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PullupDev/lib/mavlink/ardupilotmega/mavlink_msg_airspeed_autocal.h
tk 1dff1bfd33 【类 型】：fix 更新mavlink库 
【原  因】：更全更新
【过  程】：
【影  响】：

# 类型 包含:
# feat：新功能（feature）
# fix：修补bug
# docs：文档（documentation）
# style： 格式（不影响代码运行的变动）
# refactor：重构（即不是新增功能，也不是修改bug的代码变动）
# test：增加测试
# chore：构建过程或辅助工具的变动
2024-08-19 16:16:39 +08:00

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#pragma once
// MESSAGE AIRSPEED_AUTOCAL PACKING
#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL 174
MAVPACKED(
typedef struct __mavlink_airspeed_autocal_t {
float vx; /*< [m/s] GPS velocity north.*/
float vy; /*< [m/s] GPS velocity east.*/
float vz; /*< [m/s] GPS velocity down.*/
float diff_pressure; /*< [Pa] Differential pressure.*/
float EAS2TAS; /*< Estimated to true airspeed ratio.*/
float ratio; /*< Airspeed ratio.*/
float state_x; /*< EKF state x.*/
float state_y; /*< EKF state y.*/
float state_z; /*< EKF state z.*/
float Pax; /*< EKF Pax.*/
float Pby; /*< EKF Pby.*/
float Pcz; /*< EKF Pcz.*/
}) mavlink_airspeed_autocal_t;
#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN 48
#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN 48
#define MAVLINK_MSG_ID_174_LEN 48
#define MAVLINK_MSG_ID_174_MIN_LEN 48
#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC 167
#define MAVLINK_MSG_ID_174_CRC 167
#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL { \
174, \
"AIRSPEED_AUTOCAL", \
12, \
{ { "vx", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_autocal_t, vx) }, \
{ "vy", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_autocal_t, vy) }, \
{ "vz", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_airspeed_autocal_t, vz) }, \
{ "diff_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_airspeed_autocal_t, diff_pressure) }, \
{ "EAS2TAS", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_airspeed_autocal_t, EAS2TAS) }, \
{ "ratio", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_airspeed_autocal_t, ratio) }, \
{ "state_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_airspeed_autocal_t, state_x) }, \
{ "state_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_airspeed_autocal_t, state_y) }, \
{ "state_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_airspeed_autocal_t, state_z) }, \
{ "Pax", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_airspeed_autocal_t, Pax) }, \
{ "Pby", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_airspeed_autocal_t, Pby) }, \
{ "Pcz", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_airspeed_autocal_t, Pcz) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL { \
"AIRSPEED_AUTOCAL", \
12, \
{ { "vx", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_autocal_t, vx) }, \
{ "vy", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_autocal_t, vy) }, \
{ "vz", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_airspeed_autocal_t, vz) }, \
{ "diff_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_airspeed_autocal_t, diff_pressure) }, \
{ "EAS2TAS", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_airspeed_autocal_t, EAS2TAS) }, \
{ "ratio", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_airspeed_autocal_t, ratio) }, \
{ "state_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_airspeed_autocal_t, state_x) }, \
{ "state_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_airspeed_autocal_t, state_y) }, \
{ "state_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_airspeed_autocal_t, state_z) }, \
{ "Pax", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_airspeed_autocal_t, Pax) }, \
{ "Pby", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_airspeed_autocal_t, Pby) }, \
{ "Pcz", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_airspeed_autocal_t, Pcz) }, \
} \
}
#endif
/**
* @brief Pack a airspeed_autocal 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 vx [m/s] GPS velocity north.
* @param vy [m/s] GPS velocity east.
* @param vz [m/s] GPS velocity down.
* @param diff_pressure [Pa] Differential pressure.
* @param EAS2TAS Estimated to true airspeed ratio.
* @param ratio Airspeed ratio.
* @param state_x EKF state x.
* @param state_y EKF state y.
* @param state_z EKF state z.
* @param Pax EKF Pax.
* @param Pby EKF Pby.
* @param Pcz EKF Pcz.
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_airspeed_autocal_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN];
_mav_put_float(buf, 0, vx);
_mav_put_float(buf, 4, vy);
_mav_put_float(buf, 8, vz);
_mav_put_float(buf, 12, diff_pressure);
_mav_put_float(buf, 16, EAS2TAS);
_mav_put_float(buf, 20, ratio);
_mav_put_float(buf, 24, state_x);
_mav_put_float(buf, 28, state_y);
_mav_put_float(buf, 32, state_z);
_mav_put_float(buf, 36, Pax);
_mav_put_float(buf, 40, Pby);
_mav_put_float(buf, 44, Pcz);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
#else
mavlink_airspeed_autocal_t packet;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.diff_pressure = diff_pressure;
packet.EAS2TAS = EAS2TAS;
packet.ratio = ratio;
packet.state_x = state_x;
packet.state_y = state_y;
packet.state_z = state_z;
packet.Pax = Pax;
packet.Pby = Pby;
packet.Pcz = Pcz;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_AIRSPEED_AUTOCAL;
return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC);
}
/**
* @brief Pack a airspeed_autocal 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 vx [m/s] GPS velocity north.
* @param vy [m/s] GPS velocity east.
* @param vz [m/s] GPS velocity down.
* @param diff_pressure [Pa] Differential pressure.
* @param EAS2TAS Estimated to true airspeed ratio.
* @param ratio Airspeed ratio.
* @param state_x EKF state x.
* @param state_y EKF state y.
* @param state_z EKF state z.
* @param Pax EKF Pax.
* @param Pby EKF Pby.
* @param Pcz EKF Pcz.
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_airspeed_autocal_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
float vx,float vy,float vz,float diff_pressure,float EAS2TAS,float ratio,float state_x,float state_y,float state_z,float Pax,float Pby,float Pcz)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN];
_mav_put_float(buf, 0, vx);
_mav_put_float(buf, 4, vy);
_mav_put_float(buf, 8, vz);
_mav_put_float(buf, 12, diff_pressure);
_mav_put_float(buf, 16, EAS2TAS);
_mav_put_float(buf, 20, ratio);
_mav_put_float(buf, 24, state_x);
_mav_put_float(buf, 28, state_y);
_mav_put_float(buf, 32, state_z);
_mav_put_float(buf, 36, Pax);
_mav_put_float(buf, 40, Pby);
_mav_put_float(buf, 44, Pcz);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
#else
mavlink_airspeed_autocal_t packet;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.diff_pressure = diff_pressure;
packet.EAS2TAS = EAS2TAS;
packet.ratio = ratio;
packet.state_x = state_x;
packet.state_y = state_y;
packet.state_z = state_z;
packet.Pax = Pax;
packet.Pby = Pby;
packet.Pcz = Pcz;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_AIRSPEED_AUTOCAL;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC);
}
/**
* @brief Encode a airspeed_autocal 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 airspeed_autocal C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_airspeed_autocal_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_airspeed_autocal_t* airspeed_autocal)
{
return mavlink_msg_airspeed_autocal_pack(system_id, component_id, msg, airspeed_autocal->vx, airspeed_autocal->vy, airspeed_autocal->vz, airspeed_autocal->diff_pressure, airspeed_autocal->EAS2TAS, airspeed_autocal->ratio, airspeed_autocal->state_x, airspeed_autocal->state_y, airspeed_autocal->state_z, airspeed_autocal->Pax, airspeed_autocal->Pby, airspeed_autocal->Pcz);
}
/**
* @brief Encode a airspeed_autocal 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 airspeed_autocal C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_airspeed_autocal_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_airspeed_autocal_t* airspeed_autocal)
{
return mavlink_msg_airspeed_autocal_pack_chan(system_id, component_id, chan, msg, airspeed_autocal->vx, airspeed_autocal->vy, airspeed_autocal->vz, airspeed_autocal->diff_pressure, airspeed_autocal->EAS2TAS, airspeed_autocal->ratio, airspeed_autocal->state_x, airspeed_autocal->state_y, airspeed_autocal->state_z, airspeed_autocal->Pax, airspeed_autocal->Pby, airspeed_autocal->Pcz);
}
/**
* @brief Send a airspeed_autocal message
* @param chan MAVLink channel to send the message
*
* @param vx [m/s] GPS velocity north.
* @param vy [m/s] GPS velocity east.
* @param vz [m/s] GPS velocity down.
* @param diff_pressure [Pa] Differential pressure.
* @param EAS2TAS Estimated to true airspeed ratio.
* @param ratio Airspeed ratio.
* @param state_x EKF state x.
* @param state_y EKF state y.
* @param state_z EKF state z.
* @param Pax EKF Pax.
* @param Pby EKF Pby.
* @param Pcz EKF Pcz.
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_airspeed_autocal_send(mavlink_channel_t chan, float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN];
_mav_put_float(buf, 0, vx);
_mav_put_float(buf, 4, vy);
_mav_put_float(buf, 8, vz);
_mav_put_float(buf, 12, diff_pressure);
_mav_put_float(buf, 16, EAS2TAS);
_mav_put_float(buf, 20, ratio);
_mav_put_float(buf, 24, state_x);
_mav_put_float(buf, 28, state_y);
_mav_put_float(buf, 32, state_z);
_mav_put_float(buf, 36, Pax);
_mav_put_float(buf, 40, Pby);
_mav_put_float(buf, 44, Pcz);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC);
#else
mavlink_airspeed_autocal_t packet;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.diff_pressure = diff_pressure;
packet.EAS2TAS = EAS2TAS;
packet.ratio = ratio;
packet.state_x = state_x;
packet.state_y = state_y;
packet.state_z = state_z;
packet.Pax = Pax;
packet.Pby = Pby;
packet.Pcz = Pcz;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)&packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC);
#endif
}
/**
* @brief Send a airspeed_autocal message
* @param chan MAVLink channel to send the message
* @param struct The MAVLink struct to serialize
*/
static inline void mavlink_msg_airspeed_autocal_send_struct(mavlink_channel_t chan, const mavlink_airspeed_autocal_t* airspeed_autocal)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_airspeed_autocal_send(chan, airspeed_autocal->vx, airspeed_autocal->vy, airspeed_autocal->vz, airspeed_autocal->diff_pressure, airspeed_autocal->EAS2TAS, airspeed_autocal->ratio, airspeed_autocal->state_x, airspeed_autocal->state_y, airspeed_autocal->state_z, airspeed_autocal->Pax, airspeed_autocal->Pby, airspeed_autocal->Pcz);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)airspeed_autocal, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC);
#endif
}
#if MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN <= MAVLINK_MAX_PAYLOAD_LEN
/*
This varient 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_airspeed_autocal_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_float(buf, 0, vx);
_mav_put_float(buf, 4, vy);
_mav_put_float(buf, 8, vz);
_mav_put_float(buf, 12, diff_pressure);
_mav_put_float(buf, 16, EAS2TAS);
_mav_put_float(buf, 20, ratio);
_mav_put_float(buf, 24, state_x);
_mav_put_float(buf, 28, state_y);
_mav_put_float(buf, 32, state_z);
_mav_put_float(buf, 36, Pax);
_mav_put_float(buf, 40, Pby);
_mav_put_float(buf, 44, Pcz);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC);
#else
mavlink_airspeed_autocal_t *packet = (mavlink_airspeed_autocal_t *)msgbuf;
packet->vx = vx;
packet->vy = vy;
packet->vz = vz;
packet->diff_pressure = diff_pressure;
packet->EAS2TAS = EAS2TAS;
packet->ratio = ratio;
packet->state_x = state_x;
packet->state_y = state_y;
packet->state_z = state_z;
packet->Pax = Pax;
packet->Pby = Pby;
packet->Pcz = Pcz;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC);
#endif
}
#endif
#endif
// MESSAGE AIRSPEED_AUTOCAL UNPACKING
/**
* @brief Get field vx from airspeed_autocal message
*
* @return [m/s] GPS velocity north.
*/
static inline float mavlink_msg_airspeed_autocal_get_vx(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 0);
}
/**
* @brief Get field vy from airspeed_autocal message
*
* @return [m/s] GPS velocity east.
*/
static inline float mavlink_msg_airspeed_autocal_get_vy(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 4);
}
/**
* @brief Get field vz from airspeed_autocal message
*
* @return [m/s] GPS velocity down.
*/
static inline float mavlink_msg_airspeed_autocal_get_vz(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 8);
}
/**
* @brief Get field diff_pressure from airspeed_autocal message
*
* @return [Pa] Differential pressure.
*/
static inline float mavlink_msg_airspeed_autocal_get_diff_pressure(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 12);
}
/**
* @brief Get field EAS2TAS from airspeed_autocal message
*
* @return Estimated to true airspeed ratio.
*/
static inline float mavlink_msg_airspeed_autocal_get_EAS2TAS(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 16);
}
/**
* @brief Get field ratio from airspeed_autocal message
*
* @return Airspeed ratio.
*/
static inline float mavlink_msg_airspeed_autocal_get_ratio(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 20);
}
/**
* @brief Get field state_x from airspeed_autocal message
*
* @return EKF state x.
*/
static inline float mavlink_msg_airspeed_autocal_get_state_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
}
/**
* @brief Get field state_y from airspeed_autocal message
*
* @return EKF state y.
*/
static inline float mavlink_msg_airspeed_autocal_get_state_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 28);
}
/**
* @brief Get field state_z from airspeed_autocal message
*
* @return EKF state z.
*/
static inline float mavlink_msg_airspeed_autocal_get_state_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 32);
}
/**
* @brief Get field Pax from airspeed_autocal message
*
* @return EKF Pax.
*/
static inline float mavlink_msg_airspeed_autocal_get_Pax(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 36);
}
/**
* @brief Get field Pby from airspeed_autocal message
*
* @return EKF Pby.
*/
static inline float mavlink_msg_airspeed_autocal_get_Pby(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 40);
}
/**
* @brief Get field Pcz from airspeed_autocal message
*
* @return EKF Pcz.
*/
static inline float mavlink_msg_airspeed_autocal_get_Pcz(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 44);
}
/**
* @brief Decode a airspeed_autocal message into a struct
*
* @param msg The message to decode
* @param airspeed_autocal C-struct to decode the message contents into
*/
static inline void mavlink_msg_airspeed_autocal_decode(const mavlink_message_t* msg, mavlink_airspeed_autocal_t* airspeed_autocal)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
airspeed_autocal->vx = mavlink_msg_airspeed_autocal_get_vx(msg);
airspeed_autocal->vy = mavlink_msg_airspeed_autocal_get_vy(msg);
airspeed_autocal->vz = mavlink_msg_airspeed_autocal_get_vz(msg);
airspeed_autocal->diff_pressure = mavlink_msg_airspeed_autocal_get_diff_pressure(msg);
airspeed_autocal->EAS2TAS = mavlink_msg_airspeed_autocal_get_EAS2TAS(msg);
airspeed_autocal->ratio = mavlink_msg_airspeed_autocal_get_ratio(msg);
airspeed_autocal->state_x = mavlink_msg_airspeed_autocal_get_state_x(msg);
airspeed_autocal->state_y = mavlink_msg_airspeed_autocal_get_state_y(msg);
airspeed_autocal->state_z = mavlink_msg_airspeed_autocal_get_state_z(msg);
airspeed_autocal->Pax = mavlink_msg_airspeed_autocal_get_Pax(msg);
airspeed_autocal->Pby = mavlink_msg_airspeed_autocal_get_Pby(msg);
airspeed_autocal->Pcz = mavlink_msg_airspeed_autocal_get_Pcz(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN? msg->len : MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN;
memset(airspeed_autocal, 0, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
memcpy(airspeed_autocal, _MAV_PAYLOAD(msg), len);
#endif
}
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