data/method/mavlink/c_library_v2-master/development/mavlink_msg_airspeed.h

373 lines
14 KiB
C

#pragma once
// MESSAGE AIRSPEED PACKING
#define MAVLINK_MSG_ID_AIRSPEED 295
typedef struct __mavlink_airspeed_t {
float airspeed; /*< [m/s] Calibrated airspeed (CAS).*/
float raw_press; /*< [hPa] Raw differential pressure. NaN for value unknown/not supplied.*/
int16_t temperature; /*< [cdegC] Temperature. INT16_MAX for value unknown/not supplied.*/
uint8_t id; /*< Sensor ID.*/
uint8_t flags; /*< Airspeed sensor flags.*/
} mavlink_airspeed_t;
#define MAVLINK_MSG_ID_AIRSPEED_LEN 12
#define MAVLINK_MSG_ID_AIRSPEED_MIN_LEN 12
#define MAVLINK_MSG_ID_295_LEN 12
#define MAVLINK_MSG_ID_295_MIN_LEN 12
#define MAVLINK_MSG_ID_AIRSPEED_CRC 234
#define MAVLINK_MSG_ID_295_CRC 234
#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_AIRSPEED { \
295, \
"AIRSPEED", \
5, \
{ { "id", NULL, MAVLINK_TYPE_UINT8_T, 0, 10, offsetof(mavlink_airspeed_t, id) }, \
{ "airspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_t, airspeed) }, \
{ "temperature", NULL, MAVLINK_TYPE_INT16_T, 0, 8, offsetof(mavlink_airspeed_t, temperature) }, \
{ "raw_press", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_t, raw_press) }, \
{ "flags", NULL, MAVLINK_TYPE_UINT8_T, 0, 11, offsetof(mavlink_airspeed_t, flags) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_AIRSPEED { \
"AIRSPEED", \
5, \
{ { "id", NULL, MAVLINK_TYPE_UINT8_T, 0, 10, offsetof(mavlink_airspeed_t, id) }, \
{ "airspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_t, airspeed) }, \
{ "temperature", NULL, MAVLINK_TYPE_INT16_T, 0, 8, offsetof(mavlink_airspeed_t, temperature) }, \
{ "raw_press", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_t, raw_press) }, \
{ "flags", NULL, MAVLINK_TYPE_UINT8_T, 0, 11, offsetof(mavlink_airspeed_t, flags) }, \
} \
}
#endif
/**
* @brief Pack a airspeed 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 id Sensor ID.
* @param airspeed [m/s] Calibrated airspeed (CAS).
* @param temperature [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
* @param raw_press [hPa] Raw differential pressure. NaN for value unknown/not supplied.
* @param flags Airspeed sensor flags.
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_airspeed_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint8_t id, float airspeed, int16_t temperature, float raw_press, uint8_t flags)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_AIRSPEED_LEN];
_mav_put_float(buf, 0, airspeed);
_mav_put_float(buf, 4, raw_press);
_mav_put_int16_t(buf, 8, temperature);
_mav_put_uint8_t(buf, 10, id);
_mav_put_uint8_t(buf, 11, flags);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_LEN);
#else
mavlink_airspeed_t packet;
packet.airspeed = airspeed;
packet.raw_press = raw_press;
packet.temperature = temperature;
packet.id = id;
packet.flags = flags;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_AIRSPEED;
return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN, MAVLINK_MSG_ID_AIRSPEED_CRC);
}
/**
* @brief Pack a airspeed 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 id Sensor ID.
* @param airspeed [m/s] Calibrated airspeed (CAS).
* @param temperature [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
* @param raw_press [hPa] Raw differential pressure. NaN for value unknown/not supplied.
* @param flags Airspeed sensor flags.
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_airspeed_pack_status(uint8_t system_id, uint8_t component_id, mavlink_status_t *_status, mavlink_message_t* msg,
uint8_t id, float airspeed, int16_t temperature, float raw_press, uint8_t flags)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_AIRSPEED_LEN];
_mav_put_float(buf, 0, airspeed);
_mav_put_float(buf, 4, raw_press);
_mav_put_int16_t(buf, 8, temperature);
_mav_put_uint8_t(buf, 10, id);
_mav_put_uint8_t(buf, 11, flags);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_LEN);
#else
mavlink_airspeed_t packet;
packet.airspeed = airspeed;
packet.raw_press = raw_press;
packet.temperature = temperature;
packet.id = id;
packet.flags = flags;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_AIRSPEED;
#if MAVLINK_CRC_EXTRA
return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN, MAVLINK_MSG_ID_AIRSPEED_CRC);
#else
return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN);
#endif
}
/**
* @brief Pack a airspeed 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 id Sensor ID.
* @param airspeed [m/s] Calibrated airspeed (CAS).
* @param temperature [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
* @param raw_press [hPa] Raw differential pressure. NaN for value unknown/not supplied.
* @param flags Airspeed sensor flags.
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_airspeed_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint8_t id,float airspeed,int16_t temperature,float raw_press,uint8_t flags)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_AIRSPEED_LEN];
_mav_put_float(buf, 0, airspeed);
_mav_put_float(buf, 4, raw_press);
_mav_put_int16_t(buf, 8, temperature);
_mav_put_uint8_t(buf, 10, id);
_mav_put_uint8_t(buf, 11, flags);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_LEN);
#else
mavlink_airspeed_t packet;
packet.airspeed = airspeed;
packet.raw_press = raw_press;
packet.temperature = temperature;
packet.id = id;
packet.flags = flags;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_AIRSPEED;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN, MAVLINK_MSG_ID_AIRSPEED_CRC);
}
/**
* @brief Encode a airspeed 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 C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_airspeed_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_airspeed_t* airspeed)
{
return mavlink_msg_airspeed_pack(system_id, component_id, msg, airspeed->id, airspeed->airspeed, airspeed->temperature, airspeed->raw_press, airspeed->flags);
}
/**
* @brief Encode a airspeed 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 C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_airspeed_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_airspeed_t* airspeed)
{
return mavlink_msg_airspeed_pack_chan(system_id, component_id, chan, msg, airspeed->id, airspeed->airspeed, airspeed->temperature, airspeed->raw_press, airspeed->flags);
}
/**
* @brief Encode a airspeed 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 airspeed C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_airspeed_encode_status(uint8_t system_id, uint8_t component_id, mavlink_status_t* _status, mavlink_message_t* msg, const mavlink_airspeed_t* airspeed)
{
return mavlink_msg_airspeed_pack_status(system_id, component_id, _status, msg, airspeed->id, airspeed->airspeed, airspeed->temperature, airspeed->raw_press, airspeed->flags);
}
/**
* @brief Send a airspeed message
* @param chan MAVLink channel to send the message
*
* @param id Sensor ID.
* @param airspeed [m/s] Calibrated airspeed (CAS).
* @param temperature [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
* @param raw_press [hPa] Raw differential pressure. NaN for value unknown/not supplied.
* @param flags Airspeed sensor flags.
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_airspeed_send(mavlink_channel_t chan, uint8_t id, float airspeed, int16_t temperature, float raw_press, uint8_t flags)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_AIRSPEED_LEN];
_mav_put_float(buf, 0, airspeed);
_mav_put_float(buf, 4, raw_press);
_mav_put_int16_t(buf, 8, temperature);
_mav_put_uint8_t(buf, 10, id);
_mav_put_uint8_t(buf, 11, flags);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED, buf, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN, MAVLINK_MSG_ID_AIRSPEED_CRC);
#else
mavlink_airspeed_t packet;
packet.airspeed = airspeed;
packet.raw_press = raw_press;
packet.temperature = temperature;
packet.id = id;
packet.flags = flags;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED, (const char *)&packet, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN, MAVLINK_MSG_ID_AIRSPEED_CRC);
#endif
}
/**
* @brief Send a airspeed message
* @param chan MAVLink channel to send the message
* @param struct The MAVLink struct to serialize
*/
static inline void mavlink_msg_airspeed_send_struct(mavlink_channel_t chan, const mavlink_airspeed_t* airspeed)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_airspeed_send(chan, airspeed->id, airspeed->airspeed, airspeed->temperature, airspeed->raw_press, airspeed->flags);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED, (const char *)airspeed, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN, MAVLINK_MSG_ID_AIRSPEED_CRC);
#endif
}
#if MAVLINK_MSG_ID_AIRSPEED_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_airspeed_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t id, float airspeed, int16_t temperature, float raw_press, uint8_t flags)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_float(buf, 0, airspeed);
_mav_put_float(buf, 4, raw_press);
_mav_put_int16_t(buf, 8, temperature);
_mav_put_uint8_t(buf, 10, id);
_mav_put_uint8_t(buf, 11, flags);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED, buf, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN, MAVLINK_MSG_ID_AIRSPEED_CRC);
#else
mavlink_airspeed_t *packet = (mavlink_airspeed_t *)msgbuf;
packet->airspeed = airspeed;
packet->raw_press = raw_press;
packet->temperature = temperature;
packet->id = id;
packet->flags = flags;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED, (const char *)packet, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN, MAVLINK_MSG_ID_AIRSPEED_CRC);
#endif
}
#endif
#endif
// MESSAGE AIRSPEED UNPACKING
/**
* @brief Get field id from airspeed message
*
* @return Sensor ID.
*/
static inline uint8_t mavlink_msg_airspeed_get_id(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 10);
}
/**
* @brief Get field airspeed from airspeed message
*
* @return [m/s] Calibrated airspeed (CAS).
*/
static inline float mavlink_msg_airspeed_get_airspeed(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 0);
}
/**
* @brief Get field temperature from airspeed message
*
* @return [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
*/
static inline int16_t mavlink_msg_airspeed_get_temperature(const mavlink_message_t* msg)
{
return _MAV_RETURN_int16_t(msg, 8);
}
/**
* @brief Get field raw_press from airspeed message
*
* @return [hPa] Raw differential pressure. NaN for value unknown/not supplied.
*/
static inline float mavlink_msg_airspeed_get_raw_press(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 4);
}
/**
* @brief Get field flags from airspeed message
*
* @return Airspeed sensor flags.
*/
static inline uint8_t mavlink_msg_airspeed_get_flags(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 11);
}
/**
* @brief Decode a airspeed message into a struct
*
* @param msg The message to decode
* @param airspeed C-struct to decode the message contents into
*/
static inline void mavlink_msg_airspeed_decode(const mavlink_message_t* msg, mavlink_airspeed_t* airspeed)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
airspeed->airspeed = mavlink_msg_airspeed_get_airspeed(msg);
airspeed->raw_press = mavlink_msg_airspeed_get_raw_press(msg);
airspeed->temperature = mavlink_msg_airspeed_get_temperature(msg);
airspeed->id = mavlink_msg_airspeed_get_id(msg);
airspeed->flags = mavlink_msg_airspeed_get_flags(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_AIRSPEED_LEN? msg->len : MAVLINK_MSG_ID_AIRSPEED_LEN;
memset(airspeed, 0, MAVLINK_MSG_ID_AIRSPEED_LEN);
memcpy(airspeed, _MAV_PAYLOAD(msg), len);
#endif
}