diff options
Diffstat (limited to 'mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h')
| -rw-r--r-- | mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h | 419 |
1 files changed, 0 insertions, 419 deletions
diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h deleted file mode 100644 index d046f2ad0..000000000 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h +++ /dev/null @@ -1,419 +0,0 @@ -// MESSAGE AIRSPEED_AUTOCAL PACKING - -#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL 174 - -typedef struct __mavlink_airspeed_autocal_t -{ - float vx; ///< GPS velocity north m/s - float vy; ///< GPS velocity east m/s - float vz; ///< GPS velocity down m/s - float diff_pressure; ///< Differential pressure pascals - 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_174_LEN 48 - -#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC 167 -#define MAVLINK_MSG_ID_174_CRC 167 - - - -#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) }, \ - } \ -} - - -/** - * @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 GPS velocity north m/s - * @param vy GPS velocity east m/s - * @param vz GPS velocity down m/s - * @param diff_pressure Differential pressure pascals - * @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; -#if MAVLINK_CRC_EXTRA - return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); -#else - return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); -#endif -} - -/** - * @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 GPS velocity north m/s - * @param vy GPS velocity east m/s - * @param vz GPS velocity down m/s - * @param diff_pressure Differential pressure pascals - * @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; -#if MAVLINK_CRC_EXTRA - return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); -#else - return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); -#endif -} - -/** - * @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 GPS velocity north m/s - * @param vy GPS velocity east m/s - * @param vz GPS velocity down m/s - * @param diff_pressure Differential pressure pascals - * @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); - -#if MAVLINK_CRC_EXTRA - _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); -#else - _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); -#endif -#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; - -#if MAVLINK_CRC_EXTRA - _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)&packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); -#else - _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)&packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); -#endif -#endif -} - -#endif - -// MESSAGE AIRSPEED_AUTOCAL UNPACKING - - -/** - * @brief Get field vx from airspeed_autocal message - * - * @return GPS velocity north m/s - */ -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 GPS velocity east m/s - */ -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 GPS velocity down m/s - */ -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 Differential pressure pascals - */ -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 - 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 - memcpy(airspeed_autocal, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); -#endif -} |