373 lines
14 KiB
C
373 lines
14 KiB
C
#pragma once
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// MESSAGE AIRSPEED PACKING
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#define MAVLINK_MSG_ID_AIRSPEED 295
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typedef struct __mavlink_airspeed_t {
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float airspeed; /*< [m/s] Calibrated airspeed (CAS).*/
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float raw_press; /*< [hPa] Raw differential pressure. NaN for value unknown/not supplied.*/
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int16_t temperature; /*< [cdegC] Temperature. INT16_MAX for value unknown/not supplied.*/
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uint8_t id; /*< Sensor ID.*/
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uint8_t flags; /*< Airspeed sensor flags.*/
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} mavlink_airspeed_t;
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#define MAVLINK_MSG_ID_AIRSPEED_LEN 12
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#define MAVLINK_MSG_ID_AIRSPEED_MIN_LEN 12
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#define MAVLINK_MSG_ID_295_LEN 12
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#define MAVLINK_MSG_ID_295_MIN_LEN 12
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#define MAVLINK_MSG_ID_AIRSPEED_CRC 234
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#define MAVLINK_MSG_ID_295_CRC 234
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#if MAVLINK_COMMAND_24BIT
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#define MAVLINK_MESSAGE_INFO_AIRSPEED { \
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295, \
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"AIRSPEED", \
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5, \
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{ { "id", NULL, MAVLINK_TYPE_UINT8_T, 0, 10, offsetof(mavlink_airspeed_t, id) }, \
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{ "airspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_t, airspeed) }, \
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{ "temperature", NULL, MAVLINK_TYPE_INT16_T, 0, 8, offsetof(mavlink_airspeed_t, temperature) }, \
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{ "raw_press", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_t, raw_press) }, \
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{ "flags", NULL, MAVLINK_TYPE_UINT8_T, 0, 11, offsetof(mavlink_airspeed_t, flags) }, \
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} \
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}
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#else
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#define MAVLINK_MESSAGE_INFO_AIRSPEED { \
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"AIRSPEED", \
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5, \
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{ { "id", NULL, MAVLINK_TYPE_UINT8_T, 0, 10, offsetof(mavlink_airspeed_t, id) }, \
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{ "airspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_t, airspeed) }, \
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{ "temperature", NULL, MAVLINK_TYPE_INT16_T, 0, 8, offsetof(mavlink_airspeed_t, temperature) }, \
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{ "raw_press", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_t, raw_press) }, \
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{ "flags", NULL, MAVLINK_TYPE_UINT8_T, 0, 11, offsetof(mavlink_airspeed_t, flags) }, \
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} \
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}
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#endif
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/**
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* @brief Pack a airspeed message
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param msg The MAVLink message to compress the data into
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*
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* @param id Sensor ID.
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* @param airspeed [m/s] Calibrated airspeed (CAS).
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* @param temperature [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
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* @param raw_press [hPa] Raw differential pressure. NaN for value unknown/not supplied.
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* @param flags Airspeed sensor flags.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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static inline uint16_t mavlink_msg_airspeed_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
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uint8_t id, float airspeed, int16_t temperature, float raw_press, uint8_t flags)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_AIRSPEED_LEN];
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_mav_put_float(buf, 0, airspeed);
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_mav_put_float(buf, 4, raw_press);
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_mav_put_int16_t(buf, 8, temperature);
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_mav_put_uint8_t(buf, 10, id);
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_mav_put_uint8_t(buf, 11, flags);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_LEN);
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#else
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mavlink_airspeed_t packet;
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packet.airspeed = airspeed;
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packet.raw_press = raw_press;
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packet.temperature = temperature;
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packet.id = id;
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packet.flags = flags;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_AIRSPEED;
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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);
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}
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/**
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* @brief Pack a airspeed message
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param status MAVLink status structure
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* @param msg The MAVLink message to compress the data into
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*
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* @param id Sensor ID.
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* @param airspeed [m/s] Calibrated airspeed (CAS).
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* @param temperature [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
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* @param raw_press [hPa] Raw differential pressure. NaN for value unknown/not supplied.
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* @param flags Airspeed sensor flags.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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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,
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uint8_t id, float airspeed, int16_t temperature, float raw_press, uint8_t flags)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_AIRSPEED_LEN];
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_mav_put_float(buf, 0, airspeed);
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_mav_put_float(buf, 4, raw_press);
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_mav_put_int16_t(buf, 8, temperature);
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_mav_put_uint8_t(buf, 10, id);
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_mav_put_uint8_t(buf, 11, flags);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_LEN);
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#else
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mavlink_airspeed_t packet;
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packet.airspeed = airspeed;
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packet.raw_press = raw_press;
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packet.temperature = temperature;
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packet.id = id;
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packet.flags = flags;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_AIRSPEED;
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#if MAVLINK_CRC_EXTRA
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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);
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#else
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return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_AIRSPEED_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_LEN);
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#endif
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}
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/**
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* @brief Pack a airspeed message on a channel
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param chan The MAVLink channel this message will be sent over
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* @param msg The MAVLink message to compress the data into
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* @param id Sensor ID.
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* @param airspeed [m/s] Calibrated airspeed (CAS).
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* @param temperature [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
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* @param raw_press [hPa] Raw differential pressure. NaN for value unknown/not supplied.
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* @param flags Airspeed sensor flags.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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static inline uint16_t mavlink_msg_airspeed_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
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mavlink_message_t* msg,
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uint8_t id,float airspeed,int16_t temperature,float raw_press,uint8_t flags)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_AIRSPEED_LEN];
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_mav_put_float(buf, 0, airspeed);
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_mav_put_float(buf, 4, raw_press);
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_mav_put_int16_t(buf, 8, temperature);
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_mav_put_uint8_t(buf, 10, id);
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_mav_put_uint8_t(buf, 11, flags);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_LEN);
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#else
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mavlink_airspeed_t packet;
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packet.airspeed = airspeed;
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packet.raw_press = raw_press;
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packet.temperature = temperature;
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packet.id = id;
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packet.flags = flags;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_AIRSPEED;
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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);
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}
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/**
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* @brief Encode a airspeed struct
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*
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param msg The MAVLink message to compress the data into
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* @param airspeed C-struct to read the message contents from
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*/
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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)
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{
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return mavlink_msg_airspeed_pack(system_id, component_id, msg, airspeed->id, airspeed->airspeed, airspeed->temperature, airspeed->raw_press, airspeed->flags);
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}
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/**
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* @brief Encode a airspeed struct on a channel
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*
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param chan The MAVLink channel this message will be sent over
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* @param msg The MAVLink message to compress the data into
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* @param airspeed C-struct to read the message contents from
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*/
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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)
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{
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return mavlink_msg_airspeed_pack_chan(system_id, component_id, chan, msg, airspeed->id, airspeed->airspeed, airspeed->temperature, airspeed->raw_press, airspeed->flags);
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}
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/**
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* @brief Encode a airspeed struct with provided status structure
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*
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param status MAVLink status structure
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* @param msg The MAVLink message to compress the data into
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* @param airspeed C-struct to read the message contents from
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*/
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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)
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{
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return mavlink_msg_airspeed_pack_status(system_id, component_id, _status, msg, airspeed->id, airspeed->airspeed, airspeed->temperature, airspeed->raw_press, airspeed->flags);
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}
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/**
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* @brief Send a airspeed message
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* @param chan MAVLink channel to send the message
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*
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* @param id Sensor ID.
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* @param airspeed [m/s] Calibrated airspeed (CAS).
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* @param temperature [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
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* @param raw_press [hPa] Raw differential pressure. NaN for value unknown/not supplied.
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* @param flags Airspeed sensor flags.
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*/
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#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
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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)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_AIRSPEED_LEN];
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_mav_put_float(buf, 0, airspeed);
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_mav_put_float(buf, 4, raw_press);
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_mav_put_int16_t(buf, 8, temperature);
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_mav_put_uint8_t(buf, 10, id);
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_mav_put_uint8_t(buf, 11, flags);
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_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);
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#else
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mavlink_airspeed_t packet;
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packet.airspeed = airspeed;
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packet.raw_press = raw_press;
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packet.temperature = temperature;
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packet.id = id;
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packet.flags = flags;
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_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);
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#endif
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}
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/**
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* @brief Send a airspeed message
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* @param chan MAVLink channel to send the message
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* @param struct The MAVLink struct to serialize
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*/
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static inline void mavlink_msg_airspeed_send_struct(mavlink_channel_t chan, const mavlink_airspeed_t* airspeed)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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mavlink_msg_airspeed_send(chan, airspeed->id, airspeed->airspeed, airspeed->temperature, airspeed->raw_press, airspeed->flags);
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#else
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_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);
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#endif
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}
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#if MAVLINK_MSG_ID_AIRSPEED_LEN <= MAVLINK_MAX_PAYLOAD_LEN
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/*
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This variant of _send() can be used to save stack space by re-using
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memory from the receive buffer. The caller provides a
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mavlink_message_t which is the size of a full mavlink message. This
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is usually the receive buffer for the channel, and allows a reply to an
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incoming message with minimum stack space usage.
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*/
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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)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char *buf = (char *)msgbuf;
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_mav_put_float(buf, 0, airspeed);
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_mav_put_float(buf, 4, raw_press);
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_mav_put_int16_t(buf, 8, temperature);
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_mav_put_uint8_t(buf, 10, id);
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_mav_put_uint8_t(buf, 11, flags);
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_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);
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#else
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mavlink_airspeed_t *packet = (mavlink_airspeed_t *)msgbuf;
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packet->airspeed = airspeed;
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packet->raw_press = raw_press;
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packet->temperature = temperature;
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packet->id = id;
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packet->flags = flags;
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_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);
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#endif
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}
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#endif
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#endif
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// MESSAGE AIRSPEED UNPACKING
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/**
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* @brief Get field id from airspeed message
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*
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* @return Sensor ID.
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*/
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static inline uint8_t mavlink_msg_airspeed_get_id(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_uint8_t(msg, 10);
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}
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/**
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* @brief Get field airspeed from airspeed message
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*
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* @return [m/s] Calibrated airspeed (CAS).
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*/
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static inline float mavlink_msg_airspeed_get_airspeed(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_float(msg, 0);
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}
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/**
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* @brief Get field temperature from airspeed message
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*
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* @return [cdegC] Temperature. INT16_MAX for value unknown/not supplied.
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*/
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static inline int16_t mavlink_msg_airspeed_get_temperature(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_int16_t(msg, 8);
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}
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/**
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* @brief Get field raw_press from airspeed message
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*
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* @return [hPa] Raw differential pressure. NaN for value unknown/not supplied.
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*/
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static inline float mavlink_msg_airspeed_get_raw_press(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_float(msg, 4);
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}
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/**
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* @brief Get field flags from airspeed message
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*
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* @return Airspeed sensor flags.
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*/
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static inline uint8_t mavlink_msg_airspeed_get_flags(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_uint8_t(msg, 11);
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}
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/**
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* @brief Decode a airspeed message into a struct
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*
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* @param msg The message to decode
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* @param airspeed C-struct to decode the message contents into
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*/
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static inline void mavlink_msg_airspeed_decode(const mavlink_message_t* msg, mavlink_airspeed_t* airspeed)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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airspeed->airspeed = mavlink_msg_airspeed_get_airspeed(msg);
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airspeed->raw_press = mavlink_msg_airspeed_get_raw_press(msg);
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airspeed->temperature = mavlink_msg_airspeed_get_temperature(msg);
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airspeed->id = mavlink_msg_airspeed_get_id(msg);
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airspeed->flags = mavlink_msg_airspeed_get_flags(msg);
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#else
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uint8_t len = msg->len < MAVLINK_MSG_ID_AIRSPEED_LEN? msg->len : MAVLINK_MSG_ID_AIRSPEED_LEN;
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memset(airspeed, 0, MAVLINK_MSG_ID_AIRSPEED_LEN);
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memcpy(airspeed, _MAV_PAYLOAD(msg), len);
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#endif
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}
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