vkfly_edu_status->dev_type, vkfly_edu_status->retry_cnt, vkfly_edu_status->fix_type, vkfly_edu_status->reserve, vkfly_edu_status->longitude, vkfly_edu_status->latitude, vkfly_edu_status->amsl, vkfly_edu_status->alt_relative, vkfly_edu_status->ve, vkfly_edu_status->vn, vkfly_edu_status->vu, vkfly_edu_status->yaw, vkfly_edu_status->pitch, vkfly_edu_status->roll, vkfly_edu_status->yaw_rate, vkfly_edu_status->flight_mode);
}

/**
 * @brief Encode a vkfly_edu_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 vkfly_edu_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vkfly_edu_status_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_vkfly_edu_status_t* vkfly_edu_status)
{
    return mavlink_msg_vkfly_edu_status_pack_chan(system_id, component_id, chan, msg, vkfly_edu_status->unix_timestamp, vkfly_edu_status->boot_timestamp, vkfly_edu_status->seq, vkfly_edu_status->dev_sn, vkfly_edu_status->dev_type, vkfly_edu_status->retry_cnt, vkfly_edu_status->fix_type, vkfly_edu_status->reserve, vkfly_edu_status->longitude, vkfly_edu_status->latitude, vkfly_edu_status->amsl, vkfly_edu_status->alt_relative, vkfly_edu_status->ve, vkfly_edu_status->vn, vkfly_edu_status->vu, vkfly_edu_status->yaw, vkfly_edu_status->pitch, vkfly_edu_status->roll, vkfly_edu_status->yaw_rate, vkfly_edu_status->flight_mode);
}

/**
 * @brief Encode a vkfly_edu_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 vkfly_edu_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vkfly_edu_status_encode_status(uint8_t system_id, uint8_t component_id, mavlink_status_t* _status, mavlink_message_t* msg, const mavlink_vkfly_edu_status_t* vkfly_edu_status)
{
    return mavlink_msg_vkfly_edu_status_pack_status(system_id, component_id, _status, msg,  vkfly_edu_status->unix_timestamp, vkfly_edu_status->boot_timestamp, vkfly_edu_status->seq, vkfly_edu_status->dev_sn, vkfly_edu_status->dev_type, vkfly_edu_status->retry_cnt, vkfly_edu_status->fix_type, vkfly_edu_status->reserve, vkfly_edu_status->longitude, vkfly_edu_status->latitude, vkfly_edu_status->amsl, vkfly_edu_status->alt_relative, vkfly_edu_status->ve, vkfly_edu_status->vn, vkfly_edu_status->vu, vkfly_edu_status->yaw, vkfly_edu_status->pitch, vkfly_edu_status->roll, vkfly_edu_status->yaw_rate, vkfly_edu_status->flight_mode);
}

/**
 * @brief Send a vkfly_edu_status message
 * @param chan MAVLink channel to send the message
 *
 * @param unix_timestamp [ms] Unix timestamp in ms, from 1 Jan 1970.
 * @param boot_timestamp [ms] Timestamp in ms from system boot.
 * @param seq  Sequence number for this package.
 * @param dev_sn  Device SN number.
 * @param dev_type  0 for flight controller. 1 for elec-stake
 * @param retry_cnt  Retry send this message count.
 * @param fix_type  0 no fix, 1 single, 2 RTK
 * @param reserve  
 * @param longitude [degE7] wgs84 longitude
 * @param latitude [degE7] wgs84 latitude
 * @param amsl [m] altitude amsl
 * @param alt_relative [m] altitude above takeoff
 * @param ve [cm/s] 
 * @param vn [cm/s] 
 * @param vu [cm/s] 
 * @param yaw [cdeg] 
 * @param pitch [cdeg] 
 * @param roll [cdeg] 
 * @param yaw_rate [cdeg/s] 
 * @param flight_mode  
 */
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS

static inline void mavlink_msg_vkfly_edu_status_send(mavlink_channel_t chan, uint64_t unix_timestamp, uint32_t boot_timestamp, uint32_t seq, uint32_t dev_sn, uint8_t dev_type, uint8_t retry_cnt, uint8_t fix_type, uint8_t reserve, int32_t longitude, int32_t latitude, float amsl, float alt_relative, int16_t ve, int16_t vn, int16_t vu, int16_t yaw, int16_t pitch, int16_t roll, int16_t yaw_rate, uint8_t flight_mode)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN];
    _mav_put_uint64_t(buf, 0, unix_timestamp);
    _mav_put_uint32_t(buf, 8, boot_timestamp);
    _mav_put_uint32_t(buf, 12, seq);
    _mav_put_uint32_t(buf, 16, dev_sn);
    _mav_put_int32_t(buf, 20, longitude);
    _mav_put_int32_t(buf, 24, latitude);
    _mav_put_float(buf, 28, amsl);
    _mav_put_float(buf, 32, alt_relative);
    _mav_put_int16_t(buf, 36, ve);
    _mav_put_int16_t(buf, 38, vn);
    _mav_put_int16_t(buf, 40, vu);
    _mav_put_int16_t(buf, 42, yaw);
    _mav_put_int16_t(buf, 44, pitch);
    _mav_put_int16_t(buf, 46, roll);
    _mav_put_int16_t(buf, 48, yaw_rate);
    _mav_put_uint8_t(buf, 50, dev_type);
    _mav_put_uint8_t(buf, 51, retry_cnt);
    _mav_put_uint8_t(buf, 52, fix_type);
    _mav_put_uint8_t(buf, 53, reserve);
    _mav_put_uint8_t(buf, 54, flight_mode);

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFLY_EDU_STATUS, buf, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC);
#else
    mavlink_vkfly_edu_status_t packet;
    packet.unix_timestamp = unix_timestamp;
    packet.boot_timestamp = boot_timestamp;
    packet.seq = seq;
    packet.dev_sn = dev_sn;
    packet.longitude = longitude;
    packet.latitude = latitude;
    packet.amsl = amsl;
    packet.alt_relative = alt_relative;
    packet.ve = ve;
    packet.vn = vn;
    packet.vu = vu;
    packet.yaw = yaw;
    packet.pitch = pitch;
    packet.roll = roll;
    packet.yaw_rate = yaw_rate;
    packet.dev_type = dev_type;
    packet.retry_cnt = retry_cnt;
    packet.fix_type = fix_type;
    packet.reserve = reserve;
    packet.flight_mode = flight_mode;

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFLY_EDU_STATUS, (const char *)&packet, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC);
#endif
}

/**
 * @brief Send a vkfly_edu_status message
 * @param chan MAVLink channel to send the message
 * @param struct The MAVLink struct to serialize
 */
static inline void mavlink_msg_vkfly_edu_status_send_struct(mavlink_channel_t chan, const mavlink_vkfly_edu_status_t* vkfly_edu_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    mavlink_msg_vkfly_edu_status_send(chan, vkfly_edu_status->unix_timestamp, vkfly_edu_status->boot_timestamp, vkfly_edu_status->seq, vkfly_edu_status->dev_sn, vkfly_edu_status->dev_type, vkfly_edu_status->retry_cnt, vkfly_edu_status->fix_type, vkfly_edu_status->reserve, vkfly_edu_status->longitude, vkfly_edu_status->latitude, vkfly_edu_status->amsl, vkfly_edu_status->alt_relative, vkfly_edu_status->ve, vkfly_edu_status->vn, vkfly_edu_status->vu, vkfly_edu_status->yaw, vkfly_edu_status->pitch, vkfly_edu_status->roll, vkfly_edu_status->yaw_rate, vkfly_edu_status->flight_mode);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFLY_EDU_STATUS, (const char *)vkfly_edu_status, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC);
#endif
}

#if MAVLINK_MSG_ID_VKFLY_EDU_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_vkfly_edu_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan,  uint64_t unix_timestamp, uint32_t boot_timestamp, uint32_t seq, uint32_t dev_sn, uint8_t dev_type, uint8_t retry_cnt, uint8_t fix_type, uint8_t reserve, int32_t longitude, int32_t latitude, float amsl, float alt_relative, int16_t ve, int16_t vn, int16_t vu, int16_t yaw, int16_t pitch, int16_t roll, int16_t yaw_rate, uint8_t flight_mode)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char *buf = (char *)msgbuf;
    _mav_put_uint64_t(buf, 0, unix_timestamp);
    _mav_put_uint32_t(buf, 8, boot_timestamp);
    _mav_put_uint32_t(buf, 12, seq);
    _mav_put_uint32_t(buf, 16, dev_sn);
    _mav_put_int32_t(buf, 20, longitude);
    _mav_put_int32_t(buf, 24, latitude);
    _mav_put_float(buf, 28, amsl);
    _mav_put_float(buf, 32, alt_relative);
    _mav_put_int16_t(buf, 36, ve);
    _mav_put_int16_t(buf, 38, vn);
    _mav_put_int16_t(buf, 40, vu);
    _mav_put_int16_t(buf, 42, yaw);
    _mav_put_int16_t(buf, 44, pitch);
    _mav_put_int16_t(buf, 46, roll);
    _mav_put_int16_t(buf, 48, yaw_rate);
    _mav_put_uint8_t(buf, 50, dev_type);
    _mav_put_uint8_t(buf, 51, retry_cnt);
    _mav_put_uint8_t(buf, 52, fix_type);
    _mav_put_uint8_t(buf, 53, reserve);
    _mav_put_uint8_t(buf, 54, flight_mode);

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFLY_EDU_STATUS, buf, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC);
#else
    mavlink_vkfly_edu_status_t *packet = (mavlink_vkfly_edu_status_t *)msgbuf;
    packet->unix_timestamp = unix_timestamp;
    packet->boot_timestamp = boot_timestamp;
    packet->seq = seq;
    packet->dev_sn = dev_sn;
    packet->longitude = longitude;
    packet->latitude = latitude;
    packet->amsl = amsl;
    packet->alt_relative = alt_relative;
    packet->ve = ve;
    packet->vn = vn;
    packet->vu = vu;
    packet->yaw = yaw;
    packet->pitch = pitch;
    packet->roll = roll;
    packet->yaw_rate = yaw_rate;
    packet->dev_type = dev_type;
    packet->retry_cnt = retry_cnt;
    packet->fix_type = fix_type;
    packet->reserve = reserve;
    packet->flight_mode = flight_mode;

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKFLY_EDU_STATUS, (const char *)packet, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_CRC);
#endif
}
#endif

#endif

// MESSAGE VKFLY_EDU_STATUS UNPACKING


/**
 * @brief Get field unix_timestamp from vkfly_edu_status message
 *
 * @return [ms] Unix timestamp in ms, from 1 Jan 1970.
 */
static inline uint64_t mavlink_msg_vkfly_edu_status_get_unix_timestamp(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint64_t(msg,  0);
}

/**
 * @brief Get field boot_timestamp from vkfly_edu_status message
 *
 * @return [ms] Timestamp in ms from system boot.
 */
static inline uint32_t mavlink_msg_vkfly_edu_status_get_boot_timestamp(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint32_t(msg,  8);
}

/**
 * @brief Get field seq from vkfly_edu_status message
 *
 * @return  Sequence number for this package.
 */
static inline uint32_t mavlink_msg_vkfly_edu_status_get_seq(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint32_t(msg,  12);
}

/**
 * @brief Get field dev_sn from vkfly_edu_status message
 *
 * @return  Device SN number.
 */
static inline uint32_t mavlink_msg_vkfly_edu_status_get_dev_sn(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint32_t(msg,  16);
}

/**
 * @brief Get field dev_type from vkfly_edu_status message
 *
 * @return  0 for flight controller. 1 for elec-stake
 */
static inline uint8_t mavlink_msg_vkfly_edu_status_get_dev_type(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  50);
}

/**
 * @brief Get field retry_cnt from vkfly_edu_status message
 *
 * @return  Retry send this message count.
 */
static inline uint8_t mavlink_msg_vkfly_edu_status_get_retry_cnt(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  51);
}

/**
 * @brief Get field fix_type from vkfly_edu_status message
 *
 * @return  0 no fix, 1 single, 2 RTK
 */
static inline uint8_t mavlink_msg_vkfly_edu_status_get_fix_type(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  52);
}

/**
 * @brief Get field reserve from vkfly_edu_status message
 *
 * @return  
 */
static inline uint8_t mavlink_msg_vkfly_edu_status_get_reserve(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  53);
}

/**
 * @brief Get field longitude from vkfly_edu_status message
 *
 * @return [degE7] wgs84 longitude
 */
static inline int32_t mavlink_msg_vkfly_edu_status_get_longitude(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int32_t(msg,  20);
}

/**
 * @brief Get field latitude from vkfly_edu_status message
 *
 * @return [degE7] wgs84 latitude
 */
static inline int32_t mavlink_msg_vkfly_edu_status_get_latitude(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int32_t(msg,  24);
}

/**
 * @brief Get field amsl from vkfly_edu_status message
 *
 * @return [m] altitude amsl
 */
static inline float mavlink_msg_vkfly_edu_status_get_amsl(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  28);
}

/**
 * @brief Get field alt_relative from vkfly_edu_status message
 *
 * @return [m] altitude above takeoff
 */
static inline float mavlink_msg_vkfly_edu_status_get_alt_relative(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  32);
}

/**
 * @brief Get field ve from vkfly_edu_status message
 *
 * @return [cm/s] 
 */
static inline int16_t mavlink_msg_vkfly_edu_status_get_ve(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int16_t(msg,  36);
}

/**
 * @brief Get field vn from vkfly_edu_status message
 *
 * @return [cm/s] 
 */
static inline int16_t mavlink_msg_vkfly_edu_status_get_vn(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int16_t(msg,  38);
}

/**
 * @brief Get field vu from vkfly_edu_status message
 *
 * @return [cm/s] 
 */
static inline int16_t mavlink_msg_vkfly_edu_status_get_vu(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int16_t(msg,  40);
}

/**
 * @brief Get field yaw from vkfly_edu_status message
 *
 * @return [cdeg] 
 */
static inline int16_t mavlink_msg_vkfly_edu_status_get_yaw(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int16_t(msg,  42);
}

/**
 * @brief Get field pitch from vkfly_edu_status message
 *
 * @return [cdeg] 
 */
static inline int16_t mavlink_msg_vkfly_edu_status_get_pitch(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int16_t(msg,  44);
}

/**
 * @brief Get field roll from vkfly_edu_status message
 *
 * @return [cdeg] 
 */
static inline int16_t mavlink_msg_vkfly_edu_status_get_roll(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int16_t(msg,  46);
}

/**
 * @brief Get field yaw_rate from vkfly_edu_status message
 *
 * @return [cdeg/s] 
 */
static inline int16_t mavlink_msg_vkfly_edu_status_get_yaw_rate(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int16_t(msg,  48);
}

/**
 * @brief Get field flight_mode from vkfly_edu_status message
 *
 * @return  
 */
static inline uint8_t mavlink_msg_vkfly_edu_status_get_flight_mode(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  54);
}

/**
 * @brief Decode a vkfly_edu_status message into a struct
 *
 * @param msg The message to decode
 * @param vkfly_edu_status C-struct to decode the message contents into
 */
static inline void mavlink_msg_vkfly_edu_status_decode(const mavlink_message_t* msg, mavlink_vkfly_edu_status_t* vkfly_edu_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    vkfly_edu_status->unix_timestamp = mavlink_msg_vkfly_edu_status_get_unix_timestamp(msg);
    vkfly_edu_status->boot_timestamp = mavlink_msg_vkfly_edu_status_get_boot_timestamp(msg);
    vkfly_edu_status->seq = mavlink_msg_vkfly_edu_status_get_seq(msg);
    vkfly_edu_status->dev_sn = mavlink_msg_vkfly_edu_status_get_dev_sn(msg);
    vkfly_edu_status->longitude = mavlink_msg_vkfly_edu_status_get_longitude(msg);
    vkfly_edu_status->latitude = mavlink_msg_vkfly_edu_status_get_latitude(msg);
    vkfly_edu_status->amsl = mavlink_msg_vkfly_edu_status_get_amsl(msg);
    vkfly_edu_status->alt_relative = mavlink_msg_vkfly_edu_status_get_alt_relative(msg);
    vkfly_edu_status->ve = mavlink_msg_vkfly_edu_status_get_ve(msg);
    vkfly_edu_status->vn = mavlink_msg_vkfly_edu_status_get_vn(msg);
    vkfly_edu_status->vu = mavlink_msg_vkfly_edu_status_get_vu(msg);
    vkfly_edu_status->yaw = mavlink_msg_vkfly_edu_status_get_yaw(msg);
    vkfly_edu_status->pitch = mavlink_msg_vkfly_edu_status_get_pitch(msg);
    vkfly_edu_status->roll = mavlink_msg_vkfly_edu_status_get_roll(msg);
    vkfly_edu_status->yaw_rate = mavlink_msg_vkfly_edu_status_get_yaw_rate(msg);
    vkfly_edu_status->dev_type = mavlink_msg_vkfly_edu_status_get_dev_type(msg);
    vkfly_edu_status->retry_cnt = mavlink_msg_vkfly_edu_status_get_retry_cnt(msg);
    vkfly_edu_status->fix_type = mavlink_msg_vkfly_edu_status_get_fix_type(msg);
    vkfly_edu_status->reserve = mavlink_msg_vkfly_edu_status_get_reserve(msg);
    vkfly_edu_status->flight_mode = mavlink_msg_vkfly_edu_status_get_flight_mode(msg);
#else
        uint8_t len = msg->len < MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN? msg->len : MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN;
        memset(vkfly_edu_status, 0, MAVLINK_MSG_ID_VKFLY_EDU_STATUS_LEN);
    memcpy(vkfly_edu_status, _MAV_PAYLOAD(msg), len);
#endif
}