1dff1bfd33
【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
489 lines
19 KiB
C
489 lines
19 KiB
C
#pragma once
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// MESSAGE AIRSPEED_AUTOCAL PACKING
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#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL 174
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MAVPACKED(
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typedef struct __mavlink_airspeed_autocal_t {
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float vx; /*< [m/s] GPS velocity north.*/
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float vy; /*< [m/s] GPS velocity east.*/
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float vz; /*< [m/s] GPS velocity down.*/
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float diff_pressure; /*< [Pa] Differential pressure.*/
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float EAS2TAS; /*< Estimated to true airspeed ratio.*/
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float ratio; /*< Airspeed ratio.*/
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float state_x; /*< EKF state x.*/
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float state_y; /*< EKF state y.*/
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float state_z; /*< EKF state z.*/
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float Pax; /*< EKF Pax.*/
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float Pby; /*< EKF Pby.*/
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float Pcz; /*< EKF Pcz.*/
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}) mavlink_airspeed_autocal_t;
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#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN 48
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#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN 48
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#define MAVLINK_MSG_ID_174_LEN 48
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#define MAVLINK_MSG_ID_174_MIN_LEN 48
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#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC 167
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#define MAVLINK_MSG_ID_174_CRC 167
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#if MAVLINK_COMMAND_24BIT
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#define MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL { \
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174, \
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"AIRSPEED_AUTOCAL", \
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12, \
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{ { "vx", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_autocal_t, vx) }, \
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{ "vy", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_autocal_t, vy) }, \
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{ "vz", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_airspeed_autocal_t, vz) }, \
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{ "diff_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_airspeed_autocal_t, diff_pressure) }, \
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{ "EAS2TAS", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_airspeed_autocal_t, EAS2TAS) }, \
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{ "ratio", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_airspeed_autocal_t, ratio) }, \
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{ "state_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_airspeed_autocal_t, state_x) }, \
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{ "state_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_airspeed_autocal_t, state_y) }, \
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{ "state_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_airspeed_autocal_t, state_z) }, \
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{ "Pax", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_airspeed_autocal_t, Pax) }, \
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{ "Pby", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_airspeed_autocal_t, Pby) }, \
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{ "Pcz", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_airspeed_autocal_t, Pcz) }, \
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} \
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}
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#else
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#define MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL { \
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"AIRSPEED_AUTOCAL", \
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12, \
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{ { "vx", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_autocal_t, vx) }, \
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{ "vy", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_autocal_t, vy) }, \
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{ "vz", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_airspeed_autocal_t, vz) }, \
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{ "diff_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_airspeed_autocal_t, diff_pressure) }, \
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{ "EAS2TAS", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_airspeed_autocal_t, EAS2TAS) }, \
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{ "ratio", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_airspeed_autocal_t, ratio) }, \
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{ "state_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_airspeed_autocal_t, state_x) }, \
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{ "state_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_airspeed_autocal_t, state_y) }, \
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{ "state_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_airspeed_autocal_t, state_z) }, \
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{ "Pax", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_airspeed_autocal_t, Pax) }, \
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{ "Pby", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_airspeed_autocal_t, Pby) }, \
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{ "Pcz", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_airspeed_autocal_t, Pcz) }, \
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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_autocal 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 vx [m/s] GPS velocity north.
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* @param vy [m/s] GPS velocity east.
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* @param vz [m/s] GPS velocity down.
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* @param diff_pressure [Pa] Differential pressure.
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* @param EAS2TAS Estimated to true airspeed ratio.
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* @param ratio Airspeed ratio.
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* @param state_x EKF state x.
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* @param state_y EKF state y.
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* @param state_z EKF state z.
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* @param Pax EKF Pax.
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* @param Pby EKF Pby.
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* @param Pcz EKF Pcz.
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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_autocal_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
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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)
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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_AUTOCAL_LEN];
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_mav_put_float(buf, 0, vx);
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_mav_put_float(buf, 4, vy);
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_mav_put_float(buf, 8, vz);
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_mav_put_float(buf, 12, diff_pressure);
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_mav_put_float(buf, 16, EAS2TAS);
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_mav_put_float(buf, 20, ratio);
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_mav_put_float(buf, 24, state_x);
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_mav_put_float(buf, 28, state_y);
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_mav_put_float(buf, 32, state_z);
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_mav_put_float(buf, 36, Pax);
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_mav_put_float(buf, 40, Pby);
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_mav_put_float(buf, 44, Pcz);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
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#else
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mavlink_airspeed_autocal_t packet;
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packet.vx = vx;
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packet.vy = vy;
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packet.vz = vz;
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packet.diff_pressure = diff_pressure;
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packet.EAS2TAS = EAS2TAS;
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packet.ratio = ratio;
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packet.state_x = state_x;
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packet.state_y = state_y;
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packet.state_z = state_z;
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packet.Pax = Pax;
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packet.Pby = Pby;
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packet.Pcz = Pcz;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_AIRSPEED_AUTOCAL;
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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);
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}
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/**
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* @brief Pack a airspeed_autocal 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 vx [m/s] GPS velocity north.
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* @param vy [m/s] GPS velocity east.
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* @param vz [m/s] GPS velocity down.
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* @param diff_pressure [Pa] Differential pressure.
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* @param EAS2TAS Estimated to true airspeed ratio.
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* @param ratio Airspeed ratio.
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* @param state_x EKF state x.
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* @param state_y EKF state y.
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* @param state_z EKF state z.
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* @param Pax EKF Pax.
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* @param Pby EKF Pby.
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* @param Pcz EKF Pcz.
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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_autocal_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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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)
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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_AUTOCAL_LEN];
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_mav_put_float(buf, 0, vx);
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_mav_put_float(buf, 4, vy);
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_mav_put_float(buf, 8, vz);
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_mav_put_float(buf, 12, diff_pressure);
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_mav_put_float(buf, 16, EAS2TAS);
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_mav_put_float(buf, 20, ratio);
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_mav_put_float(buf, 24, state_x);
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_mav_put_float(buf, 28, state_y);
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_mav_put_float(buf, 32, state_z);
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_mav_put_float(buf, 36, Pax);
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_mav_put_float(buf, 40, Pby);
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_mav_put_float(buf, 44, Pcz);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
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#else
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mavlink_airspeed_autocal_t packet;
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packet.vx = vx;
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packet.vy = vy;
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packet.vz = vz;
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packet.diff_pressure = diff_pressure;
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packet.EAS2TAS = EAS2TAS;
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packet.ratio = ratio;
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packet.state_x = state_x;
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packet.state_y = state_y;
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packet.state_z = state_z;
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packet.Pax = Pax;
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packet.Pby = Pby;
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packet.Pcz = Pcz;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_AIRSPEED_AUTOCAL;
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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);
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}
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/**
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* @brief Encode a airspeed_autocal 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_autocal C-struct to read the message contents from
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*/
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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)
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{
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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);
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}
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/**
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* @brief Encode a airspeed_autocal 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_autocal C-struct to read the message contents from
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*/
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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)
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{
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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);
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}
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/**
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* @brief Send a airspeed_autocal message
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* @param chan MAVLink channel to send the message
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*
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* @param vx [m/s] GPS velocity north.
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* @param vy [m/s] GPS velocity east.
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* @param vz [m/s] GPS velocity down.
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* @param diff_pressure [Pa] Differential pressure.
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* @param EAS2TAS Estimated to true airspeed ratio.
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* @param ratio Airspeed ratio.
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* @param state_x EKF state x.
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* @param state_y EKF state y.
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* @param state_z EKF state z.
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* @param Pax EKF Pax.
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* @param Pby EKF Pby.
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* @param Pcz EKF Pcz.
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*/
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#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
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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)
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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_AUTOCAL_LEN];
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_mav_put_float(buf, 0, vx);
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_mav_put_float(buf, 4, vy);
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_mav_put_float(buf, 8, vz);
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_mav_put_float(buf, 12, diff_pressure);
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_mav_put_float(buf, 16, EAS2TAS);
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_mav_put_float(buf, 20, ratio);
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_mav_put_float(buf, 24, state_x);
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_mav_put_float(buf, 28, state_y);
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_mav_put_float(buf, 32, state_z);
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_mav_put_float(buf, 36, Pax);
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_mav_put_float(buf, 40, Pby);
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_mav_put_float(buf, 44, Pcz);
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_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);
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#else
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mavlink_airspeed_autocal_t packet;
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packet.vx = vx;
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packet.vy = vy;
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packet.vz = vz;
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packet.diff_pressure = diff_pressure;
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packet.EAS2TAS = EAS2TAS;
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packet.ratio = ratio;
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packet.state_x = state_x;
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packet.state_y = state_y;
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packet.state_z = state_z;
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packet.Pax = Pax;
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packet.Pby = Pby;
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packet.Pcz = Pcz;
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_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);
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#endif
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}
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/**
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* @brief Send a airspeed_autocal 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_autocal_send_struct(mavlink_channel_t chan, const mavlink_airspeed_autocal_t* airspeed_autocal)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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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);
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#else
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_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);
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#endif
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}
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#if MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN <= MAVLINK_MAX_PAYLOAD_LEN
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/*
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This varient 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_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)
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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, vx);
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_mav_put_float(buf, 4, vy);
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_mav_put_float(buf, 8, vz);
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_mav_put_float(buf, 12, diff_pressure);
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_mav_put_float(buf, 16, EAS2TAS);
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_mav_put_float(buf, 20, ratio);
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_mav_put_float(buf, 24, state_x);
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_mav_put_float(buf, 28, state_y);
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_mav_put_float(buf, 32, state_z);
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_mav_put_float(buf, 36, Pax);
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_mav_put_float(buf, 40, Pby);
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_mav_put_float(buf, 44, Pcz);
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_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);
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#else
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mavlink_airspeed_autocal_t *packet = (mavlink_airspeed_autocal_t *)msgbuf;
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packet->vx = vx;
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packet->vy = vy;
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packet->vz = vz;
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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
|
|
}
|