#pragma once // MESSAGE AIRSPEED_AUTOCAL PACKING #define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL 174 MAVPACKED( typedef struct __mavlink_airspeed_autocal_t { float vx; /*< [m/s] GPS velocity north.*/ float vy; /*< [m/s] GPS velocity east.*/ float vz; /*< [m/s] GPS velocity down.*/ float diff_pressure; /*< [Pa] Differential pressure.*/ float EAS2TAS; /*< Estimated to true airspeed ratio.*/ float ratio; /*< Airspeed ratio.*/ float state_x; /*< EKF state x.*/ float state_y; /*< EKF state y.*/ float state_z; /*< EKF state z.*/ float Pax; /*< EKF Pax.*/ float Pby; /*< EKF Pby.*/ float Pcz; /*< EKF Pcz.*/ }) mavlink_airspeed_autocal_t; #define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN 48 #define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN 48 #define MAVLINK_MSG_ID_174_LEN 48 #define MAVLINK_MSG_ID_174_MIN_LEN 48 #define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC 167 #define MAVLINK_MSG_ID_174_CRC 167 #if MAVLINK_COMMAND_24BIT #define MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL { \ 174, \ "AIRSPEED_AUTOCAL", \ 12, \ { { "vx", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_autocal_t, vx) }, \ { "vy", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_autocal_t, vy) }, \ { "vz", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_airspeed_autocal_t, vz) }, \ { "diff_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_airspeed_autocal_t, diff_pressure) }, \ { "EAS2TAS", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_airspeed_autocal_t, EAS2TAS) }, \ { "ratio", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_airspeed_autocal_t, ratio) }, \ { "state_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_airspeed_autocal_t, state_x) }, \ { "state_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_airspeed_autocal_t, state_y) }, \ { "state_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_airspeed_autocal_t, state_z) }, \ { "Pax", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_airspeed_autocal_t, Pax) }, \ { "Pby", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_airspeed_autocal_t, Pby) }, \ { "Pcz", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_airspeed_autocal_t, Pcz) }, \ } \ } #else #define MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL { \ "AIRSPEED_AUTOCAL", \ 12, \ { { "vx", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_autocal_t, vx) }, \ { "vy", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_autocal_t, vy) }, \ { "vz", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_airspeed_autocal_t, vz) }, \ { "diff_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_airspeed_autocal_t, diff_pressure) }, \ { "EAS2TAS", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_airspeed_autocal_t, EAS2TAS) }, \ { "ratio", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_airspeed_autocal_t, ratio) }, \ { "state_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_airspeed_autocal_t, state_x) }, \ { "state_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_airspeed_autocal_t, state_y) }, \ { "state_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_airspeed_autocal_t, state_z) }, \ { "Pax", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_airspeed_autocal_t, Pax) }, \ { "Pby", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_airspeed_autocal_t, Pby) }, \ { "Pcz", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_airspeed_autocal_t, Pcz) }, \ } \ } #endif /** * @brief Pack a airspeed_autocal message * @param system_id ID of this system * @param component_id ID of this component (e.g. 200 for IMU) * @param msg The MAVLink message to compress the data into * * @param vx [m/s] GPS velocity north. * @param vy [m/s] GPS velocity east. * @param vz [m/s] GPS velocity down. * @param diff_pressure [Pa] Differential pressure. * @param EAS2TAS Estimated to true airspeed ratio. * @param ratio Airspeed ratio. * @param state_x EKF state x. * @param state_y EKF state y. * @param state_z EKF state z. * @param Pax EKF Pax. * @param Pby EKF Pby. * @param Pcz EKF Pcz. * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_airspeed_autocal_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN]; _mav_put_float(buf, 0, vx); _mav_put_float(buf, 4, vy); _mav_put_float(buf, 8, vz); _mav_put_float(buf, 12, diff_pressure); _mav_put_float(buf, 16, EAS2TAS); _mav_put_float(buf, 20, ratio); _mav_put_float(buf, 24, state_x); _mav_put_float(buf, 28, state_y); _mav_put_float(buf, 32, state_z); _mav_put_float(buf, 36, Pax); _mav_put_float(buf, 40, Pby); _mav_put_float(buf, 44, Pcz); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); #else mavlink_airspeed_autocal_t packet; packet.vx = vx; packet.vy = vy; packet.vz = vz; packet.diff_pressure = diff_pressure; packet.EAS2TAS = EAS2TAS; packet.ratio = ratio; packet.state_x = state_x; packet.state_y = state_y; packet.state_z = state_z; packet.Pax = Pax; packet.Pby = Pby; packet.Pcz = Pcz; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); #endif msg->msgid = MAVLINK_MSG_ID_AIRSPEED_AUTOCAL; return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); } /** * @brief Pack a airspeed_autocal message on a channel * @param system_id ID of this system * @param component_id ID of this component (e.g. 200 for IMU) * @param chan The MAVLink channel this message will be sent over * @param msg The MAVLink message to compress the data into * @param vx [m/s] GPS velocity north. * @param vy [m/s] GPS velocity east. * @param vz [m/s] GPS velocity down. * @param diff_pressure [Pa] Differential pressure. * @param EAS2TAS Estimated to true airspeed ratio. * @param ratio Airspeed ratio. * @param state_x EKF state x. * @param state_y EKF state y. * @param state_z EKF state z. * @param Pax EKF Pax. * @param Pby EKF Pby. * @param Pcz EKF Pcz. * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_airspeed_autocal_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, float vx,float vy,float vz,float diff_pressure,float EAS2TAS,float ratio,float state_x,float state_y,float state_z,float Pax,float Pby,float Pcz) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN]; _mav_put_float(buf, 0, vx); _mav_put_float(buf, 4, vy); _mav_put_float(buf, 8, vz); _mav_put_float(buf, 12, diff_pressure); _mav_put_float(buf, 16, EAS2TAS); _mav_put_float(buf, 20, ratio); _mav_put_float(buf, 24, state_x); _mav_put_float(buf, 28, state_y); _mav_put_float(buf, 32, state_z); _mav_put_float(buf, 36, Pax); _mav_put_float(buf, 40, Pby); _mav_put_float(buf, 44, Pcz); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); #else mavlink_airspeed_autocal_t packet; packet.vx = vx; packet.vy = vy; packet.vz = vz; packet.diff_pressure = diff_pressure; packet.EAS2TAS = EAS2TAS; packet.ratio = ratio; packet.state_x = state_x; packet.state_y = state_y; packet.state_z = state_z; packet.Pax = Pax; packet.Pby = Pby; packet.Pcz = Pcz; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); #endif msg->msgid = MAVLINK_MSG_ID_AIRSPEED_AUTOCAL; return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); } /** * @brief Encode a airspeed_autocal struct * * @param system_id ID of this system * @param component_id ID of this component (e.g. 200 for IMU) * @param msg The MAVLink message to compress the data into * @param airspeed_autocal C-struct to read the message contents from */ static inline uint16_t mavlink_msg_airspeed_autocal_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_airspeed_autocal_t* airspeed_autocal) { return mavlink_msg_airspeed_autocal_pack(system_id, component_id, msg, airspeed_autocal->vx, airspeed_autocal->vy, airspeed_autocal->vz, airspeed_autocal->diff_pressure, airspeed_autocal->EAS2TAS, airspeed_autocal->ratio, airspeed_autocal->state_x, airspeed_autocal->state_y, airspeed_autocal->state_z, airspeed_autocal->Pax, airspeed_autocal->Pby, airspeed_autocal->Pcz); } /** * @brief Encode a airspeed_autocal struct on a channel * * @param system_id ID of this system * @param component_id ID of this component (e.g. 200 for IMU) * @param chan The MAVLink channel this message will be sent over * @param msg The MAVLink message to compress the data into * @param airspeed_autocal C-struct to read the message contents from */ static inline uint16_t mavlink_msg_airspeed_autocal_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_airspeed_autocal_t* airspeed_autocal) { return mavlink_msg_airspeed_autocal_pack_chan(system_id, component_id, chan, msg, airspeed_autocal->vx, airspeed_autocal->vy, airspeed_autocal->vz, airspeed_autocal->diff_pressure, airspeed_autocal->EAS2TAS, airspeed_autocal->ratio, airspeed_autocal->state_x, airspeed_autocal->state_y, airspeed_autocal->state_z, airspeed_autocal->Pax, airspeed_autocal->Pby, airspeed_autocal->Pcz); } /** * @brief Send a airspeed_autocal message * @param chan MAVLink channel to send the message * * @param vx [m/s] GPS velocity north. * @param vy [m/s] GPS velocity east. * @param vz [m/s] GPS velocity down. * @param diff_pressure [Pa] Differential pressure. * @param EAS2TAS Estimated to true airspeed ratio. * @param ratio Airspeed ratio. * @param state_x EKF state x. * @param state_y EKF state y. * @param state_z EKF state z. * @param Pax EKF Pax. * @param Pby EKF Pby. * @param Pcz EKF Pcz. */ #ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS static inline void mavlink_msg_airspeed_autocal_send(mavlink_channel_t chan, float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN]; _mav_put_float(buf, 0, vx); _mav_put_float(buf, 4, vy); _mav_put_float(buf, 8, vz); _mav_put_float(buf, 12, diff_pressure); _mav_put_float(buf, 16, EAS2TAS); _mav_put_float(buf, 20, ratio); _mav_put_float(buf, 24, state_x); _mav_put_float(buf, 28, state_y); _mav_put_float(buf, 32, state_z); _mav_put_float(buf, 36, Pax); _mav_put_float(buf, 40, Pby); _mav_put_float(buf, 44, Pcz); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); #else mavlink_airspeed_autocal_t packet; packet.vx = vx; packet.vy = vy; packet.vz = vz; packet.diff_pressure = diff_pressure; packet.EAS2TAS = EAS2TAS; packet.ratio = ratio; packet.state_x = state_x; packet.state_y = state_y; packet.state_z = state_z; packet.Pax = Pax; packet.Pby = Pby; packet.Pcz = Pcz; _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)&packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); #endif } /** * @brief Send a airspeed_autocal message * @param chan MAVLink channel to send the message * @param struct The MAVLink struct to serialize */ static inline void mavlink_msg_airspeed_autocal_send_struct(mavlink_channel_t chan, const mavlink_airspeed_autocal_t* airspeed_autocal) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS mavlink_msg_airspeed_autocal_send(chan, airspeed_autocal->vx, airspeed_autocal->vy, airspeed_autocal->vz, airspeed_autocal->diff_pressure, airspeed_autocal->EAS2TAS, airspeed_autocal->ratio, airspeed_autocal->state_x, airspeed_autocal->state_y, airspeed_autocal->state_z, airspeed_autocal->Pax, airspeed_autocal->Pby, airspeed_autocal->Pcz); #else _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)airspeed_autocal, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); #endif } #if MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN <= MAVLINK_MAX_PAYLOAD_LEN /* This varient of _send() can be used to save stack space by re-using memory from the receive buffer. The caller provides a mavlink_message_t which is the size of a full mavlink message. This is usually the receive buffer for the channel, and allows a reply to an incoming message with minimum stack space usage. */ static inline void mavlink_msg_airspeed_autocal_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char *buf = (char *)msgbuf; _mav_put_float(buf, 0, vx); _mav_put_float(buf, 4, vy); _mav_put_float(buf, 8, vz); _mav_put_float(buf, 12, diff_pressure); _mav_put_float(buf, 16, EAS2TAS); _mav_put_float(buf, 20, ratio); _mav_put_float(buf, 24, state_x); _mav_put_float(buf, 28, state_y); _mav_put_float(buf, 32, state_z); _mav_put_float(buf, 36, Pax); _mav_put_float(buf, 40, Pby); _mav_put_float(buf, 44, Pcz); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); #else mavlink_airspeed_autocal_t *packet = (mavlink_airspeed_autocal_t *)msgbuf; packet->vx = vx; packet->vy = vy; packet->vz = vz; packet->diff_pressure = diff_pressure; packet->EAS2TAS = EAS2TAS; packet->ratio = ratio; packet->state_x = state_x; packet->state_y = state_y; packet->state_z = state_z; packet->Pax = Pax; packet->Pby = Pby; packet->Pcz = Pcz; _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_MIN_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); #endif } #endif #endif // MESSAGE AIRSPEED_AUTOCAL UNPACKING /** * @brief Get field vx from airspeed_autocal message * * @return [m/s] GPS velocity north. */ static inline float mavlink_msg_airspeed_autocal_get_vx(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 0); } /** * @brief Get field vy from airspeed_autocal message * * @return [m/s] GPS velocity east. */ static inline float mavlink_msg_airspeed_autocal_get_vy(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 4); } /** * @brief Get field vz from airspeed_autocal message * * @return [m/s] GPS velocity down. */ static inline float mavlink_msg_airspeed_autocal_get_vz(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 8); } /** * @brief Get field diff_pressure from airspeed_autocal message * * @return [Pa] Differential pressure. */ static inline float mavlink_msg_airspeed_autocal_get_diff_pressure(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 12); } /** * @brief Get field EAS2TAS from airspeed_autocal message * * @return Estimated to true airspeed ratio. */ static inline float mavlink_msg_airspeed_autocal_get_EAS2TAS(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 16); } /** * @brief Get field ratio from airspeed_autocal message * * @return Airspeed ratio. */ static inline float mavlink_msg_airspeed_autocal_get_ratio(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 20); } /** * @brief Get field state_x from airspeed_autocal message * * @return EKF state x. */ static inline float mavlink_msg_airspeed_autocal_get_state_x(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 24); } /** * @brief Get field state_y from airspeed_autocal message * * @return EKF state y. */ static inline float mavlink_msg_airspeed_autocal_get_state_y(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 28); } /** * @brief Get field state_z from airspeed_autocal message * * @return EKF state z. */ static inline float mavlink_msg_airspeed_autocal_get_state_z(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 32); } /** * @brief Get field Pax from airspeed_autocal message * * @return EKF Pax. */ static inline float mavlink_msg_airspeed_autocal_get_Pax(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 36); } /** * @brief Get field Pby from airspeed_autocal message * * @return EKF Pby. */ static inline float mavlink_msg_airspeed_autocal_get_Pby(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 40); } /** * @brief Get field Pcz from airspeed_autocal message * * @return EKF Pcz. */ static inline float mavlink_msg_airspeed_autocal_get_Pcz(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 44); } /** * @brief Decode a airspeed_autocal message into a struct * * @param msg The message to decode * @param airspeed_autocal C-struct to decode the message contents into */ static inline void mavlink_msg_airspeed_autocal_decode(const mavlink_message_t* msg, mavlink_airspeed_autocal_t* airspeed_autocal) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS airspeed_autocal->vx = mavlink_msg_airspeed_autocal_get_vx(msg); airspeed_autocal->vy = mavlink_msg_airspeed_autocal_get_vy(msg); airspeed_autocal->vz = mavlink_msg_airspeed_autocal_get_vz(msg); airspeed_autocal->diff_pressure = mavlink_msg_airspeed_autocal_get_diff_pressure(msg); airspeed_autocal->EAS2TAS = mavlink_msg_airspeed_autocal_get_EAS2TAS(msg); airspeed_autocal->ratio = mavlink_msg_airspeed_autocal_get_ratio(msg); airspeed_autocal->state_x = mavlink_msg_airspeed_autocal_get_state_x(msg); airspeed_autocal->state_y = mavlink_msg_airspeed_autocal_get_state_y(msg); airspeed_autocal->state_z = mavlink_msg_airspeed_autocal_get_state_z(msg); airspeed_autocal->Pax = mavlink_msg_airspeed_autocal_get_Pax(msg); airspeed_autocal->Pby = mavlink_msg_airspeed_autocal_get_Pby(msg); airspeed_autocal->Pcz = mavlink_msg_airspeed_autocal_get_Pcz(msg); #else uint8_t len = msg->len < MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN? msg->len : MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN; memset(airspeed_autocal, 0, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); memcpy(airspeed_autocal, _MAV_PAYLOAD(msg), len); #endif }