429 lines
18 KiB
C
429 lines
18 KiB
C
#pragma once
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// MESSAGE AIRSPEEDS PACKING
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#define MAVLINK_MSG_ID_AIRSPEEDS 182
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typedef struct __mavlink_airspeeds_t {
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uint32_t time_boot_ms; /*< Timestamp (milliseconds since system boot)*/
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int16_t airspeed_imu; /*< Airspeed estimate from IMU, cm/s*/
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int16_t airspeed_pitot; /*< Pitot measured forward airpseed, cm/s*/
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int16_t airspeed_hot_wire; /*< Hot wire anenometer measured airspeed, cm/s*/
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int16_t airspeed_ultrasonic; /*< Ultrasonic measured airspeed, cm/s*/
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int16_t aoa; /*< Angle of attack sensor, degrees * 10*/
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int16_t aoy; /*< Yaw angle sensor, degrees * 10*/
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} mavlink_airspeeds_t;
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#define MAVLINK_MSG_ID_AIRSPEEDS_LEN 16
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#define MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN 16
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#define MAVLINK_MSG_ID_182_LEN 16
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#define MAVLINK_MSG_ID_182_MIN_LEN 16
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#define MAVLINK_MSG_ID_AIRSPEEDS_CRC 154
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#define MAVLINK_MSG_ID_182_CRC 154
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#if MAVLINK_COMMAND_24BIT
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#define MAVLINK_MESSAGE_INFO_AIRSPEEDS { \
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182, \
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"AIRSPEEDS", \
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7, \
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{ { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_airspeeds_t, time_boot_ms) }, \
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{ "airspeed_imu", NULL, MAVLINK_TYPE_INT16_T, 0, 4, offsetof(mavlink_airspeeds_t, airspeed_imu) }, \
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{ "airspeed_pitot", NULL, MAVLINK_TYPE_INT16_T, 0, 6, offsetof(mavlink_airspeeds_t, airspeed_pitot) }, \
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{ "airspeed_hot_wire", NULL, MAVLINK_TYPE_INT16_T, 0, 8, offsetof(mavlink_airspeeds_t, airspeed_hot_wire) }, \
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{ "airspeed_ultrasonic", NULL, MAVLINK_TYPE_INT16_T, 0, 10, offsetof(mavlink_airspeeds_t, airspeed_ultrasonic) }, \
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{ "aoa", NULL, MAVLINK_TYPE_INT16_T, 0, 12, offsetof(mavlink_airspeeds_t, aoa) }, \
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{ "aoy", NULL, MAVLINK_TYPE_INT16_T, 0, 14, offsetof(mavlink_airspeeds_t, aoy) }, \
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} \
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}
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#else
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#define MAVLINK_MESSAGE_INFO_AIRSPEEDS { \
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"AIRSPEEDS", \
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7, \
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{ { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_airspeeds_t, time_boot_ms) }, \
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{ "airspeed_imu", NULL, MAVLINK_TYPE_INT16_T, 0, 4, offsetof(mavlink_airspeeds_t, airspeed_imu) }, \
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{ "airspeed_pitot", NULL, MAVLINK_TYPE_INT16_T, 0, 6, offsetof(mavlink_airspeeds_t, airspeed_pitot) }, \
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{ "airspeed_hot_wire", NULL, MAVLINK_TYPE_INT16_T, 0, 8, offsetof(mavlink_airspeeds_t, airspeed_hot_wire) }, \
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{ "airspeed_ultrasonic", NULL, MAVLINK_TYPE_INT16_T, 0, 10, offsetof(mavlink_airspeeds_t, airspeed_ultrasonic) }, \
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{ "aoa", NULL, MAVLINK_TYPE_INT16_T, 0, 12, offsetof(mavlink_airspeeds_t, aoa) }, \
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{ "aoy", NULL, MAVLINK_TYPE_INT16_T, 0, 14, offsetof(mavlink_airspeeds_t, aoy) }, \
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} \
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}
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#endif
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/**
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* @brief Pack a airspeeds 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 time_boot_ms Timestamp (milliseconds since system boot)
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* @param airspeed_imu Airspeed estimate from IMU, cm/s
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* @param airspeed_pitot Pitot measured forward airpseed, cm/s
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* @param airspeed_hot_wire Hot wire anenometer measured airspeed, cm/s
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* @param airspeed_ultrasonic Ultrasonic measured airspeed, cm/s
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* @param aoa Angle of attack sensor, degrees * 10
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* @param aoy Yaw angle sensor, degrees * 10
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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_airspeeds_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
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uint32_t time_boot_ms, int16_t airspeed_imu, int16_t airspeed_pitot, int16_t airspeed_hot_wire, int16_t airspeed_ultrasonic, int16_t aoa, int16_t aoy)
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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_AIRSPEEDS_LEN];
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_mav_put_uint32_t(buf, 0, time_boot_ms);
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_mav_put_int16_t(buf, 4, airspeed_imu);
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_mav_put_int16_t(buf, 6, airspeed_pitot);
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_mav_put_int16_t(buf, 8, airspeed_hot_wire);
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_mav_put_int16_t(buf, 10, airspeed_ultrasonic);
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_mav_put_int16_t(buf, 12, aoa);
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_mav_put_int16_t(buf, 14, aoy);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEEDS_LEN);
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#else
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mavlink_airspeeds_t packet;
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packet.time_boot_ms = time_boot_ms;
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packet.airspeed_imu = airspeed_imu;
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packet.airspeed_pitot = airspeed_pitot;
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packet.airspeed_hot_wire = airspeed_hot_wire;
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packet.airspeed_ultrasonic = airspeed_ultrasonic;
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packet.aoa = aoa;
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packet.aoy = aoy;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEEDS_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_AIRSPEEDS;
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return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC);
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}
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/**
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* @brief Pack a airspeeds 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 time_boot_ms Timestamp (milliseconds since system boot)
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* @param airspeed_imu Airspeed estimate from IMU, cm/s
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* @param airspeed_pitot Pitot measured forward airpseed, cm/s
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* @param airspeed_hot_wire Hot wire anenometer measured airspeed, cm/s
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* @param airspeed_ultrasonic Ultrasonic measured airspeed, cm/s
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* @param aoa Angle of attack sensor, degrees * 10
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* @param aoy Yaw angle sensor, degrees * 10
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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_airspeeds_pack_status(uint8_t system_id, uint8_t component_id, mavlink_status_t *_status, mavlink_message_t* msg,
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uint32_t time_boot_ms, int16_t airspeed_imu, int16_t airspeed_pitot, int16_t airspeed_hot_wire, int16_t airspeed_ultrasonic, int16_t aoa, int16_t aoy)
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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_AIRSPEEDS_LEN];
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_mav_put_uint32_t(buf, 0, time_boot_ms);
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_mav_put_int16_t(buf, 4, airspeed_imu);
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_mav_put_int16_t(buf, 6, airspeed_pitot);
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_mav_put_int16_t(buf, 8, airspeed_hot_wire);
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_mav_put_int16_t(buf, 10, airspeed_ultrasonic);
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_mav_put_int16_t(buf, 12, aoa);
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_mav_put_int16_t(buf, 14, aoy);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEEDS_LEN);
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#else
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mavlink_airspeeds_t packet;
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packet.time_boot_ms = time_boot_ms;
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packet.airspeed_imu = airspeed_imu;
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packet.airspeed_pitot = airspeed_pitot;
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packet.airspeed_hot_wire = airspeed_hot_wire;
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packet.airspeed_ultrasonic = airspeed_ultrasonic;
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packet.aoa = aoa;
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packet.aoy = aoy;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEEDS_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_AIRSPEEDS;
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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_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC);
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#else
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return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN);
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#endif
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}
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/**
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* @brief Pack a airspeeds 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 time_boot_ms Timestamp (milliseconds since system boot)
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* @param airspeed_imu Airspeed estimate from IMU, cm/s
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* @param airspeed_pitot Pitot measured forward airpseed, cm/s
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* @param airspeed_hot_wire Hot wire anenometer measured airspeed, cm/s
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* @param airspeed_ultrasonic Ultrasonic measured airspeed, cm/s
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* @param aoa Angle of attack sensor, degrees * 10
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* @param aoy Yaw angle sensor, degrees * 10
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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_airspeeds_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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uint32_t time_boot_ms,int16_t airspeed_imu,int16_t airspeed_pitot,int16_t airspeed_hot_wire,int16_t airspeed_ultrasonic,int16_t aoa,int16_t aoy)
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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_AIRSPEEDS_LEN];
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_mav_put_uint32_t(buf, 0, time_boot_ms);
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_mav_put_int16_t(buf, 4, airspeed_imu);
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_mav_put_int16_t(buf, 6, airspeed_pitot);
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_mav_put_int16_t(buf, 8, airspeed_hot_wire);
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_mav_put_int16_t(buf, 10, airspeed_ultrasonic);
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_mav_put_int16_t(buf, 12, aoa);
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_mav_put_int16_t(buf, 14, aoy);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEEDS_LEN);
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#else
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mavlink_airspeeds_t packet;
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packet.time_boot_ms = time_boot_ms;
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packet.airspeed_imu = airspeed_imu;
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packet.airspeed_pitot = airspeed_pitot;
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packet.airspeed_hot_wire = airspeed_hot_wire;
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packet.airspeed_ultrasonic = airspeed_ultrasonic;
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packet.aoa = aoa;
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packet.aoy = aoy;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEEDS_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_AIRSPEEDS;
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return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC);
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}
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/**
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* @brief Encode a airspeeds 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 airspeeds C-struct to read the message contents from
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*/
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static inline uint16_t mavlink_msg_airspeeds_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_airspeeds_t* airspeeds)
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{
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return mavlink_msg_airspeeds_pack(system_id, component_id, msg, airspeeds->time_boot_ms, airspeeds->airspeed_imu, airspeeds->airspeed_pitot, airspeeds->airspeed_hot_wire, airspeeds->airspeed_ultrasonic, airspeeds->aoa, airspeeds->aoy);
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}
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/**
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* @brief Encode a airspeeds 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 airspeeds C-struct to read the message contents from
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*/
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static inline uint16_t mavlink_msg_airspeeds_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_airspeeds_t* airspeeds)
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{
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return mavlink_msg_airspeeds_pack_chan(system_id, component_id, chan, msg, airspeeds->time_boot_ms, airspeeds->airspeed_imu, airspeeds->airspeed_pitot, airspeeds->airspeed_hot_wire, airspeeds->airspeed_ultrasonic, airspeeds->aoa, airspeeds->aoy);
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}
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/**
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* @brief Encode a airspeeds 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 airspeeds C-struct to read the message contents from
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*/
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static inline uint16_t mavlink_msg_airspeeds_encode_status(uint8_t system_id, uint8_t component_id, mavlink_status_t* _status, mavlink_message_t* msg, const mavlink_airspeeds_t* airspeeds)
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{
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return mavlink_msg_airspeeds_pack_status(system_id, component_id, _status, msg, airspeeds->time_boot_ms, airspeeds->airspeed_imu, airspeeds->airspeed_pitot, airspeeds->airspeed_hot_wire, airspeeds->airspeed_ultrasonic, airspeeds->aoa, airspeeds->aoy);
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}
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/**
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* @brief Send a airspeeds message
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* @param chan MAVLink channel to send the message
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*
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* @param time_boot_ms Timestamp (milliseconds since system boot)
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* @param airspeed_imu Airspeed estimate from IMU, cm/s
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* @param airspeed_pitot Pitot measured forward airpseed, cm/s
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* @param airspeed_hot_wire Hot wire anenometer measured airspeed, cm/s
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* @param airspeed_ultrasonic Ultrasonic measured airspeed, cm/s
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* @param aoa Angle of attack sensor, degrees * 10
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* @param aoy Yaw angle sensor, degrees * 10
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*/
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#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
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static inline void mavlink_msg_airspeeds_send(mavlink_channel_t chan, uint32_t time_boot_ms, int16_t airspeed_imu, int16_t airspeed_pitot, int16_t airspeed_hot_wire, int16_t airspeed_ultrasonic, int16_t aoa, int16_t aoy)
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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_AIRSPEEDS_LEN];
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_mav_put_uint32_t(buf, 0, time_boot_ms);
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_mav_put_int16_t(buf, 4, airspeed_imu);
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_mav_put_int16_t(buf, 6, airspeed_pitot);
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_mav_put_int16_t(buf, 8, airspeed_hot_wire);
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_mav_put_int16_t(buf, 10, airspeed_ultrasonic);
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_mav_put_int16_t(buf, 12, aoa);
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_mav_put_int16_t(buf, 14, aoy);
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, buf, MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC);
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#else
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mavlink_airspeeds_t packet;
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packet.time_boot_ms = time_boot_ms;
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packet.airspeed_imu = airspeed_imu;
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packet.airspeed_pitot = airspeed_pitot;
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packet.airspeed_hot_wire = airspeed_hot_wire;
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packet.airspeed_ultrasonic = airspeed_ultrasonic;
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packet.aoa = aoa;
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packet.aoy = aoy;
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, (const char *)&packet, MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC);
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#endif
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}
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/**
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* @brief Send a airspeeds 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_airspeeds_send_struct(mavlink_channel_t chan, const mavlink_airspeeds_t* airspeeds)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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mavlink_msg_airspeeds_send(chan, airspeeds->time_boot_ms, airspeeds->airspeed_imu, airspeeds->airspeed_pitot, airspeeds->airspeed_hot_wire, airspeeds->airspeed_ultrasonic, airspeeds->aoa, airspeeds->aoy);
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#else
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, (const char *)airspeeds, MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC);
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#endif
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}
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#if MAVLINK_MSG_ID_AIRSPEEDS_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_airspeeds_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, int16_t airspeed_imu, int16_t airspeed_pitot, int16_t airspeed_hot_wire, int16_t airspeed_ultrasonic, int16_t aoa, int16_t aoy)
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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_uint32_t(buf, 0, time_boot_ms);
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_mav_put_int16_t(buf, 4, airspeed_imu);
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_mav_put_int16_t(buf, 6, airspeed_pitot);
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_mav_put_int16_t(buf, 8, airspeed_hot_wire);
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_mav_put_int16_t(buf, 10, airspeed_ultrasonic);
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_mav_put_int16_t(buf, 12, aoa);
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_mav_put_int16_t(buf, 14, aoy);
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, buf, MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC);
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#else
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mavlink_airspeeds_t *packet = (mavlink_airspeeds_t *)msgbuf;
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|
packet->time_boot_ms = time_boot_ms;
|
|
packet->airspeed_imu = airspeed_imu;
|
|
packet->airspeed_pitot = airspeed_pitot;
|
|
packet->airspeed_hot_wire = airspeed_hot_wire;
|
|
packet->airspeed_ultrasonic = airspeed_ultrasonic;
|
|
packet->aoa = aoa;
|
|
packet->aoy = aoy;
|
|
|
|
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, (const char *)packet, MAVLINK_MSG_ID_AIRSPEEDS_MIN_LEN, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC);
|
|
#endif
|
|
}
|
|
#endif
|
|
|
|
#endif
|
|
|
|
// MESSAGE AIRSPEEDS UNPACKING
|
|
|
|
|
|
/**
|
|
* @brief Get field time_boot_ms from airspeeds message
|
|
*
|
|
* @return Timestamp (milliseconds since system boot)
|
|
*/
|
|
static inline uint32_t mavlink_msg_airspeeds_get_time_boot_ms(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint32_t(msg, 0);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field airspeed_imu from airspeeds message
|
|
*
|
|
* @return Airspeed estimate from IMU, cm/s
|
|
*/
|
|
static inline int16_t mavlink_msg_airspeeds_get_airspeed_imu(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int16_t(msg, 4);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field airspeed_pitot from airspeeds message
|
|
*
|
|
* @return Pitot measured forward airpseed, cm/s
|
|
*/
|
|
static inline int16_t mavlink_msg_airspeeds_get_airspeed_pitot(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int16_t(msg, 6);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field airspeed_hot_wire from airspeeds message
|
|
*
|
|
* @return Hot wire anenometer measured airspeed, cm/s
|
|
*/
|
|
static inline int16_t mavlink_msg_airspeeds_get_airspeed_hot_wire(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int16_t(msg, 8);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field airspeed_ultrasonic from airspeeds message
|
|
*
|
|
* @return Ultrasonic measured airspeed, cm/s
|
|
*/
|
|
static inline int16_t mavlink_msg_airspeeds_get_airspeed_ultrasonic(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int16_t(msg, 10);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field aoa from airspeeds message
|
|
*
|
|
* @return Angle of attack sensor, degrees * 10
|
|
*/
|
|
static inline int16_t mavlink_msg_airspeeds_get_aoa(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int16_t(msg, 12);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field aoy from airspeeds message
|
|
*
|
|
* @return Yaw angle sensor, degrees * 10
|
|
*/
|
|
static inline int16_t mavlink_msg_airspeeds_get_aoy(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int16_t(msg, 14);
|
|
}
|
|
|
|
/**
|
|
* @brief Decode a airspeeds message into a struct
|
|
*
|
|
* @param msg The message to decode
|
|
* @param airspeeds C-struct to decode the message contents into
|
|
*/
|
|
static inline void mavlink_msg_airspeeds_decode(const mavlink_message_t* msg, mavlink_airspeeds_t* airspeeds)
|
|
{
|
|
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
|
airspeeds->time_boot_ms = mavlink_msg_airspeeds_get_time_boot_ms(msg);
|
|
airspeeds->airspeed_imu = mavlink_msg_airspeeds_get_airspeed_imu(msg);
|
|
airspeeds->airspeed_pitot = mavlink_msg_airspeeds_get_airspeed_pitot(msg);
|
|
airspeeds->airspeed_hot_wire = mavlink_msg_airspeeds_get_airspeed_hot_wire(msg);
|
|
airspeeds->airspeed_ultrasonic = mavlink_msg_airspeeds_get_airspeed_ultrasonic(msg);
|
|
airspeeds->aoa = mavlink_msg_airspeeds_get_aoa(msg);
|
|
airspeeds->aoy = mavlink_msg_airspeeds_get_aoy(msg);
|
|
#else
|
|
uint8_t len = msg->len < MAVLINK_MSG_ID_AIRSPEEDS_LEN? msg->len : MAVLINK_MSG_ID_AIRSPEEDS_LEN;
|
|
memset(airspeeds, 0, MAVLINK_MSG_ID_AIRSPEEDS_LEN);
|
|
memcpy(airspeeds, _MAV_PAYLOAD(msg), len);
|
|
#endif
|
|
}
|