// MESSAGE FW_SOARING_DATA PACKING #define MAVLINK_MSG_ID_FW_SOARING_DATA 210 typedef struct __mavlink_fw_soaring_data_t { uint64_t timestamp; /*< Timestamp [ms]*/ uint64_t timestampModeChanged; /*< Timestamp since last mode change[ms]*/ float CurrentUpdraftSpeed; /*< Updraft speed at current/local airplane position [m/s]*/ float xW; /*< Thermal core updraft strength [m/s]*/ float xR; /*< Thermal radius [m]*/ float xLat; /*< Thermal center latitude [deg]*/ float xLon; /*< Thermal center longitude [deg]*/ float VarW; /*< Variance W*/ float VarR; /*< Variance R*/ float VarLat; /*< Variance Lat*/ float VarLon; /*< Variance Lon */ float LoiterRadius; /*< Suggested loiter radius [m]*/ uint8_t ControlMode; /*< Control Mode [-]*/ uint8_t valid; /*< Data valid [-]*/ } mavlink_fw_soaring_data_t; #define MAVLINK_MSG_ID_FW_SOARING_DATA_LEN 58 #define MAVLINK_MSG_ID_210_LEN 58 #define MAVLINK_MSG_ID_FW_SOARING_DATA_CRC 129 #define MAVLINK_MSG_ID_210_CRC 129 #define MAVLINK_MESSAGE_INFO_FW_SOARING_DATA { \ "FW_SOARING_DATA", \ 14, \ { { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_fw_soaring_data_t, timestamp) }, \ { "timestampModeChanged", NULL, MAVLINK_TYPE_UINT64_T, 0, 8, offsetof(mavlink_fw_soaring_data_t, timestampModeChanged) }, \ { "CurrentUpdraftSpeed", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_fw_soaring_data_t, CurrentUpdraftSpeed) }, \ { "xW", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_fw_soaring_data_t, xW) }, \ { "xR", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_fw_soaring_data_t, xR) }, \ { "xLat", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_fw_soaring_data_t, xLat) }, \ { "xLon", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_fw_soaring_data_t, xLon) }, \ { "VarW", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_fw_soaring_data_t, VarW) }, \ { "VarR", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_fw_soaring_data_t, VarR) }, \ { "VarLat", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_fw_soaring_data_t, VarLat) }, \ { "VarLon", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_fw_soaring_data_t, VarLon) }, \ { "LoiterRadius", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_fw_soaring_data_t, LoiterRadius) }, \ { "ControlMode", NULL, MAVLINK_TYPE_UINT8_T, 0, 56, offsetof(mavlink_fw_soaring_data_t, ControlMode) }, \ { "valid", NULL, MAVLINK_TYPE_UINT8_T, 0, 57, offsetof(mavlink_fw_soaring_data_t, valid) }, \ } \ } /** * @brief Pack a fw_soaring_data 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 timestamp Timestamp [ms] * @param timestampModeChanged Timestamp since last mode change[ms] * @param CurrentUpdraftSpeed Updraft speed at current/local airplane position [m/s] * @param xW Thermal core updraft strength [m/s] * @param xR Thermal radius [m] * @param xLat Thermal center latitude [deg] * @param xLon Thermal center longitude [deg] * @param VarW Variance W * @param VarR Variance R * @param VarLat Variance Lat * @param VarLon Variance Lon * @param LoiterRadius Suggested loiter radius [m] * @param ControlMode Control Mode [-] * @param valid Data valid [-] * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_fw_soaring_data_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, uint64_t timestamp, uint64_t timestampModeChanged, float CurrentUpdraftSpeed, float xW, float xR, float xLat, float xLon, float VarW, float VarR, float VarLat, float VarLon, float LoiterRadius, uint8_t ControlMode, uint8_t valid) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_FW_SOARING_DATA_LEN]; _mav_put_uint64_t(buf, 0, timestamp); _mav_put_uint64_t(buf, 8, timestampModeChanged); _mav_put_float(buf, 16, CurrentUpdraftSpeed); _mav_put_float(buf, 20, xW); _mav_put_float(buf, 24, xR); _mav_put_float(buf, 28, xLat); _mav_put_float(buf, 32, xLon); _mav_put_float(buf, 36, VarW); _mav_put_float(buf, 40, VarR); _mav_put_float(buf, 44, VarLat); _mav_put_float(buf, 48, VarLon); _mav_put_float(buf, 52, LoiterRadius); _mav_put_uint8_t(buf, 56, ControlMode); _mav_put_uint8_t(buf, 57, valid); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #else mavlink_fw_soaring_data_t packet; packet.timestamp = timestamp; packet.timestampModeChanged = timestampModeChanged; packet.CurrentUpdraftSpeed = CurrentUpdraftSpeed; packet.xW = xW; packet.xR = xR; packet.xLat = xLat; packet.xLon = xLon; packet.VarW = VarW; packet.VarR = VarR; packet.VarLat = VarLat; packet.VarLon = VarLon; packet.LoiterRadius = LoiterRadius; packet.ControlMode = ControlMode; packet.valid = valid; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif msg->msgid = MAVLINK_MSG_ID_FW_SOARING_DATA; #if MAVLINK_CRC_EXTRA return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC); #else return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif } /** * @brief Pack a fw_soaring_data 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 timestamp Timestamp [ms] * @param timestampModeChanged Timestamp since last mode change[ms] * @param CurrentUpdraftSpeed Updraft speed at current/local airplane position [m/s] * @param xW Thermal core updraft strength [m/s] * @param xR Thermal radius [m] * @param xLat Thermal center latitude [deg] * @param xLon Thermal center longitude [deg] * @param VarW Variance W * @param VarR Variance R * @param VarLat Variance Lat * @param VarLon Variance Lon * @param LoiterRadius Suggested loiter radius [m] * @param ControlMode Control Mode [-] * @param valid Data valid [-] * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_fw_soaring_data_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, uint64_t timestamp,uint64_t timestampModeChanged,float CurrentUpdraftSpeed,float xW,float xR,float xLat,float xLon,float VarW,float VarR,float VarLat,float VarLon,float LoiterRadius,uint8_t ControlMode,uint8_t valid) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_FW_SOARING_DATA_LEN]; _mav_put_uint64_t(buf, 0, timestamp); _mav_put_uint64_t(buf, 8, timestampModeChanged); _mav_put_float(buf, 16, CurrentUpdraftSpeed); _mav_put_float(buf, 20, xW); _mav_put_float(buf, 24, xR); _mav_put_float(buf, 28, xLat); _mav_put_float(buf, 32, xLon); _mav_put_float(buf, 36, VarW); _mav_put_float(buf, 40, VarR); _mav_put_float(buf, 44, VarLat); _mav_put_float(buf, 48, VarLon); _mav_put_float(buf, 52, LoiterRadius); _mav_put_uint8_t(buf, 56, ControlMode); _mav_put_uint8_t(buf, 57, valid); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #else mavlink_fw_soaring_data_t packet; packet.timestamp = timestamp; packet.timestampModeChanged = timestampModeChanged; packet.CurrentUpdraftSpeed = CurrentUpdraftSpeed; packet.xW = xW; packet.xR = xR; packet.xLat = xLat; packet.xLon = xLon; packet.VarW = VarW; packet.VarR = VarR; packet.VarLat = VarLat; packet.VarLon = VarLon; packet.LoiterRadius = LoiterRadius; packet.ControlMode = ControlMode; packet.valid = valid; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif msg->msgid = MAVLINK_MSG_ID_FW_SOARING_DATA; #if MAVLINK_CRC_EXTRA return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC); #else return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif } /** * @brief Encode a fw_soaring_data 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 fw_soaring_data C-struct to read the message contents from */ static inline uint16_t mavlink_msg_fw_soaring_data_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_fw_soaring_data_t* fw_soaring_data) { return mavlink_msg_fw_soaring_data_pack(system_id, component_id, msg, fw_soaring_data->timestamp, fw_soaring_data->timestampModeChanged, fw_soaring_data->CurrentUpdraftSpeed, fw_soaring_data->xW, fw_soaring_data->xR, fw_soaring_data->xLat, fw_soaring_data->xLon, fw_soaring_data->VarW, fw_soaring_data->VarR, fw_soaring_data->VarLat, fw_soaring_data->VarLon, fw_soaring_data->LoiterRadius, fw_soaring_data->ControlMode, fw_soaring_data->valid); } /** * @brief Encode a fw_soaring_data 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 fw_soaring_data C-struct to read the message contents from */ static inline uint16_t mavlink_msg_fw_soaring_data_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_fw_soaring_data_t* fw_soaring_data) { return mavlink_msg_fw_soaring_data_pack_chan(system_id, component_id, chan, msg, fw_soaring_data->timestamp, fw_soaring_data->timestampModeChanged, fw_soaring_data->CurrentUpdraftSpeed, fw_soaring_data->xW, fw_soaring_data->xR, fw_soaring_data->xLat, fw_soaring_data->xLon, fw_soaring_data->VarW, fw_soaring_data->VarR, fw_soaring_data->VarLat, fw_soaring_data->VarLon, fw_soaring_data->LoiterRadius, fw_soaring_data->ControlMode, fw_soaring_data->valid); } /** * @brief Send a fw_soaring_data message * @param chan MAVLink channel to send the message * * @param timestamp Timestamp [ms] * @param timestampModeChanged Timestamp since last mode change[ms] * @param CurrentUpdraftSpeed Updraft speed at current/local airplane position [m/s] * @param xW Thermal core updraft strength [m/s] * @param xR Thermal radius [m] * @param xLat Thermal center latitude [deg] * @param xLon Thermal center longitude [deg] * @param VarW Variance W * @param VarR Variance R * @param VarLat Variance Lat * @param VarLon Variance Lon * @param LoiterRadius Suggested loiter radius [m] * @param ControlMode Control Mode [-] * @param valid Data valid [-] */ #ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS static inline void mavlink_msg_fw_soaring_data_send(mavlink_channel_t chan, uint64_t timestamp, uint64_t timestampModeChanged, float CurrentUpdraftSpeed, float xW, float xR, float xLat, float xLon, float VarW, float VarR, float VarLat, float VarLon, float LoiterRadius, uint8_t ControlMode, uint8_t valid) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_FW_SOARING_DATA_LEN]; _mav_put_uint64_t(buf, 0, timestamp); _mav_put_uint64_t(buf, 8, timestampModeChanged); _mav_put_float(buf, 16, CurrentUpdraftSpeed); _mav_put_float(buf, 20, xW); _mav_put_float(buf, 24, xR); _mav_put_float(buf, 28, xLat); _mav_put_float(buf, 32, xLon); _mav_put_float(buf, 36, VarW); _mav_put_float(buf, 40, VarR); _mav_put_float(buf, 44, VarLat); _mav_put_float(buf, 48, VarLon); _mav_put_float(buf, 52, LoiterRadius); _mav_put_uint8_t(buf, 56, ControlMode); _mav_put_uint8_t(buf, 57, valid); #if MAVLINK_CRC_EXTRA _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, buf, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC); #else _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, buf, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif #else mavlink_fw_soaring_data_t packet; packet.timestamp = timestamp; packet.timestampModeChanged = timestampModeChanged; packet.CurrentUpdraftSpeed = CurrentUpdraftSpeed; packet.xW = xW; packet.xR = xR; packet.xLat = xLat; packet.xLon = xLon; packet.VarW = VarW; packet.VarR = VarR; packet.VarLat = VarLat; packet.VarLon = VarLon; packet.LoiterRadius = LoiterRadius; packet.ControlMode = ControlMode; packet.valid = valid; #if MAVLINK_CRC_EXTRA _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, (const char *)&packet, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC); #else _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, (const char *)&packet, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif #endif } #if MAVLINK_MSG_ID_FW_SOARING_DATA_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_fw_soaring_data_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint64_t timestampModeChanged, float CurrentUpdraftSpeed, float xW, float xR, float xLat, float xLon, float VarW, float VarR, float VarLat, float VarLon, float LoiterRadius, uint8_t ControlMode, uint8_t valid) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char *buf = (char *)msgbuf; _mav_put_uint64_t(buf, 0, timestamp); _mav_put_uint64_t(buf, 8, timestampModeChanged); _mav_put_float(buf, 16, CurrentUpdraftSpeed); _mav_put_float(buf, 20, xW); _mav_put_float(buf, 24, xR); _mav_put_float(buf, 28, xLat); _mav_put_float(buf, 32, xLon); _mav_put_float(buf, 36, VarW); _mav_put_float(buf, 40, VarR); _mav_put_float(buf, 44, VarLat); _mav_put_float(buf, 48, VarLon); _mav_put_float(buf, 52, LoiterRadius); _mav_put_uint8_t(buf, 56, ControlMode); _mav_put_uint8_t(buf, 57, valid); #if MAVLINK_CRC_EXTRA _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, buf, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC); #else _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, buf, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif #else mavlink_fw_soaring_data_t *packet = (mavlink_fw_soaring_data_t *)msgbuf; packet->timestamp = timestamp; packet->timestampModeChanged = timestampModeChanged; packet->CurrentUpdraftSpeed = CurrentUpdraftSpeed; packet->xW = xW; packet->xR = xR; packet->xLat = xLat; packet->xLon = xLon; packet->VarW = VarW; packet->VarR = VarR; packet->VarLat = VarLat; packet->VarLon = VarLon; packet->LoiterRadius = LoiterRadius; packet->ControlMode = ControlMode; packet->valid = valid; #if MAVLINK_CRC_EXTRA _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, (const char *)packet, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC); #else _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, (const char *)packet, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif #endif } #endif #endif // MESSAGE FW_SOARING_DATA UNPACKING /** * @brief Get field timestamp from fw_soaring_data message * * @return Timestamp [ms] */ static inline uint64_t mavlink_msg_fw_soaring_data_get_timestamp(const mavlink_message_t* msg) { return _MAV_RETURN_uint64_t(msg, 0); } /** * @brief Get field timestampModeChanged from fw_soaring_data message * * @return Timestamp since last mode change[ms] */ static inline uint64_t mavlink_msg_fw_soaring_data_get_timestampModeChanged(const mavlink_message_t* msg) { return _MAV_RETURN_uint64_t(msg, 8); } /** * @brief Get field CurrentUpdraftSpeed from fw_soaring_data message * * @return Updraft speed at current/local airplane position [m/s] */ static inline float mavlink_msg_fw_soaring_data_get_CurrentUpdraftSpeed(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 16); } /** * @brief Get field xW from fw_soaring_data message * * @return Thermal core updraft strength [m/s] */ static inline float mavlink_msg_fw_soaring_data_get_xW(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 20); } /** * @brief Get field xR from fw_soaring_data message * * @return Thermal radius [m] */ static inline float mavlink_msg_fw_soaring_data_get_xR(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 24); } /** * @brief Get field xLat from fw_soaring_data message * * @return Thermal center latitude [deg] */ static inline float mavlink_msg_fw_soaring_data_get_xLat(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 28); } /** * @brief Get field xLon from fw_soaring_data message * * @return Thermal center longitude [deg] */ static inline float mavlink_msg_fw_soaring_data_get_xLon(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 32); } /** * @brief Get field VarW from fw_soaring_data message * * @return Variance W */ static inline float mavlink_msg_fw_soaring_data_get_VarW(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 36); } /** * @brief Get field VarR from fw_soaring_data message * * @return Variance R */ static inline float mavlink_msg_fw_soaring_data_get_VarR(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 40); } /** * @brief Get field VarLat from fw_soaring_data message * * @return Variance Lat */ static inline float mavlink_msg_fw_soaring_data_get_VarLat(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 44); } /** * @brief Get field VarLon from fw_soaring_data message * * @return Variance Lon */ static inline float mavlink_msg_fw_soaring_data_get_VarLon(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 48); } /** * @brief Get field LoiterRadius from fw_soaring_data message * * @return Suggested loiter radius [m] */ static inline float mavlink_msg_fw_soaring_data_get_LoiterRadius(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 52); } /** * @brief Get field ControlMode from fw_soaring_data message * * @return Control Mode [-] */ static inline uint8_t mavlink_msg_fw_soaring_data_get_ControlMode(const mavlink_message_t* msg) { return _MAV_RETURN_uint8_t(msg, 56); } /** * @brief Get field valid from fw_soaring_data message * * @return Data valid [-] */ static inline uint8_t mavlink_msg_fw_soaring_data_get_valid(const mavlink_message_t* msg) { return _MAV_RETURN_uint8_t(msg, 57); } /** * @brief Decode a fw_soaring_data message into a struct * * @param msg The message to decode * @param fw_soaring_data C-struct to decode the message contents into */ static inline void mavlink_msg_fw_soaring_data_decode(const mavlink_message_t* msg, mavlink_fw_soaring_data_t* fw_soaring_data) { #if MAVLINK_NEED_BYTE_SWAP fw_soaring_data->timestamp = mavlink_msg_fw_soaring_data_get_timestamp(msg); fw_soaring_data->timestampModeChanged = mavlink_msg_fw_soaring_data_get_timestampModeChanged(msg); fw_soaring_data->CurrentUpdraftSpeed = mavlink_msg_fw_soaring_data_get_CurrentUpdraftSpeed(msg); fw_soaring_data->xW = mavlink_msg_fw_soaring_data_get_xW(msg); fw_soaring_data->xR = mavlink_msg_fw_soaring_data_get_xR(msg); fw_soaring_data->xLat = mavlink_msg_fw_soaring_data_get_xLat(msg); fw_soaring_data->xLon = mavlink_msg_fw_soaring_data_get_xLon(msg); fw_soaring_data->VarW = mavlink_msg_fw_soaring_data_get_VarW(msg); fw_soaring_data->VarR = mavlink_msg_fw_soaring_data_get_VarR(msg); fw_soaring_data->VarLat = mavlink_msg_fw_soaring_data_get_VarLat(msg); fw_soaring_data->VarLon = mavlink_msg_fw_soaring_data_get_VarLon(msg); fw_soaring_data->LoiterRadius = mavlink_msg_fw_soaring_data_get_LoiterRadius(msg); fw_soaring_data->ControlMode = mavlink_msg_fw_soaring_data_get_ControlMode(msg); fw_soaring_data->valid = mavlink_msg_fw_soaring_data_get_valid(msg); #else memcpy(fw_soaring_data, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_FW_SOARING_DATA_LEN); #endif }