diff options
Diffstat (limited to 'mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h')
| -rw-r--r-- | mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h | 501 |
1 files changed, 0 insertions, 501 deletions
diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h deleted file mode 100644 index 732176193..000000000 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h +++ /dev/null @@ -1,501 +0,0 @@ -// MESSAGE HIL_STATE_QUATERNION PACKING - -#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION 115 - -typedef struct __mavlink_hil_state_quaternion_t -{ - uint64_t time_usec; ///< Timestamp (microseconds since UNIX epoch or microseconds since system boot) - float attitude_quaternion[4]; ///< Vehicle attitude expressed as normalized quaternion - float rollspeed; ///< Body frame roll / phi angular speed (rad/s) - float pitchspeed; ///< Body frame pitch / theta angular speed (rad/s) - float yawspeed; ///< Body frame yaw / psi angular speed (rad/s) - int32_t lat; ///< Latitude, expressed as * 1E7 - int32_t lon; ///< Longitude, expressed as * 1E7 - int32_t alt; ///< Altitude in meters, expressed as * 1000 (millimeters) - int16_t vx; ///< Ground X Speed (Latitude), expressed as m/s * 100 - int16_t vy; ///< Ground Y Speed (Longitude), expressed as m/s * 100 - int16_t vz; ///< Ground Z Speed (Altitude), expressed as m/s * 100 - uint16_t ind_airspeed; ///< Indicated airspeed, expressed as m/s * 100 - uint16_t true_airspeed; ///< True airspeed, expressed as m/s * 100 - int16_t xacc; ///< X acceleration (mg) - int16_t yacc; ///< Y acceleration (mg) - int16_t zacc; ///< Z acceleration (mg) -} mavlink_hil_state_quaternion_t; - -#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN 64 -#define MAVLINK_MSG_ID_115_LEN 64 - -#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC 4 -#define MAVLINK_MSG_ID_115_CRC 4 - -#define MAVLINK_MSG_HIL_STATE_QUATERNION_FIELD_ATTITUDE_QUATERNION_LEN 4 - -#define MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION { \ - "HIL_STATE_QUATERNION", \ - 16, \ - { { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \ - { "attitude_quaternion", NULL, MAVLINK_TYPE_FLOAT, 4, 8, offsetof(mavlink_hil_state_quaternion_t, attitude_quaternion) }, \ - { "rollspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_state_quaternion_t, rollspeed) }, \ - { "pitchspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_state_quaternion_t, pitchspeed) }, \ - { "yawspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_hil_state_quaternion_t, yawspeed) }, \ - { "lat", NULL, MAVLINK_TYPE_INT32_T, 0, 36, offsetof(mavlink_hil_state_quaternion_t, lat) }, \ - { "lon", NULL, MAVLINK_TYPE_INT32_T, 0, 40, offsetof(mavlink_hil_state_quaternion_t, lon) }, \ - { "alt", NULL, MAVLINK_TYPE_INT32_T, 0, 44, offsetof(mavlink_hil_state_quaternion_t, alt) }, \ - { "vx", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_hil_state_quaternion_t, vx) }, \ - { "vy", NULL, MAVLINK_TYPE_INT16_T, 0, 50, offsetof(mavlink_hil_state_quaternion_t, vy) }, \ - { "vz", NULL, MAVLINK_TYPE_INT16_T, 0, 52, offsetof(mavlink_hil_state_quaternion_t, vz) }, \ - { "ind_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 54, offsetof(mavlink_hil_state_quaternion_t, ind_airspeed) }, \ - { "true_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 56, offsetof(mavlink_hil_state_quaternion_t, true_airspeed) }, \ - { "xacc", NULL, MAVLINK_TYPE_INT16_T, 0, 58, offsetof(mavlink_hil_state_quaternion_t, xacc) }, \ - { "yacc", NULL, MAVLINK_TYPE_INT16_T, 0, 60, offsetof(mavlink_hil_state_quaternion_t, yacc) }, \ - { "zacc", NULL, MAVLINK_TYPE_INT16_T, 0, 62, offsetof(mavlink_hil_state_quaternion_t, zacc) }, \ - } \ -} - - -/** - * @brief Pack a hil_state_quaternion 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 time_usec Timestamp (microseconds since UNIX epoch or microseconds since system boot) - * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion - * @param rollspeed Body frame roll / phi angular speed (rad/s) - * @param pitchspeed Body frame pitch / theta angular speed (rad/s) - * @param yawspeed Body frame yaw / psi angular speed (rad/s) - * @param lat Latitude, expressed as * 1E7 - * @param lon Longitude, expressed as * 1E7 - * @param alt Altitude in meters, expressed as * 1000 (millimeters) - * @param vx Ground X Speed (Latitude), expressed as m/s * 100 - * @param vy Ground Y Speed (Longitude), expressed as m/s * 100 - * @param vz Ground Z Speed (Altitude), expressed as m/s * 100 - * @param ind_airspeed Indicated airspeed, expressed as m/s * 100 - * @param true_airspeed True airspeed, expressed as m/s * 100 - * @param xacc X acceleration (mg) - * @param yacc Y acceleration (mg) - * @param zacc Z acceleration (mg) - * @return length of the message in bytes (excluding serial stream start sign) - */ -static inline uint16_t mavlink_msg_hil_state_quaternion_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, - uint64_t time_usec, const float *attitude_quaternion, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, uint16_t ind_airspeed, uint16_t true_airspeed, int16_t xacc, int16_t yacc, int16_t zacc) -{ -#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS - char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN]; - _mav_put_uint64_t(buf, 0, time_usec); - _mav_put_float(buf, 24, rollspeed); - _mav_put_float(buf, 28, pitchspeed); - _mav_put_float(buf, 32, yawspeed); - _mav_put_int32_t(buf, 36, lat); - _mav_put_int32_t(buf, 40, lon); - _mav_put_int32_t(buf, 44, alt); - _mav_put_int16_t(buf, 48, vx); - _mav_put_int16_t(buf, 50, vy); - _mav_put_int16_t(buf, 52, vz); - _mav_put_uint16_t(buf, 54, ind_airspeed); - _mav_put_uint16_t(buf, 56, true_airspeed); - _mav_put_int16_t(buf, 58, xacc); - _mav_put_int16_t(buf, 60, yacc); - _mav_put_int16_t(buf, 62, zacc); - _mav_put_float_array(buf, 8, attitude_quaternion, 4); - memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#else - mavlink_hil_state_quaternion_t packet; - packet.time_usec = time_usec; - packet.rollspeed = rollspeed; - packet.pitchspeed = pitchspeed; - packet.yawspeed = yawspeed; - packet.lat = lat; - packet.lon = lon; - packet.alt = alt; - packet.vx = vx; - packet.vy = vy; - packet.vz = vz; - packet.ind_airspeed = ind_airspeed; - packet.true_airspeed = true_airspeed; - packet.xacc = xacc; - packet.yacc = yacc; - packet.zacc = zacc; - mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4); - memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#endif - - msg->msgid = MAVLINK_MSG_ID_HIL_STATE_QUATERNION; -#if MAVLINK_CRC_EXTRA - return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC); -#else - return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#endif -} - -/** - * @brief Pack a hil_state_quaternion 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 time_usec Timestamp (microseconds since UNIX epoch or microseconds since system boot) - * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion - * @param rollspeed Body frame roll / phi angular speed (rad/s) - * @param pitchspeed Body frame pitch / theta angular speed (rad/s) - * @param yawspeed Body frame yaw / psi angular speed (rad/s) - * @param lat Latitude, expressed as * 1E7 - * @param lon Longitude, expressed as * 1E7 - * @param alt Altitude in meters, expressed as * 1000 (millimeters) - * @param vx Ground X Speed (Latitude), expressed as m/s * 100 - * @param vy Ground Y Speed (Longitude), expressed as m/s * 100 - * @param vz Ground Z Speed (Altitude), expressed as m/s * 100 - * @param ind_airspeed Indicated airspeed, expressed as m/s * 100 - * @param true_airspeed True airspeed, expressed as m/s * 100 - * @param xacc X acceleration (mg) - * @param yacc Y acceleration (mg) - * @param zacc Z acceleration (mg) - * @return length of the message in bytes (excluding serial stream start sign) - */ -static inline uint16_t mavlink_msg_hil_state_quaternion_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, - mavlink_message_t* msg, - uint64_t time_usec,const float *attitude_quaternion,float rollspeed,float pitchspeed,float yawspeed,int32_t lat,int32_t lon,int32_t alt,int16_t vx,int16_t vy,int16_t vz,uint16_t ind_airspeed,uint16_t true_airspeed,int16_t xacc,int16_t yacc,int16_t zacc) -{ -#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS - char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN]; - _mav_put_uint64_t(buf, 0, time_usec); - _mav_put_float(buf, 24, rollspeed); - _mav_put_float(buf, 28, pitchspeed); - _mav_put_float(buf, 32, yawspeed); - _mav_put_int32_t(buf, 36, lat); - _mav_put_int32_t(buf, 40, lon); - _mav_put_int32_t(buf, 44, alt); - _mav_put_int16_t(buf, 48, vx); - _mav_put_int16_t(buf, 50, vy); - _mav_put_int16_t(buf, 52, vz); - _mav_put_uint16_t(buf, 54, ind_airspeed); - _mav_put_uint16_t(buf, 56, true_airspeed); - _mav_put_int16_t(buf, 58, xacc); - _mav_put_int16_t(buf, 60, yacc); - _mav_put_int16_t(buf, 62, zacc); - _mav_put_float_array(buf, 8, attitude_quaternion, 4); - memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#else - mavlink_hil_state_quaternion_t packet; - packet.time_usec = time_usec; - packet.rollspeed = rollspeed; - packet.pitchspeed = pitchspeed; - packet.yawspeed = yawspeed; - packet.lat = lat; - packet.lon = lon; - packet.alt = alt; - packet.vx = vx; - packet.vy = vy; - packet.vz = vz; - packet.ind_airspeed = ind_airspeed; - packet.true_airspeed = true_airspeed; - packet.xacc = xacc; - packet.yacc = yacc; - packet.zacc = zacc; - mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4); - memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#endif - - msg->msgid = MAVLINK_MSG_ID_HIL_STATE_QUATERNION; -#if MAVLINK_CRC_EXTRA - return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC); -#else - return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#endif -} - -/** - * @brief Encode a hil_state_quaternion 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 hil_state_quaternion C-struct to read the message contents from - */ -static inline uint16_t mavlink_msg_hil_state_quaternion_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_hil_state_quaternion_t* hil_state_quaternion) -{ - return mavlink_msg_hil_state_quaternion_pack(system_id, component_id, msg, hil_state_quaternion->time_usec, hil_state_quaternion->attitude_quaternion, hil_state_quaternion->rollspeed, hil_state_quaternion->pitchspeed, hil_state_quaternion->yawspeed, hil_state_quaternion->lat, hil_state_quaternion->lon, hil_state_quaternion->alt, hil_state_quaternion->vx, hil_state_quaternion->vy, hil_state_quaternion->vz, hil_state_quaternion->ind_airspeed, hil_state_quaternion->true_airspeed, hil_state_quaternion->xacc, hil_state_quaternion->yacc, hil_state_quaternion->zacc); -} - -/** - * @brief Encode a hil_state_quaternion 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 hil_state_quaternion C-struct to read the message contents from - */ -static inline uint16_t mavlink_msg_hil_state_quaternion_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_hil_state_quaternion_t* hil_state_quaternion) -{ - return mavlink_msg_hil_state_quaternion_pack_chan(system_id, component_id, chan, msg, hil_state_quaternion->time_usec, hil_state_quaternion->attitude_quaternion, hil_state_quaternion->rollspeed, hil_state_quaternion->pitchspeed, hil_state_quaternion->yawspeed, hil_state_quaternion->lat, hil_state_quaternion->lon, hil_state_quaternion->alt, hil_state_quaternion->vx, hil_state_quaternion->vy, hil_state_quaternion->vz, hil_state_quaternion->ind_airspeed, hil_state_quaternion->true_airspeed, hil_state_quaternion->xacc, hil_state_quaternion->yacc, hil_state_quaternion->zacc); -} - -/** - * @brief Send a hil_state_quaternion message - * @param chan MAVLink channel to send the message - * - * @param time_usec Timestamp (microseconds since UNIX epoch or microseconds since system boot) - * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion - * @param rollspeed Body frame roll / phi angular speed (rad/s) - * @param pitchspeed Body frame pitch / theta angular speed (rad/s) - * @param yawspeed Body frame yaw / psi angular speed (rad/s) - * @param lat Latitude, expressed as * 1E7 - * @param lon Longitude, expressed as * 1E7 - * @param alt Altitude in meters, expressed as * 1000 (millimeters) - * @param vx Ground X Speed (Latitude), expressed as m/s * 100 - * @param vy Ground Y Speed (Longitude), expressed as m/s * 100 - * @param vz Ground Z Speed (Altitude), expressed as m/s * 100 - * @param ind_airspeed Indicated airspeed, expressed as m/s * 100 - * @param true_airspeed True airspeed, expressed as m/s * 100 - * @param xacc X acceleration (mg) - * @param yacc Y acceleration (mg) - * @param zacc Z acceleration (mg) - */ -#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS - -static inline void mavlink_msg_hil_state_quaternion_send(mavlink_channel_t chan, uint64_t time_usec, const float *attitude_quaternion, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, uint16_t ind_airspeed, uint16_t true_airspeed, int16_t xacc, int16_t yacc, int16_t zacc) -{ -#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS - char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN]; - _mav_put_uint64_t(buf, 0, time_usec); - _mav_put_float(buf, 24, rollspeed); - _mav_put_float(buf, 28, pitchspeed); - _mav_put_float(buf, 32, yawspeed); - _mav_put_int32_t(buf, 36, lat); - _mav_put_int32_t(buf, 40, lon); - _mav_put_int32_t(buf, 44, alt); - _mav_put_int16_t(buf, 48, vx); - _mav_put_int16_t(buf, 50, vy); - _mav_put_int16_t(buf, 52, vz); - _mav_put_uint16_t(buf, 54, ind_airspeed); - _mav_put_uint16_t(buf, 56, true_airspeed); - _mav_put_int16_t(buf, 58, xacc); - _mav_put_int16_t(buf, 60, yacc); - _mav_put_int16_t(buf, 62, zacc); - _mav_put_float_array(buf, 8, attitude_quaternion, 4); -#if MAVLINK_CRC_EXTRA - _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC); -#else - _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#endif -#else - mavlink_hil_state_quaternion_t packet; - packet.time_usec = time_usec; - packet.rollspeed = rollspeed; - packet.pitchspeed = pitchspeed; - packet.yawspeed = yawspeed; - packet.lat = lat; - packet.lon = lon; - packet.alt = alt; - packet.vx = vx; - packet.vy = vy; - packet.vz = vz; - packet.ind_airspeed = ind_airspeed; - packet.true_airspeed = true_airspeed; - packet.xacc = xacc; - packet.yacc = yacc; - packet.zacc = zacc; - mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4); -#if MAVLINK_CRC_EXTRA - _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)&packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC); -#else - _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)&packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#endif -#endif -} - -#endif - -// MESSAGE HIL_STATE_QUATERNION UNPACKING - - -/** - * @brief Get field time_usec from hil_state_quaternion message - * - * @return Timestamp (microseconds since UNIX epoch or microseconds since system boot) - */ -static inline uint64_t mavlink_msg_hil_state_quaternion_get_time_usec(const mavlink_message_t* msg) -{ - return _MAV_RETURN_uint64_t(msg, 0); -} - -/** - * @brief Get field attitude_quaternion from hil_state_quaternion message - * - * @return Vehicle attitude expressed as normalized quaternion - */ -static inline uint16_t mavlink_msg_hil_state_quaternion_get_attitude_quaternion(const mavlink_message_t* msg, float *attitude_quaternion) -{ - return _MAV_RETURN_float_array(msg, attitude_quaternion, 4, 8); -} - -/** - * @brief Get field rollspeed from hil_state_quaternion message - * - * @return Body frame roll / phi angular speed (rad/s) - */ -static inline float mavlink_msg_hil_state_quaternion_get_rollspeed(const mavlink_message_t* msg) -{ - return _MAV_RETURN_float(msg, 24); -} - -/** - * @brief Get field pitchspeed from hil_state_quaternion message - * - * @return Body frame pitch / theta angular speed (rad/s) - */ -static inline float mavlink_msg_hil_state_quaternion_get_pitchspeed(const mavlink_message_t* msg) -{ - return _MAV_RETURN_float(msg, 28); -} - -/** - * @brief Get field yawspeed from hil_state_quaternion message - * - * @return Body frame yaw / psi angular speed (rad/s) - */ -static inline float mavlink_msg_hil_state_quaternion_get_yawspeed(const mavlink_message_t* msg) -{ - return _MAV_RETURN_float(msg, 32); -} - -/** - * @brief Get field lat from hil_state_quaternion message - * - * @return Latitude, expressed as * 1E7 - */ -static inline int32_t mavlink_msg_hil_state_quaternion_get_lat(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int32_t(msg, 36); -} - -/** - * @brief Get field lon from hil_state_quaternion message - * - * @return Longitude, expressed as * 1E7 - */ -static inline int32_t mavlink_msg_hil_state_quaternion_get_lon(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int32_t(msg, 40); -} - -/** - * @brief Get field alt from hil_state_quaternion message - * - * @return Altitude in meters, expressed as * 1000 (millimeters) - */ -static inline int32_t mavlink_msg_hil_state_quaternion_get_alt(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int32_t(msg, 44); -} - -/** - * @brief Get field vx from hil_state_quaternion message - * - * @return Ground X Speed (Latitude), expressed as m/s * 100 - */ -static inline int16_t mavlink_msg_hil_state_quaternion_get_vx(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int16_t(msg, 48); -} - -/** - * @brief Get field vy from hil_state_quaternion message - * - * @return Ground Y Speed (Longitude), expressed as m/s * 100 - */ -static inline int16_t mavlink_msg_hil_state_quaternion_get_vy(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int16_t(msg, 50); -} - -/** - * @brief Get field vz from hil_state_quaternion message - * - * @return Ground Z Speed (Altitude), expressed as m/s * 100 - */ -static inline int16_t mavlink_msg_hil_state_quaternion_get_vz(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int16_t(msg, 52); -} - -/** - * @brief Get field ind_airspeed from hil_state_quaternion message - * - * @return Indicated airspeed, expressed as m/s * 100 - */ -static inline uint16_t mavlink_msg_hil_state_quaternion_get_ind_airspeed(const mavlink_message_t* msg) -{ - return _MAV_RETURN_uint16_t(msg, 54); -} - -/** - * @brief Get field true_airspeed from hil_state_quaternion message - * - * @return True airspeed, expressed as m/s * 100 - */ -static inline uint16_t mavlink_msg_hil_state_quaternion_get_true_airspeed(const mavlink_message_t* msg) -{ - return _MAV_RETURN_uint16_t(msg, 56); -} - -/** - * @brief Get field xacc from hil_state_quaternion message - * - * @return X acceleration (mg) - */ -static inline int16_t mavlink_msg_hil_state_quaternion_get_xacc(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int16_t(msg, 58); -} - -/** - * @brief Get field yacc from hil_state_quaternion message - * - * @return Y acceleration (mg) - */ -static inline int16_t mavlink_msg_hil_state_quaternion_get_yacc(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int16_t(msg, 60); -} - -/** - * @brief Get field zacc from hil_state_quaternion message - * - * @return Z acceleration (mg) - */ -static inline int16_t mavlink_msg_hil_state_quaternion_get_zacc(const mavlink_message_t* msg) -{ - return _MAV_RETURN_int16_t(msg, 62); -} - -/** - * @brief Decode a hil_state_quaternion message into a struct - * - * @param msg The message to decode - * @param hil_state_quaternion C-struct to decode the message contents into - */ -static inline void mavlink_msg_hil_state_quaternion_decode(const mavlink_message_t* msg, mavlink_hil_state_quaternion_t* hil_state_quaternion) -{ -#if MAVLINK_NEED_BYTE_SWAP - hil_state_quaternion->time_usec = mavlink_msg_hil_state_quaternion_get_time_usec(msg); - mavlink_msg_hil_state_quaternion_get_attitude_quaternion(msg, hil_state_quaternion->attitude_quaternion); - hil_state_quaternion->rollspeed = mavlink_msg_hil_state_quaternion_get_rollspeed(msg); - hil_state_quaternion->pitchspeed = mavlink_msg_hil_state_quaternion_get_pitchspeed(msg); - hil_state_quaternion->yawspeed = mavlink_msg_hil_state_quaternion_get_yawspeed(msg); - hil_state_quaternion->lat = mavlink_msg_hil_state_quaternion_get_lat(msg); - hil_state_quaternion->lon = mavlink_msg_hil_state_quaternion_get_lon(msg); - hil_state_quaternion->alt = mavlink_msg_hil_state_quaternion_get_alt(msg); - hil_state_quaternion->vx = mavlink_msg_hil_state_quaternion_get_vx(msg); - hil_state_quaternion->vy = mavlink_msg_hil_state_quaternion_get_vy(msg); - hil_state_quaternion->vz = mavlink_msg_hil_state_quaternion_get_vz(msg); - hil_state_quaternion->ind_airspeed = mavlink_msg_hil_state_quaternion_get_ind_airspeed(msg); - hil_state_quaternion->true_airspeed = mavlink_msg_hil_state_quaternion_get_true_airspeed(msg); - hil_state_quaternion->xacc = mavlink_msg_hil_state_quaternion_get_xacc(msg); - hil_state_quaternion->yacc = mavlink_msg_hil_state_quaternion_get_yacc(msg); - hil_state_quaternion->zacc = mavlink_msg_hil_state_quaternion_get_zacc(msg); -#else - memcpy(hil_state_quaternion, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); -#endif -} |