#pragma once // MESSAGE UAVIONIX_ADSB_OUT_DYNAMIC PACKING #define MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC 10002 typedef struct __mavlink_uavionix_adsb_out_dynamic_t { uint32_t utcTime; /*< [s] UTC time in seconds since GPS epoch (Jan 6, 1980). If unknown set to UINT32_MAX*/ int32_t gpsLat; /*< [degE7] Latitude WGS84 (deg * 1E7). If unknown set to INT32_MAX*/ int32_t gpsLon; /*< [degE7] Longitude WGS84 (deg * 1E7). If unknown set to INT32_MAX*/ int32_t gpsAlt; /*< [mm] Altitude (WGS84). UP +ve. If unknown set to INT32_MAX*/ int32_t baroAltMSL; /*< [mbar] Barometric pressure altitude (MSL) relative to a standard atmosphere of 1013.2 mBar and NOT bar corrected altitude (m * 1E-3). (up +ve). If unknown set to INT32_MAX*/ uint32_t accuracyHor; /*< [mm] Horizontal accuracy in mm (m * 1E-3). If unknown set to UINT32_MAX*/ uint16_t accuracyVert; /*< [cm] Vertical accuracy in cm. If unknown set to UINT16_MAX*/ uint16_t accuracyVel; /*< [mm/s] Velocity accuracy in mm/s (m * 1E-3). If unknown set to UINT16_MAX*/ int16_t velVert; /*< [cm/s] GPS vertical speed in cm/s. If unknown set to INT16_MAX*/ int16_t velNS; /*< [cm/s] North-South velocity over ground in cm/s North +ve. If unknown set to INT16_MAX*/ int16_t VelEW; /*< [cm/s] East-West velocity over ground in cm/s East +ve. If unknown set to INT16_MAX*/ uint16_t state; /*< ADS-B transponder dynamic input state flags*/ uint16_t squawk; /*< Mode A code (typically 1200 [0x04B0] for VFR)*/ uint8_t gpsFix; /*< 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS, 5: RTK*/ uint8_t numSats; /*< Number of satellites visible. If unknown set to UINT8_MAX*/ uint8_t emergencyStatus; /*< Emergency status*/ } mavlink_uavionix_adsb_out_dynamic_t; #define MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN 41 #define MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_MIN_LEN 41 #define MAVLINK_MSG_ID_10002_LEN 41 #define MAVLINK_MSG_ID_10002_MIN_LEN 41 #define MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_CRC 186 #define MAVLINK_MSG_ID_10002_CRC 186 #if MAVLINK_COMMAND_24BIT #define MAVLINK_MESSAGE_INFO_UAVIONIX_ADSB_OUT_DYNAMIC { \ 10002, \ "UAVIONIX_ADSB_OUT_DYNAMIC", \ 16, \ { { "utcTime", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_uavionix_adsb_out_dynamic_t, utcTime) }, \ { "gpsLat", NULL, MAVLINK_TYPE_INT32_T, 0, 4, offsetof(mavlink_uavionix_adsb_out_dynamic_t, gpsLat) }, \ { "gpsLon", NULL, MAVLINK_TYPE_INT32_T, 0, 8, offsetof(mavlink_uavionix_adsb_out_dynamic_t, gpsLon) }, \ { "gpsAlt", NULL, MAVLINK_TYPE_INT32_T, 0, 12, offsetof(mavlink_uavionix_adsb_out_dynamic_t, gpsAlt) }, \ { "gpsFix", NULL, MAVLINK_TYPE_UINT8_T, 0, 38, offsetof(mavlink_uavionix_adsb_out_dynamic_t, gpsFix) }, \ { "numSats", NULL, MAVLINK_TYPE_UINT8_T, 0, 39, offsetof(mavlink_uavionix_adsb_out_dynamic_t, numSats) }, \ { "baroAltMSL", NULL, MAVLINK_TYPE_INT32_T, 0, 16, offsetof(mavlink_uavionix_adsb_out_dynamic_t, baroAltMSL) }, \ { "accuracyHor", NULL, MAVLINK_TYPE_UINT32_T, 0, 20, offsetof(mavlink_uavionix_adsb_out_dynamic_t, accuracyHor) }, \ { "accuracyVert", NULL, MAVLINK_TYPE_UINT16_T, 0, 24, offsetof(mavlink_uavionix_adsb_out_dynamic_t, accuracyVert) }, \ { "accuracyVel", NULL, MAVLINK_TYPE_UINT16_T, 0, 26, offsetof(mavlink_uavionix_adsb_out_dynamic_t, accuracyVel) }, \ { "velVert", NULL, MAVLINK_TYPE_INT16_T, 0, 28, offsetof(mavlink_uavionix_adsb_out_dynamic_t, velVert) }, \ { "velNS", NULL, MAVLINK_TYPE_INT16_T, 0, 30, offsetof(mavlink_uavionix_adsb_out_dynamic_t, velNS) }, \ { "VelEW", NULL, MAVLINK_TYPE_INT16_T, 0, 32, offsetof(mavlink_uavionix_adsb_out_dynamic_t, VelEW) }, \ { "emergencyStatus", NULL, MAVLINK_TYPE_UINT8_T, 0, 40, offsetof(mavlink_uavionix_adsb_out_dynamic_t, emergencyStatus) }, \ { "state", NULL, MAVLINK_TYPE_UINT16_T, 0, 34, offsetof(mavlink_uavionix_adsb_out_dynamic_t, state) }, \ { "squawk", NULL, MAVLINK_TYPE_UINT16_T, 0, 36, offsetof(mavlink_uavionix_adsb_out_dynamic_t, squawk) }, \ } \ } #else #define MAVLINK_MESSAGE_INFO_UAVIONIX_ADSB_OUT_DYNAMIC { \ "UAVIONIX_ADSB_OUT_DYNAMIC", \ 16, \ { { "utcTime", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_uavionix_adsb_out_dynamic_t, utcTime) }, \ { "gpsLat", NULL, MAVLINK_TYPE_INT32_T, 0, 4, offsetof(mavlink_uavionix_adsb_out_dynamic_t, gpsLat) }, \ { "gpsLon", NULL, MAVLINK_TYPE_INT32_T, 0, 8, offsetof(mavlink_uavionix_adsb_out_dynamic_t, gpsLon) }, \ { "gpsAlt", NULL, MAVLINK_TYPE_INT32_T, 0, 12, offsetof(mavlink_uavionix_adsb_out_dynamic_t, gpsAlt) }, \ { "gpsFix", NULL, MAVLINK_TYPE_UINT8_T, 0, 38, offsetof(mavlink_uavionix_adsb_out_dynamic_t, gpsFix) }, \ { "numSats", NULL, MAVLINK_TYPE_UINT8_T, 0, 39, offsetof(mavlink_uavionix_adsb_out_dynamic_t, numSats) }, \ { "baroAltMSL", NULL, MAVLINK_TYPE_INT32_T, 0, 16, offsetof(mavlink_uavionix_adsb_out_dynamic_t, baroAltMSL) }, \ { "accuracyHor", NULL, MAVLINK_TYPE_UINT32_T, 0, 20, offsetof(mavlink_uavionix_adsb_out_dynamic_t, accuracyHor) }, \ { "accuracyVert", NULL, MAVLINK_TYPE_UINT16_T, 0, 24, offsetof(mavlink_uavionix_adsb_out_dynamic_t, accuracyVert) }, \ { "accuracyVel", NULL, MAVLINK_TYPE_UINT16_T, 0, 26, offsetof(mavlink_uavionix_adsb_out_dynamic_t, accuracyVel) }, \ { "velVert", NULL, MAVLINK_TYPE_INT16_T, 0, 28, offsetof(mavlink_uavionix_adsb_out_dynamic_t, velVert) }, \ { "velNS", NULL, MAVLINK_TYPE_INT16_T, 0, 30, offsetof(mavlink_uavionix_adsb_out_dynamic_t, velNS) }, \ { "VelEW", NULL, MAVLINK_TYPE_INT16_T, 0, 32, offsetof(mavlink_uavionix_adsb_out_dynamic_t, VelEW) }, \ { "emergencyStatus", NULL, MAVLINK_TYPE_UINT8_T, 0, 40, offsetof(mavlink_uavionix_adsb_out_dynamic_t, emergencyStatus) }, \ { "state", NULL, MAVLINK_TYPE_UINT16_T, 0, 34, offsetof(mavlink_uavionix_adsb_out_dynamic_t, state) }, \ { "squawk", NULL, MAVLINK_TYPE_UINT16_T, 0, 36, offsetof(mavlink_uavionix_adsb_out_dynamic_t, squawk) }, \ } \ } #endif /** * @brief Pack a uavionix_adsb_out_dynamic 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 utcTime [s] UTC time in seconds since GPS epoch (Jan 6, 1980). If unknown set to UINT32_MAX * @param gpsLat [degE7] Latitude WGS84 (deg * 1E7). If unknown set to INT32_MAX * @param gpsLon [degE7] Longitude WGS84 (deg * 1E7). If unknown set to INT32_MAX * @param gpsAlt [mm] Altitude (WGS84). UP +ve. If unknown set to INT32_MAX * @param gpsFix 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS, 5: RTK * @param numSats Number of satellites visible. If unknown set to UINT8_MAX * @param baroAltMSL [mbar] Barometric pressure altitude (MSL) relative to a standard atmosphere of 1013.2 mBar and NOT bar corrected altitude (m * 1E-3). (up +ve). If unknown set to INT32_MAX * @param accuracyHor [mm] Horizontal accuracy in mm (m * 1E-3). If unknown set to UINT32_MAX * @param accuracyVert [cm] Vertical accuracy in cm. If unknown set to UINT16_MAX * @param accuracyVel [mm/s] Velocity accuracy in mm/s (m * 1E-3). If unknown set to UINT16_MAX * @param velVert [cm/s] GPS vertical speed in cm/s. If unknown set to INT16_MAX * @param velNS [cm/s] North-South velocity over ground in cm/s North +ve. If unknown set to INT16_MAX * @param VelEW [cm/s] East-West velocity over ground in cm/s East +ve. If unknown set to INT16_MAX * @param emergencyStatus Emergency status * @param state ADS-B transponder dynamic input state flags * @param squawk Mode A code (typically 1200 [0x04B0] for VFR) * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_uavionix_adsb_out_dynamic_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, uint32_t utcTime, int32_t gpsLat, int32_t gpsLon, int32_t gpsAlt, uint8_t gpsFix, uint8_t numSats, int32_t baroAltMSL, uint32_t accuracyHor, uint16_t accuracyVert, uint16_t accuracyVel, int16_t velVert, int16_t velNS, int16_t VelEW, uint8_t emergencyStatus, uint16_t state, uint16_t squawk) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN]; _mav_put_uint32_t(buf, 0, utcTime); _mav_put_int32_t(buf, 4, gpsLat); _mav_put_int32_t(buf, 8, gpsLon); _mav_put_int32_t(buf, 12, gpsAlt); _mav_put_int32_t(buf, 16, baroAltMSL); _mav_put_uint32_t(buf, 20, accuracyHor); _mav_put_uint16_t(buf, 24, accuracyVert); _mav_put_uint16_t(buf, 26, accuracyVel); _mav_put_int16_t(buf, 28, velVert); _mav_put_int16_t(buf, 30, velNS); _mav_put_int16_t(buf, 32, VelEW); _mav_put_uint16_t(buf, 34, state); _mav_put_uint16_t(buf, 36, squawk); _mav_put_uint8_t(buf, 38, gpsFix); _mav_put_uint8_t(buf, 39, numSats); _mav_put_uint8_t(buf, 40, emergencyStatus); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN); #else mavlink_uavionix_adsb_out_dynamic_t packet; packet.utcTime = utcTime; packet.gpsLat = gpsLat; packet.gpsLon = gpsLon; packet.gpsAlt = gpsAlt; packet.baroAltMSL = baroAltMSL; packet.accuracyHor = accuracyHor; packet.accuracyVert = accuracyVert; packet.accuracyVel = accuracyVel; packet.velVert = velVert; packet.velNS = velNS; packet.VelEW = VelEW; packet.state = state; packet.squawk = squawk; packet.gpsFix = gpsFix; packet.numSats = numSats; packet.emergencyStatus = emergencyStatus; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN); #endif msg->msgid = MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC; return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_MIN_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_CRC); } /** * @brief Pack a uavionix_adsb_out_dynamic 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 utcTime [s] UTC time in seconds since GPS epoch (Jan 6, 1980). If unknown set to UINT32_MAX * @param gpsLat [degE7] Latitude WGS84 (deg * 1E7). If unknown set to INT32_MAX * @param gpsLon [degE7] Longitude WGS84 (deg * 1E7). If unknown set to INT32_MAX * @param gpsAlt [mm] Altitude (WGS84). UP +ve. If unknown set to INT32_MAX * @param gpsFix 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS, 5: RTK * @param numSats Number of satellites visible. If unknown set to UINT8_MAX * @param baroAltMSL [mbar] Barometric pressure altitude (MSL) relative to a standard atmosphere of 1013.2 mBar and NOT bar corrected altitude (m * 1E-3). (up +ve). If unknown set to INT32_MAX * @param accuracyHor [mm] Horizontal accuracy in mm (m * 1E-3). If unknown set to UINT32_MAX * @param accuracyVert [cm] Vertical accuracy in cm. If unknown set to UINT16_MAX * @param accuracyVel [mm/s] Velocity accuracy in mm/s (m * 1E-3). If unknown set to UINT16_MAX * @param velVert [cm/s] GPS vertical speed in cm/s. If unknown set to INT16_MAX * @param velNS [cm/s] North-South velocity over ground in cm/s North +ve. If unknown set to INT16_MAX * @param VelEW [cm/s] East-West velocity over ground in cm/s East +ve. If unknown set to INT16_MAX * @param emergencyStatus Emergency status * @param state ADS-B transponder dynamic input state flags * @param squawk Mode A code (typically 1200 [0x04B0] for VFR) * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_uavionix_adsb_out_dynamic_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, uint32_t utcTime,int32_t gpsLat,int32_t gpsLon,int32_t gpsAlt,uint8_t gpsFix,uint8_t numSats,int32_t baroAltMSL,uint32_t accuracyHor,uint16_t accuracyVert,uint16_t accuracyVel,int16_t velVert,int16_t velNS,int16_t VelEW,uint8_t emergencyStatus,uint16_t state,uint16_t squawk) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN]; _mav_put_uint32_t(buf, 0, utcTime); _mav_put_int32_t(buf, 4, gpsLat); _mav_put_int32_t(buf, 8, gpsLon); _mav_put_int32_t(buf, 12, gpsAlt); _mav_put_int32_t(buf, 16, baroAltMSL); _mav_put_uint32_t(buf, 20, accuracyHor); _mav_put_uint16_t(buf, 24, accuracyVert); _mav_put_uint16_t(buf, 26, accuracyVel); _mav_put_int16_t(buf, 28, velVert); _mav_put_int16_t(buf, 30, velNS); _mav_put_int16_t(buf, 32, VelEW); _mav_put_uint16_t(buf, 34, state); _mav_put_uint16_t(buf, 36, squawk); _mav_put_uint8_t(buf, 38, gpsFix); _mav_put_uint8_t(buf, 39, numSats); _mav_put_uint8_t(buf, 40, emergencyStatus); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN); #else mavlink_uavionix_adsb_out_dynamic_t packet; packet.utcTime = utcTime; packet.gpsLat = gpsLat; packet.gpsLon = gpsLon; packet.gpsAlt = gpsAlt; packet.baroAltMSL = baroAltMSL; packet.accuracyHor = accuracyHor; packet.accuracyVert = accuracyVert; packet.accuracyVel = accuracyVel; packet.velVert = velVert; packet.velNS = velNS; packet.VelEW = VelEW; packet.state = state; packet.squawk = squawk; packet.gpsFix = gpsFix; packet.numSats = numSats; packet.emergencyStatus = emergencyStatus; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN); #endif msg->msgid = MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC; return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_MIN_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_CRC); } /** * @brief Encode a uavionix_adsb_out_dynamic 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 uavionix_adsb_out_dynamic C-struct to read the message contents from */ static inline uint16_t mavlink_msg_uavionix_adsb_out_dynamic_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_uavionix_adsb_out_dynamic_t* uavionix_adsb_out_dynamic) { return mavlink_msg_uavionix_adsb_out_dynamic_pack(system_id, component_id, msg, uavionix_adsb_out_dynamic->utcTime, uavionix_adsb_out_dynamic->gpsLat, uavionix_adsb_out_dynamic->gpsLon, uavionix_adsb_out_dynamic->gpsAlt, uavionix_adsb_out_dynamic->gpsFix, uavionix_adsb_out_dynamic->numSats, uavionix_adsb_out_dynamic->baroAltMSL, uavionix_adsb_out_dynamic->accuracyHor, uavionix_adsb_out_dynamic->accuracyVert, uavionix_adsb_out_dynamic->accuracyVel, uavionix_adsb_out_dynamic->velVert, uavionix_adsb_out_dynamic->velNS, uavionix_adsb_out_dynamic->VelEW, uavionix_adsb_out_dynamic->emergencyStatus, uavionix_adsb_out_dynamic->state, uavionix_adsb_out_dynamic->squawk); } /** * @brief Encode a uavionix_adsb_out_dynamic 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 uavionix_adsb_out_dynamic C-struct to read the message contents from */ static inline uint16_t mavlink_msg_uavionix_adsb_out_dynamic_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_uavionix_adsb_out_dynamic_t* uavionix_adsb_out_dynamic) { return mavlink_msg_uavionix_adsb_out_dynamic_pack_chan(system_id, component_id, chan, msg, uavionix_adsb_out_dynamic->utcTime, uavionix_adsb_out_dynamic->gpsLat, uavionix_adsb_out_dynamic->gpsLon, uavionix_adsb_out_dynamic->gpsAlt, uavionix_adsb_out_dynamic->gpsFix, uavionix_adsb_out_dynamic->numSats, uavionix_adsb_out_dynamic->baroAltMSL, uavionix_adsb_out_dynamic->accuracyHor, uavionix_adsb_out_dynamic->accuracyVert, uavionix_adsb_out_dynamic->accuracyVel, uavionix_adsb_out_dynamic->velVert, uavionix_adsb_out_dynamic->velNS, uavionix_adsb_out_dynamic->VelEW, uavionix_adsb_out_dynamic->emergencyStatus, uavionix_adsb_out_dynamic->state, uavionix_adsb_out_dynamic->squawk); } /** * @brief Send a uavionix_adsb_out_dynamic message * @param chan MAVLink channel to send the message * * @param utcTime [s] UTC time in seconds since GPS epoch (Jan 6, 1980). If unknown set to UINT32_MAX * @param gpsLat [degE7] Latitude WGS84 (deg * 1E7). If unknown set to INT32_MAX * @param gpsLon [degE7] Longitude WGS84 (deg * 1E7). If unknown set to INT32_MAX * @param gpsAlt [mm] Altitude (WGS84). UP +ve. If unknown set to INT32_MAX * @param gpsFix 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS, 5: RTK * @param numSats Number of satellites visible. If unknown set to UINT8_MAX * @param baroAltMSL [mbar] Barometric pressure altitude (MSL) relative to a standard atmosphere of 1013.2 mBar and NOT bar corrected altitude (m * 1E-3). (up +ve). If unknown set to INT32_MAX * @param accuracyHor [mm] Horizontal accuracy in mm (m * 1E-3). If unknown set to UINT32_MAX * @param accuracyVert [cm] Vertical accuracy in cm. If unknown set to UINT16_MAX * @param accuracyVel [mm/s] Velocity accuracy in mm/s (m * 1E-3). If unknown set to UINT16_MAX * @param velVert [cm/s] GPS vertical speed in cm/s. If unknown set to INT16_MAX * @param velNS [cm/s] North-South velocity over ground in cm/s North +ve. If unknown set to INT16_MAX * @param VelEW [cm/s] East-West velocity over ground in cm/s East +ve. If unknown set to INT16_MAX * @param emergencyStatus Emergency status * @param state ADS-B transponder dynamic input state flags * @param squawk Mode A code (typically 1200 [0x04B0] for VFR) */ #ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS static inline void mavlink_msg_uavionix_adsb_out_dynamic_send(mavlink_channel_t chan, uint32_t utcTime, int32_t gpsLat, int32_t gpsLon, int32_t gpsAlt, uint8_t gpsFix, uint8_t numSats, int32_t baroAltMSL, uint32_t accuracyHor, uint16_t accuracyVert, uint16_t accuracyVel, int16_t velVert, int16_t velNS, int16_t VelEW, uint8_t emergencyStatus, uint16_t state, uint16_t squawk) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN]; _mav_put_uint32_t(buf, 0, utcTime); _mav_put_int32_t(buf, 4, gpsLat); _mav_put_int32_t(buf, 8, gpsLon); _mav_put_int32_t(buf, 12, gpsAlt); _mav_put_int32_t(buf, 16, baroAltMSL); _mav_put_uint32_t(buf, 20, accuracyHor); _mav_put_uint16_t(buf, 24, accuracyVert); _mav_put_uint16_t(buf, 26, accuracyVel); _mav_put_int16_t(buf, 28, velVert); _mav_put_int16_t(buf, 30, velNS); _mav_put_int16_t(buf, 32, VelEW); _mav_put_uint16_t(buf, 34, state); _mav_put_uint16_t(buf, 36, squawk); _mav_put_uint8_t(buf, 38, gpsFix); _mav_put_uint8_t(buf, 39, numSats); _mav_put_uint8_t(buf, 40, emergencyStatus); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC, buf, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_MIN_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_CRC); #else mavlink_uavionix_adsb_out_dynamic_t packet; packet.utcTime = utcTime; packet.gpsLat = gpsLat; packet.gpsLon = gpsLon; packet.gpsAlt = gpsAlt; packet.baroAltMSL = baroAltMSL; packet.accuracyHor = accuracyHor; packet.accuracyVert = accuracyVert; packet.accuracyVel = accuracyVel; packet.velVert = velVert; packet.velNS = velNS; packet.VelEW = VelEW; packet.state = state; packet.squawk = squawk; packet.gpsFix = gpsFix; packet.numSats = numSats; packet.emergencyStatus = emergencyStatus; _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC, (const char *)&packet, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_MIN_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_CRC); #endif } /** * @brief Send a uavionix_adsb_out_dynamic message * @param chan MAVLink channel to send the message * @param struct The MAVLink struct to serialize */ static inline void mavlink_msg_uavionix_adsb_out_dynamic_send_struct(mavlink_channel_t chan, const mavlink_uavionix_adsb_out_dynamic_t* uavionix_adsb_out_dynamic) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS mavlink_msg_uavionix_adsb_out_dynamic_send(chan, uavionix_adsb_out_dynamic->utcTime, uavionix_adsb_out_dynamic->gpsLat, uavionix_adsb_out_dynamic->gpsLon, uavionix_adsb_out_dynamic->gpsAlt, uavionix_adsb_out_dynamic->gpsFix, uavionix_adsb_out_dynamic->numSats, uavionix_adsb_out_dynamic->baroAltMSL, uavionix_adsb_out_dynamic->accuracyHor, uavionix_adsb_out_dynamic->accuracyVert, uavionix_adsb_out_dynamic->accuracyVel, uavionix_adsb_out_dynamic->velVert, uavionix_adsb_out_dynamic->velNS, uavionix_adsb_out_dynamic->VelEW, uavionix_adsb_out_dynamic->emergencyStatus, uavionix_adsb_out_dynamic->state, uavionix_adsb_out_dynamic->squawk); #else _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC, (const char *)uavionix_adsb_out_dynamic, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_MIN_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_CRC); #endif } #if MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN <= MAVLINK_MAX_PAYLOAD_LEN /* This variant 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_uavionix_adsb_out_dynamic_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t utcTime, int32_t gpsLat, int32_t gpsLon, int32_t gpsAlt, uint8_t gpsFix, uint8_t numSats, int32_t baroAltMSL, uint32_t accuracyHor, uint16_t accuracyVert, uint16_t accuracyVel, int16_t velVert, int16_t velNS, int16_t VelEW, uint8_t emergencyStatus, uint16_t state, uint16_t squawk) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char *buf = (char *)msgbuf; _mav_put_uint32_t(buf, 0, utcTime); _mav_put_int32_t(buf, 4, gpsLat); _mav_put_int32_t(buf, 8, gpsLon); _mav_put_int32_t(buf, 12, gpsAlt); _mav_put_int32_t(buf, 16, baroAltMSL); _mav_put_uint32_t(buf, 20, accuracyHor); _mav_put_uint16_t(buf, 24, accuracyVert); _mav_put_uint16_t(buf, 26, accuracyVel); _mav_put_int16_t(buf, 28, velVert); _mav_put_int16_t(buf, 30, velNS); _mav_put_int16_t(buf, 32, VelEW); _mav_put_uint16_t(buf, 34, state); _mav_put_uint16_t(buf, 36, squawk); _mav_put_uint8_t(buf, 38, gpsFix); _mav_put_uint8_t(buf, 39, numSats); _mav_put_uint8_t(buf, 40, emergencyStatus); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC, buf, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_MIN_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_CRC); #else mavlink_uavionix_adsb_out_dynamic_t *packet = (mavlink_uavionix_adsb_out_dynamic_t *)msgbuf; packet->utcTime = utcTime; packet->gpsLat = gpsLat; packet->gpsLon = gpsLon; packet->gpsAlt = gpsAlt; packet->baroAltMSL = baroAltMSL; packet->accuracyHor = accuracyHor; packet->accuracyVert = accuracyVert; packet->accuracyVel = accuracyVel; packet->velVert = velVert; packet->velNS = velNS; packet->VelEW = VelEW; packet->state = state; packet->squawk = squawk; packet->gpsFix = gpsFix; packet->numSats = numSats; packet->emergencyStatus = emergencyStatus; _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC, (const char *)packet, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_MIN_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_CRC); #endif } #endif #endif // MESSAGE UAVIONIX_ADSB_OUT_DYNAMIC UNPACKING /** * @brief Get field utcTime from uavionix_adsb_out_dynamic message * * @return [s] UTC time in seconds since GPS epoch (Jan 6, 1980). If unknown set to UINT32_MAX */ static inline uint32_t mavlink_msg_uavionix_adsb_out_dynamic_get_utcTime(const mavlink_message_t* msg) { return _MAV_RETURN_uint32_t(msg, 0); } /** * @brief Get field gpsLat from uavionix_adsb_out_dynamic message * * @return [degE7] Latitude WGS84 (deg * 1E7). If unknown set to INT32_MAX */ static inline int32_t mavlink_msg_uavionix_adsb_out_dynamic_get_gpsLat(const mavlink_message_t* msg) { return _MAV_RETURN_int32_t(msg, 4); } /** * @brief Get field gpsLon from uavionix_adsb_out_dynamic message * * @return [degE7] Longitude WGS84 (deg * 1E7). If unknown set to INT32_MAX */ static inline int32_t mavlink_msg_uavionix_adsb_out_dynamic_get_gpsLon(const mavlink_message_t* msg) { return _MAV_RETURN_int32_t(msg, 8); } /** * @brief Get field gpsAlt from uavionix_adsb_out_dynamic message * * @return [mm] Altitude (WGS84). UP +ve. If unknown set to INT32_MAX */ static inline int32_t mavlink_msg_uavionix_adsb_out_dynamic_get_gpsAlt(const mavlink_message_t* msg) { return _MAV_RETURN_int32_t(msg, 12); } /** * @brief Get field gpsFix from uavionix_adsb_out_dynamic message * * @return 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS, 5: RTK */ static inline uint8_t mavlink_msg_uavionix_adsb_out_dynamic_get_gpsFix(const mavlink_message_t* msg) { return _MAV_RETURN_uint8_t(msg, 38); } /** * @brief Get field numSats from uavionix_adsb_out_dynamic message * * @return Number of satellites visible. If unknown set to UINT8_MAX */ static inline uint8_t mavlink_msg_uavionix_adsb_out_dynamic_get_numSats(const mavlink_message_t* msg) { return _MAV_RETURN_uint8_t(msg, 39); } /** * @brief Get field baroAltMSL from uavionix_adsb_out_dynamic message * * @return [mbar] Barometric pressure altitude (MSL) relative to a standard atmosphere of 1013.2 mBar and NOT bar corrected altitude (m * 1E-3). (up +ve). If unknown set to INT32_MAX */ static inline int32_t mavlink_msg_uavionix_adsb_out_dynamic_get_baroAltMSL(const mavlink_message_t* msg) { return _MAV_RETURN_int32_t(msg, 16); } /** * @brief Get field accuracyHor from uavionix_adsb_out_dynamic message * * @return [mm] Horizontal accuracy in mm (m * 1E-3). If unknown set to UINT32_MAX */ static inline uint32_t mavlink_msg_uavionix_adsb_out_dynamic_get_accuracyHor(const mavlink_message_t* msg) { return _MAV_RETURN_uint32_t(msg, 20); } /** * @brief Get field accuracyVert from uavionix_adsb_out_dynamic message * * @return [cm] Vertical accuracy in cm. If unknown set to UINT16_MAX */ static inline uint16_t mavlink_msg_uavionix_adsb_out_dynamic_get_accuracyVert(const mavlink_message_t* msg) { return _MAV_RETURN_uint16_t(msg, 24); } /** * @brief Get field accuracyVel from uavionix_adsb_out_dynamic message * * @return [mm/s] Velocity accuracy in mm/s (m * 1E-3). If unknown set to UINT16_MAX */ static inline uint16_t mavlink_msg_uavionix_adsb_out_dynamic_get_accuracyVel(const mavlink_message_t* msg) { return _MAV_RETURN_uint16_t(msg, 26); } /** * @brief Get field velVert from uavionix_adsb_out_dynamic message * * @return [cm/s] GPS vertical speed in cm/s. If unknown set to INT16_MAX */ static inline int16_t mavlink_msg_uavionix_adsb_out_dynamic_get_velVert(const mavlink_message_t* msg) { return _MAV_RETURN_int16_t(msg, 28); } /** * @brief Get field velNS from uavionix_adsb_out_dynamic message * * @return [cm/s] North-South velocity over ground in cm/s North +ve. If unknown set to INT16_MAX */ static inline int16_t mavlink_msg_uavionix_adsb_out_dynamic_get_velNS(const mavlink_message_t* msg) { return _MAV_RETURN_int16_t(msg, 30); } /** * @brief Get field VelEW from uavionix_adsb_out_dynamic message * * @return [cm/s] East-West velocity over ground in cm/s East +ve. If unknown set to INT16_MAX */ static inline int16_t mavlink_msg_uavionix_adsb_out_dynamic_get_VelEW(const mavlink_message_t* msg) { return _MAV_RETURN_int16_t(msg, 32); } /** * @brief Get field emergencyStatus from uavionix_adsb_out_dynamic message * * @return Emergency status */ static inline uint8_t mavlink_msg_uavionix_adsb_out_dynamic_get_emergencyStatus(const mavlink_message_t* msg) { return _MAV_RETURN_uint8_t(msg, 40); } /** * @brief Get field state from uavionix_adsb_out_dynamic message * * @return ADS-B transponder dynamic input state flags */ static inline uint16_t mavlink_msg_uavionix_adsb_out_dynamic_get_state(const mavlink_message_t* msg) { return _MAV_RETURN_uint16_t(msg, 34); } /** * @brief Get field squawk from uavionix_adsb_out_dynamic message * * @return Mode A code (typically 1200 [0x04B0] for VFR) */ static inline uint16_t mavlink_msg_uavionix_adsb_out_dynamic_get_squawk(const mavlink_message_t* msg) { return _MAV_RETURN_uint16_t(msg, 36); } /** * @brief Decode a uavionix_adsb_out_dynamic message into a struct * * @param msg The message to decode * @param uavionix_adsb_out_dynamic C-struct to decode the message contents into */ static inline void mavlink_msg_uavionix_adsb_out_dynamic_decode(const mavlink_message_t* msg, mavlink_uavionix_adsb_out_dynamic_t* uavionix_adsb_out_dynamic) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS uavionix_adsb_out_dynamic->utcTime = mavlink_msg_uavionix_adsb_out_dynamic_get_utcTime(msg); uavionix_adsb_out_dynamic->gpsLat = mavlink_msg_uavionix_adsb_out_dynamic_get_gpsLat(msg); uavionix_adsb_out_dynamic->gpsLon = mavlink_msg_uavionix_adsb_out_dynamic_get_gpsLon(msg); uavionix_adsb_out_dynamic->gpsAlt = mavlink_msg_uavionix_adsb_out_dynamic_get_gpsAlt(msg); uavionix_adsb_out_dynamic->baroAltMSL = mavlink_msg_uavionix_adsb_out_dynamic_get_baroAltMSL(msg); uavionix_adsb_out_dynamic->accuracyHor = mavlink_msg_uavionix_adsb_out_dynamic_get_accuracyHor(msg); uavionix_adsb_out_dynamic->accuracyVert = mavlink_msg_uavionix_adsb_out_dynamic_get_accuracyVert(msg); uavionix_adsb_out_dynamic->accuracyVel = mavlink_msg_uavionix_adsb_out_dynamic_get_accuracyVel(msg); uavionix_adsb_out_dynamic->velVert = mavlink_msg_uavionix_adsb_out_dynamic_get_velVert(msg); uavionix_adsb_out_dynamic->velNS = mavlink_msg_uavionix_adsb_out_dynamic_get_velNS(msg); uavionix_adsb_out_dynamic->VelEW = mavlink_msg_uavionix_adsb_out_dynamic_get_VelEW(msg); uavionix_adsb_out_dynamic->state = mavlink_msg_uavionix_adsb_out_dynamic_get_state(msg); uavionix_adsb_out_dynamic->squawk = mavlink_msg_uavionix_adsb_out_dynamic_get_squawk(msg); uavionix_adsb_out_dynamic->gpsFix = mavlink_msg_uavionix_adsb_out_dynamic_get_gpsFix(msg); uavionix_adsb_out_dynamic->numSats = mavlink_msg_uavionix_adsb_out_dynamic_get_numSats(msg); uavionix_adsb_out_dynamic->emergencyStatus = mavlink_msg_uavionix_adsb_out_dynamic_get_emergencyStatus(msg); #else uint8_t len = msg->len < MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN? msg->len : MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN; memset(uavionix_adsb_out_dynamic, 0, MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC_LEN); memcpy(uavionix_adsb_out_dynamic, _MAV_PAYLOAD(msg), len); #endif }