VK_Mavlink/v2.0/VKFly/mavlink_msg_vkins_status.h

#pragma once
// MESSAGE VKINS_STATUS PACKING

#define MAVLINK_MSG_ID_VKINS_STATUS 53000


typedef struct __mavlink_vkins_status_t {
 uint32_t time_boot_ms; /*< [ms] Timestamp in ms from system boot.*/
 float g0; /*< [m/s/s] vkins initial calibrated gravitation acceleration.*/
 int32_t raw_latitude; /*< [degE7] raw longitude for data fusion*/
 int32_t raw_longitude; /*< [degE7] raw latitidue for data fusion*/
 float baro_alt; /*< [m] raw baromoter altitude for data fusion*/
 float raw_gps_alt; /*< [m] gps amsl altitude for data fusion*/
 int16_t temperature; /*< [cdegC] temperature*/
 uint8_t nav_status; /*<  VKINS
        navigation status flag.*/
 uint8_t s_flag1; /*<  vinks flag1*/
 uint8_t s_flag2; /*<  vinks flag2.*/
 uint8_t s_flag3; /*<  vinks flag3.*/
 uint8_t s_flag4; /*<  vinks flag4.*/
 uint8_t s_flag5; /*<  vinks flag5.*/
 uint8_t s_flag6; /*<  vinks flag6.*/
 uint8_t mag_calib_stage; /*<  vkins mag calib
        stage.*/
 uint8_t solv_psat_num; /*<  satelites number for position*/
 uint8_t solv_hsat_num; /*<  satelites number for heading*/
 uint8_t vibe_coe; /*<  */
} mavlink_vkins_status_t;

#define MAVLINK_MSG_ID_VKINS_STATUS_LEN 37
#define MAVLINK_MSG_ID_VKINS_STATUS_MIN_LEN 37
#define MAVLINK_MSG_ID_53000_LEN 37
#define MAVLINK_MSG_ID_53000_MIN_LEN 37

#define MAVLINK_MSG_ID_VKINS_STATUS_CRC 22
#define MAVLINK_MSG_ID_53000_CRC 22



#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_VKINS_STATUS { \
    53000, \
    "VKINS_STATUS", \
    18, \
    {  { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vkins_status_t, time_boot_ms) }, \
         { "nav_status", "0x%02x", MAVLINK_TYPE_UINT8_T, 0, 26, offsetof(mavlink_vkins_status_t, nav_status) }, \
         { "s_flag1", NULL, MAVLINK_TYPE_UINT8_T, 0, 27, offsetof(mavlink_vkins_status_t, s_flag1) }, \
         { "s_flag2", NULL, MAVLINK_TYPE_UINT8_T, 0, 28, offsetof(mavlink_vkins_status_t, s_flag2) }, \
         { "s_flag3", NULL, MAVLINK_TYPE_UINT8_T, 0, 29, offsetof(mavlink_vkins_status_t, s_flag3) }, \
         { "s_flag4", NULL, MAVLINK_TYPE_UINT8_T, 0, 30, offsetof(mavlink_vkins_status_t, s_flag4) }, \
         { "s_flag5", NULL, MAVLINK_TYPE_UINT8_T, 0, 31, offsetof(mavlink_vkins_status_t, s_flag5) }, \
         { "s_flag6", NULL, MAVLINK_TYPE_UINT8_T, 0, 32, offsetof(mavlink_vkins_status_t, s_flag6) }, \
         { "mag_calib_stage", NULL, MAVLINK_TYPE_UINT8_T, 0, 33, offsetof(mavlink_vkins_status_t, mag_calib_stage) }, \
         { "g0", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_vkins_status_t, g0) }, \
         { "raw_latitude", NULL, MAVLINK_TYPE_INT32_T, 0, 8, offsetof(mavlink_vkins_status_t, raw_latitude) }, \
         { "raw_longitude", NULL, MAVLINK_TYPE_INT32_T, 0, 12, offsetof(mavlink_vkins_status_t, raw_longitude) }, \
         { "baro_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_vkins_status_t, baro_alt) }, \
         { "raw_gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_vkins_status_t, raw_gps_alt) }, \
         { "solv_psat_num", NULL, MAVLINK_TYPE_UINT8_T, 0, 34, offsetof(mavlink_vkins_status_t, solv_psat_num) }, \
         { "solv_hsat_num", NULL, MAVLINK_TYPE_UINT8_T, 0, 35, offsetof(mavlink_vkins_status_t, solv_hsat_num) }, \
         { "temperature", NULL, MAVLINK_TYPE_INT16_T, 0, 24, offsetof(mavlink_vkins_status_t, temperature) }, \
         { "vibe_coe", NULL, MAVLINK_TYPE_UINT8_T, 0, 36, offsetof(mavlink_vkins_status_t, vibe_coe) }, \
         } \
}
#else
#define MAVLINK_MESSAGE_INFO_VKINS_STATUS { \
    "VKINS_STATUS", \
    18, \
    {  { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vkins_status_t, time_boot_ms) }, \
         { "nav_status", "0x%02x", MAVLINK_TYPE_UINT8_T, 0, 26, offsetof(mavlink_vkins_status_t, nav_status) }, \
         { "s_flag1", NULL, MAVLINK_TYPE_UINT8_T, 0, 27, offsetof(mavlink_vkins_status_t, s_flag1) }, \
         { "s_flag2", NULL, MAVLINK_TYPE_UINT8_T, 0, 28, offsetof(mavlink_vkins_status_t, s_flag2) }, \
         { "s_flag3", NULL, MAVLINK_TYPE_UINT8_T, 0, 29, offsetof(mavlink_vkins_status_t, s_flag3) }, \
         { "s_flag4", NULL, MAVLINK_TYPE_UINT8_T, 0, 30, offsetof(mavlink_vkins_status_t, s_flag4) }, \
         { "s_flag5", NULL, MAVLINK_TYPE_UINT8_T, 0, 31, offsetof(mavlink_vkins_status_t, s_flag5) }, \
         { "s_flag6", NULL, MAVLINK_TYPE_UINT8_T, 0, 32, offsetof(mavlink_vkins_status_t, s_flag6) }, \
         { "mag_calib_stage", NULL, MAVLINK_TYPE_UINT8_T, 0, 33, offsetof(mavlink_vkins_status_t, mag_calib_stage) }, \
         { "g0", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_vkins_status_t, g0) }, \
         { "raw_latitude", NULL, MAVLINK_TYPE_INT32_T, 0, 8, offsetof(mavlink_vkins_status_t, raw_latitude) }, \
         { "raw_longitude", NULL, MAVLINK_TYPE_INT32_T, 0, 12, offsetof(mavlink_vkins_status_t, raw_longitude) }, \
         { "baro_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_vkins_status_t, baro_alt) }, \
         { "raw_gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_vkins_status_t, raw_gps_alt) }, \
         { "solv_psat_num", NULL, MAVLINK_TYPE_UINT8_T, 0, 34, offsetof(mavlink_vkins_status_t, solv_psat_num) }, \
         { "solv_hsat_num", NULL, MAVLINK_TYPE_UINT8_T, 0, 35, offsetof(mavlink_vkins_status_t, solv_hsat_num) }, \
         { "temperature", NULL, MAVLINK_TYPE_INT16_T, 0, 24, offsetof(mavlink_vkins_status_t, temperature) }, \
         { "vibe_coe", NULL, MAVLINK_TYPE_UINT8_T, 0, 36, offsetof(mavlink_vkins_status_t, vibe_coe) }, \
         } \
}
#endif

/**
 * @brief Pack a vkins_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 nav_status  VKINS
        navigation status flag.
 * @param s_flag1  vinks flag1
 * @param s_flag2  vinks flag2.
 * @param s_flag3  vinks flag3.
 * @param s_flag4  vinks flag4.
 * @param s_flag5  vinks flag5.
 * @param s_flag6  vinks flag6.
 * @param mag_calib_stage  vkins mag calib
        stage.
 * @param g0 [m/s/s] vkins initial calibrated gravitation acceleration.
 * @param raw_latitude [degE7] raw longitude for data fusion
 * @param raw_longitude [degE7] raw latitidue for data fusion
 * @param baro_alt [m] raw baromoter altitude for data fusion
 * @param raw_gps_alt [m] gps amsl altitude for data fusion
 * @param solv_psat_num  satelites number for position
 * @param solv_hsat_num  satelites number for heading
 * @param temperature [cdegC] temperature
 * @param vibe_coe  
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vkins_status_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
                               uint32_t time_boot_ms, uint8_t nav_status, uint8_t s_flag1, uint8_t s_flag2, uint8_t s_flag3, uint8_t s_flag4, uint8_t s_flag5, uint8_t s_flag6, uint8_t mag_calib_stage, float g0, int32_t raw_latitude, int32_t raw_longitude, float baro_alt, float raw_gps_alt, uint8_t solv_psat_num, uint8_t solv_hsat_num, int16_t temperature, uint8_t vibe_coe)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKINS_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_float(buf, 4, g0);
    _mav_put_int32_t(buf, 8, raw_latitude);
    _mav_put_int32_t(buf, 12, raw_longitude);
    _mav_put_float(buf, 16, baro_alt);
    _mav_put_float(buf, 20, raw_gps_alt);
    _mav_put_int16_t(buf, 24, temperature);
    _mav_put_uint8_t(buf, 26, nav_status);
    _mav_put_uint8_t(buf, 27, s_flag1);
    _mav_put_uint8_t(buf, 28, s_flag2);
    _mav_put_uint8_t(buf, 29, s_flag3);
    _mav_put_uint8_t(buf, 30, s_flag4);
    _mav_put_uint8_t(buf, 31, s_flag5);
    _mav_put_uint8_t(buf, 32, s_flag6);
    _mav_put_uint8_t(buf, 33, mag_calib_stage);
    _mav_put_uint8_t(buf, 34, solv_psat_num);
    _mav_put_uint8_t(buf, 35, solv_hsat_num);
    _mav_put_uint8_t(buf, 36, vibe_coe);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VKINS_STATUS_LEN);
#else
    mavlink_vkins_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.g0 = g0;
    packet.raw_latitude = raw_latitude;
    packet.raw_longitude = raw_longitude;
    packet.baro_alt = baro_alt;
    packet.raw_gps_alt = raw_gps_alt;
    packet.temperature = temperature;
    packet.nav_status = nav_status;
    packet.s_flag1 = s_flag1;
    packet.s_flag2 = s_flag2;
    packet.s_flag3 = s_flag3;
    packet.s_flag4 = s_flag4;
    packet.s_flag5 = s_flag5;
    packet.s_flag6 = s_flag6;
    packet.mag_calib_stage = mag_calib_stage;
    packet.solv_psat_num = solv_psat_num;
    packet.solv_hsat_num = solv_hsat_num;
    packet.vibe_coe = vibe_coe;

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

    msg->msgid = MAVLINK_MSG_ID_VKINS_STATUS;
    return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_VKINS_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKINS_STATUS_LEN, MAVLINK_MSG_ID_VKINS_STATUS_CRC);
}

/**
 * @brief Pack a vkins_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 nav_status  VKINS
        navigation status flag.
 * @param s_flag1  vinks flag1
 * @param s_flag2  vinks flag2.
 * @param s_flag3  vinks flag3.
 * @param s_flag4  vinks flag4.
 * @param s_flag5  vinks flag5.
 * @param s_flag6  vinks flag6.
 * @param mag_calib_stage  vkins mag calib
        stage.
 * @param g0 [m/s/s] vkins initial calibrated gravitation acceleration.
 * @param raw_latitude [degE7] raw longitude for data fusion
 * @param raw_longitude [degE7] raw latitidue for data fusion
 * @param baro_alt [m] raw baromoter altitude for data fusion
 * @param raw_gps_alt [m] gps amsl altitude for data fusion
 * @param solv_psat_num  satelites number for position
 * @param solv_hsat_num  satelites number for heading
 * @param temperature [cdegC] temperature
 * @param vibe_coe  
 * @return length of the message in bytes (excluding serial stream start sign)
 */
static inline uint16_t mavlink_msg_vkins_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 nav_status,uint8_t s_flag1,uint8_t s_flag2,uint8_t s_flag3,uint8_t s_flag4,uint8_t s_flag5,uint8_t s_flag6,uint8_t mag_calib_stage,float g0,int32_t raw_latitude,int32_t raw_longitude,float baro_alt,float raw_gps_alt,uint8_t solv_psat_num,uint8_t solv_hsat_num,int16_t temperature,uint8_t vibe_coe)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKINS_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_float(buf, 4, g0);
    _mav_put_int32_t(buf, 8, raw_latitude);
    _mav_put_int32_t(buf, 12, raw_longitude);
    _mav_put_float(buf, 16, baro_alt);
    _mav_put_float(buf, 20, raw_gps_alt);
    _mav_put_int16_t(buf, 24, temperature);
    _mav_put_uint8_t(buf, 26, nav_status);
    _mav_put_uint8_t(buf, 27, s_flag1);
    _mav_put_uint8_t(buf, 28, s_flag2);
    _mav_put_uint8_t(buf, 29, s_flag3);
    _mav_put_uint8_t(buf, 30, s_flag4);
    _mav_put_uint8_t(buf, 31, s_flag5);
    _mav_put_uint8_t(buf, 32, s_flag6);
    _mav_put_uint8_t(buf, 33, mag_calib_stage);
    _mav_put_uint8_t(buf, 34, solv_psat_num);
    _mav_put_uint8_t(buf, 35, solv_hsat_num);
    _mav_put_uint8_t(buf, 36, vibe_coe);

        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VKINS_STATUS_LEN);
#else
    mavlink_vkins_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.g0 = g0;
    packet.raw_latitude = raw_latitude;
    packet.raw_longitude = raw_longitude;
    packet.baro_alt = baro_alt;
    packet.raw_gps_alt = raw_gps_alt;
    packet.temperature = temperature;
    packet.nav_status = nav_status;
    packet.s_flag1 = s_flag1;
    packet.s_flag2 = s_flag2;
    packet.s_flag3 = s_flag3;
    packet.s_flag4 = s_flag4;
    packet.s_flag5 = s_flag5;
    packet.s_flag6 = s_flag6;
    packet.mag_calib_stage = mag_calib_stage;
    packet.solv_psat_num = solv_psat_num;
    packet.solv_hsat_num = solv_hsat_num;
    packet.vibe_coe = vibe_coe;

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

    msg->msgid = MAVLINK_MSG_ID_VKINS_STATUS;
    return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_VKINS_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKINS_STATUS_LEN, MAVLINK_MSG_ID_VKINS_STATUS_CRC);
}

/**
 * @brief Encode a vkins_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 vkins_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vkins_status_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_vkins_status_t* vkins_status)
{
    return mavlink_msg_vkins_status_pack(system_id, component_id, msg, vkins_status->time_boot_ms, vkins_status->nav_status, vkins_status->s_flag1, vkins_status->s_flag2, vkins_status->s_flag3, vkins_status->s_flag4, vkins_status->s_flag5, vkins_status->s_flag6, vkins_status->mag_calib_stage, vkins_status->g0, vkins_status->raw_latitude, vkins_status->raw_longitude, vkins_status->baro_alt, vkins_status->raw_gps_alt, vkins_status->solv_psat_num, vkins_status->solv_hsat_num, vkins_status->temperature, vkins_status->vibe_coe);
}

/**
 * @brief Encode a vkins_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 vkins_status C-struct to read the message contents from
 */
static inline uint16_t mavlink_msg_vkins_status_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_vkins_status_t* vkins_status)
{
    return mavlink_msg_vkins_status_pack_chan(system_id, component_id, chan, msg, vkins_status->time_boot_ms, vkins_status->nav_status, vkins_status->s_flag1, vkins_status->s_flag2, vkins_status->s_flag3, vkins_status->s_flag4, vkins_status->s_flag5, vkins_status->s_flag6, vkins_status->mag_calib_stage, vkins_status->g0, vkins_status->raw_latitude, vkins_status->raw_longitude, vkins_status->baro_alt, vkins_status->raw_gps_alt, vkins_status->solv_psat_num, vkins_status->solv_hsat_num, vkins_status->temperature, vkins_status->vibe_coe);
}

/**
 * @brief Send a vkins_status message
 * @param chan MAVLink channel to send the message
 *
 * @param time_boot_ms [ms] Timestamp in ms from system boot.
 * @param nav_status  VKINS
        navigation status flag.
 * @param s_flag1  vinks flag1
 * @param s_flag2  vinks flag2.
 * @param s_flag3  vinks flag3.
 * @param s_flag4  vinks flag4.
 * @param s_flag5  vinks flag5.
 * @param s_flag6  vinks flag6.
 * @param mag_calib_stage  vkins mag calib
        stage.
 * @param g0 [m/s/s] vkins initial calibrated gravitation acceleration.
 * @param raw_latitude [degE7] raw longitude for data fusion
 * @param raw_longitude [degE7] raw latitidue for data fusion
 * @param baro_alt [m] raw baromoter altitude for data fusion
 * @param raw_gps_alt [m] gps amsl altitude for data fusion
 * @param solv_psat_num  satelites number for position
 * @param solv_hsat_num  satelites number for heading
 * @param temperature [cdegC] temperature
 * @param vibe_coe  
 */
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS

static inline void mavlink_msg_vkins_status_send(mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t nav_status, uint8_t s_flag1, uint8_t s_flag2, uint8_t s_flag3, uint8_t s_flag4, uint8_t s_flag5, uint8_t s_flag6, uint8_t mag_calib_stage, float g0, int32_t raw_latitude, int32_t raw_longitude, float baro_alt, float raw_gps_alt, uint8_t solv_psat_num, uint8_t solv_hsat_num, int16_t temperature, uint8_t vibe_coe)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    char buf[MAVLINK_MSG_ID_VKINS_STATUS_LEN];
    _mav_put_uint32_t(buf, 0, time_boot_ms);
    _mav_put_float(buf, 4, g0);
    _mav_put_int32_t(buf, 8, raw_latitude);
    _mav_put_int32_t(buf, 12, raw_longitude);
    _mav_put_float(buf, 16, baro_alt);
    _mav_put_float(buf, 20, raw_gps_alt);
    _mav_put_int16_t(buf, 24, temperature);
    _mav_put_uint8_t(buf, 26, nav_status);
    _mav_put_uint8_t(buf, 27, s_flag1);
    _mav_put_uint8_t(buf, 28, s_flag2);
    _mav_put_uint8_t(buf, 29, s_flag3);
    _mav_put_uint8_t(buf, 30, s_flag4);
    _mav_put_uint8_t(buf, 31, s_flag5);
    _mav_put_uint8_t(buf, 32, s_flag6);
    _mav_put_uint8_t(buf, 33, mag_calib_stage);
    _mav_put_uint8_t(buf, 34, solv_psat_num);
    _mav_put_uint8_t(buf, 35, solv_hsat_num);
    _mav_put_uint8_t(buf, 36, vibe_coe);

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKINS_STATUS, buf, MAVLINK_MSG_ID_VKINS_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKINS_STATUS_LEN, MAVLINK_MSG_ID_VKINS_STATUS_CRC);
#else
    mavlink_vkins_status_t packet;
    packet.time_boot_ms = time_boot_ms;
    packet.g0 = g0;
    packet.raw_latitude = raw_latitude;
    packet.raw_longitude = raw_longitude;
    packet.baro_alt = baro_alt;
    packet.raw_gps_alt = raw_gps_alt;
    packet.temperature = temperature;
    packet.nav_status = nav_status;
    packet.s_flag1 = s_flag1;
    packet.s_flag2 = s_flag2;
    packet.s_flag3 = s_flag3;
    packet.s_flag4 = s_flag4;
    packet.s_flag5 = s_flag5;
    packet.s_flag6 = s_flag6;
    packet.mag_calib_stage = mag_calib_stage;
    packet.solv_psat_num = solv_psat_num;
    packet.solv_hsat_num = solv_hsat_num;
    packet.vibe_coe = vibe_coe;

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKINS_STATUS, (const char *)&packet, MAVLINK_MSG_ID_VKINS_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKINS_STATUS_LEN, MAVLINK_MSG_ID_VKINS_STATUS_CRC);
#endif
}

/**
 * @brief Send a vkins_status message
 * @param chan MAVLink channel to send the message
 * @param struct The MAVLink struct to serialize
 */
static inline void mavlink_msg_vkins_status_send_struct(mavlink_channel_t chan, const mavlink_vkins_status_t* vkins_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    mavlink_msg_vkins_status_send(chan, vkins_status->time_boot_ms, vkins_status->nav_status, vkins_status->s_flag1, vkins_status->s_flag2, vkins_status->s_flag3, vkins_status->s_flag4, vkins_status->s_flag5, vkins_status->s_flag6, vkins_status->mag_calib_stage, vkins_status->g0, vkins_status->raw_latitude, vkins_status->raw_longitude, vkins_status->baro_alt, vkins_status->raw_gps_alt, vkins_status->solv_psat_num, vkins_status->solv_hsat_num, vkins_status->temperature, vkins_status->vibe_coe);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKINS_STATUS, (const char *)vkins_status, MAVLINK_MSG_ID_VKINS_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKINS_STATUS_LEN, MAVLINK_MSG_ID_VKINS_STATUS_CRC);
#endif
}

#if MAVLINK_MSG_ID_VKINS_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_vkins_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan,  uint32_t time_boot_ms, uint8_t nav_status, uint8_t s_flag1, uint8_t s_flag2, uint8_t s_flag3, uint8_t s_flag4, uint8_t s_flag5, uint8_t s_flag6, uint8_t mag_calib_stage, float g0, int32_t raw_latitude, int32_t raw_longitude, float baro_alt, float raw_gps_alt, uint8_t solv_psat_num, uint8_t solv_hsat_num, int16_t temperature, uint8_t vibe_coe)
{
#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, 4, g0);
    _mav_put_int32_t(buf, 8, raw_latitude);
    _mav_put_int32_t(buf, 12, raw_longitude);
    _mav_put_float(buf, 16, baro_alt);
    _mav_put_float(buf, 20, raw_gps_alt);
    _mav_put_int16_t(buf, 24, temperature);
    _mav_put_uint8_t(buf, 26, nav_status);
    _mav_put_uint8_t(buf, 27, s_flag1);
    _mav_put_uint8_t(buf, 28, s_flag2);
    _mav_put_uint8_t(buf, 29, s_flag3);
    _mav_put_uint8_t(buf, 30, s_flag4);
    _mav_put_uint8_t(buf, 31, s_flag5);
    _mav_put_uint8_t(buf, 32, s_flag6);
    _mav_put_uint8_t(buf, 33, mag_calib_stage);
    _mav_put_uint8_t(buf, 34, solv_psat_num);
    _mav_put_uint8_t(buf, 35, solv_hsat_num);
    _mav_put_uint8_t(buf, 36, vibe_coe);

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKINS_STATUS, buf, MAVLINK_MSG_ID_VKINS_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKINS_STATUS_LEN, MAVLINK_MSG_ID_VKINS_STATUS_CRC);
#else
    mavlink_vkins_status_t *packet = (mavlink_vkins_status_t *)msgbuf;
    packet->time_boot_ms = time_boot_ms;
    packet->g0 = g0;
    packet->raw_latitude = raw_latitude;
    packet->raw_longitude = raw_longitude;
    packet->baro_alt = baro_alt;
    packet->raw_gps_alt = raw_gps_alt;
    packet->temperature = temperature;
    packet->nav_status = nav_status;
    packet->s_flag1 = s_flag1;
    packet->s_flag2 = s_flag2;
    packet->s_flag3 = s_flag3;
    packet->s_flag4 = s_flag4;
    packet->s_flag5 = s_flag5;
    packet->s_flag6 = s_flag6;
    packet->mag_calib_stage = mag_calib_stage;
    packet->solv_psat_num = solv_psat_num;
    packet->solv_hsat_num = solv_hsat_num;
    packet->vibe_coe = vibe_coe;

    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VKINS_STATUS, (const char *)packet, MAVLINK_MSG_ID_VKINS_STATUS_MIN_LEN, MAVLINK_MSG_ID_VKINS_STATUS_LEN, MAVLINK_MSG_ID_VKINS_STATUS_CRC);
#endif
}
#endif

#endif

// MESSAGE VKINS_STATUS UNPACKING


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

/**
 * @brief Get field nav_status from vkins_status message
 *
 * @return  VKINS
        navigation status flag.
 */
static inline uint8_t mavlink_msg_vkins_status_get_nav_status(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  26);
}

/**
 * @brief Get field s_flag1 from vkins_status message
 *
 * @return  vinks flag1
 */
static inline uint8_t mavlink_msg_vkins_status_get_s_flag1(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  27);
}

/**
 * @brief Get field s_flag2 from vkins_status message
 *
 * @return  vinks flag2.
 */
static inline uint8_t mavlink_msg_vkins_status_get_s_flag2(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  28);
}

/**
 * @brief Get field s_flag3 from vkins_status message
 *
 * @return  vinks flag3.
 */
static inline uint8_t mavlink_msg_vkins_status_get_s_flag3(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  29);
}

/**
 * @brief Get field s_flag4 from vkins_status message
 *
 * @return  vinks flag4.
 */
static inline uint8_t mavlink_msg_vkins_status_get_s_flag4(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  30);
}

/**
 * @brief Get field s_flag5 from vkins_status message
 *
 * @return  vinks flag5.
 */
static inline uint8_t mavlink_msg_vkins_status_get_s_flag5(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  31);
}

/**
 * @brief Get field s_flag6 from vkins_status message
 *
 * @return  vinks flag6.
 */
static inline uint8_t mavlink_msg_vkins_status_get_s_flag6(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  32);
}

/**
 * @brief Get field mag_calib_stage from vkins_status message
 *
 * @return  vkins mag calib
        stage.
 */
static inline uint8_t mavlink_msg_vkins_status_get_mag_calib_stage(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  33);
}

/**
 * @brief Get field g0 from vkins_status message
 *
 * @return [m/s/s] vkins initial calibrated gravitation acceleration.
 */
static inline float mavlink_msg_vkins_status_get_g0(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  4);
}

/**
 * @brief Get field raw_latitude from vkins_status message
 *
 * @return [degE7] raw longitude for data fusion
 */
static inline int32_t mavlink_msg_vkins_status_get_raw_latitude(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int32_t(msg,  8);
}

/**
 * @brief Get field raw_longitude from vkins_status message
 *
 * @return [degE7] raw latitidue for data fusion
 */
static inline int32_t mavlink_msg_vkins_status_get_raw_longitude(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int32_t(msg,  12);
}

/**
 * @brief Get field baro_alt from vkins_status message
 *
 * @return [m] raw baromoter altitude for data fusion
 */
static inline float mavlink_msg_vkins_status_get_baro_alt(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  16);
}

/**
 * @brief Get field raw_gps_alt from vkins_status message
 *
 * @return [m] gps amsl altitude for data fusion
 */
static inline float mavlink_msg_vkins_status_get_raw_gps_alt(const mavlink_message_t* msg)
{
    return _MAV_RETURN_float(msg,  20);
}

/**
 * @brief Get field solv_psat_num from vkins_status message
 *
 * @return  satelites number for position
 */
static inline uint8_t mavlink_msg_vkins_status_get_solv_psat_num(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  34);
}

/**
 * @brief Get field solv_hsat_num from vkins_status message
 *
 * @return  satelites number for heading
 */
static inline uint8_t mavlink_msg_vkins_status_get_solv_hsat_num(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  35);
}

/**
 * @brief Get field temperature from vkins_status message
 *
 * @return [cdegC] temperature
 */
static inline int16_t mavlink_msg_vkins_status_get_temperature(const mavlink_message_t* msg)
{
    return _MAV_RETURN_int16_t(msg,  24);
}

/**
 * @brief Get field vibe_coe from vkins_status message
 *
 * @return  
 */
static inline uint8_t mavlink_msg_vkins_status_get_vibe_coe(const mavlink_message_t* msg)
{
    return _MAV_RETURN_uint8_t(msg,  36);
}

/**
 * @brief Decode a vkins_status message into a struct
 *
 * @param msg The message to decode
 * @param vkins_status C-struct to decode the message contents into
 */
static inline void mavlink_msg_vkins_status_decode(const mavlink_message_t* msg, mavlink_vkins_status_t* vkins_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
    vkins_status->time_boot_ms = mavlink_msg_vkins_status_get_time_boot_ms(msg);
    vkins_status->g0 = mavlink_msg_vkins_status_get_g0(msg);
    vkins_status->raw_latitude = mavlink_msg_vkins_status_get_raw_latitude(msg);
    vkins_status->raw_longitude = mavlink_msg_vkins_status_get_raw_longitude(msg);
    vkins_status->baro_alt = mavlink_msg_vkins_status_get_baro_alt(msg);
    vkins_status->raw_gps_alt = mavlink_msg_vkins_status_get_raw_gps_alt(msg);
    vkins_status->temperature = mavlink_msg_vkins_status_get_temperature(msg);
    vkins_status->nav_status = mavlink_msg_vkins_status_get_nav_status(msg);
    vkins_status->s_flag1 = mavlink_msg_vkins_status_get_s_flag1(msg);
    vkins_status->s_flag2 = mavlink_msg_vkins_status_get_s_flag2(msg);
    vkins_status->s_flag3 = mavlink_msg_vkins_status_get_s_flag3(msg);
    vkins_status->s_flag4 = mavlink_msg_vkins_status_get_s_flag4(msg);
    vkins_status->s_flag5 = mavlink_msg_vkins_status_get_s_flag5(msg);
    vkins_status->s_flag6 = mavlink_msg_vkins_status_get_s_flag6(msg);
    vkins_status->mag_calib_stage = mavlink_msg_vkins_status_get_mag_calib_stage(msg);
    vkins_status->solv_psat_num = mavlink_msg_vkins_status_get_solv_psat_num(msg);
    vkins_status->solv_hsat_num = mavlink_msg_vkins_status_get_solv_hsat_num(msg);
    vkins_status->vibe_coe = mavlink_msg_vkins_status_get_vibe_coe(msg);
#else
        uint8_t len = msg->len < MAVLINK_MSG_ID_VKINS_STATUS_LEN? msg->len : MAVLINK_MSG_ID_VKINS_STATUS_LEN;
        memset(vkins_status, 0, MAVLINK_MSG_ID_VKINS_STATUS_LEN);
    memcpy(vkins_status, _MAV_PAYLOAD(msg), len);
#endif
}